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$21 USD / hour
Flag of INDIA
berhampur, india
$21 USD / hour
It's currently 1:10 AM here
Joined July 10, 2020
1 Recommendation

Devbrat N.

@Drexx52

 3.5 (8 reviews)
2.8
2.8
64%
64%
$21 USD / hour
Flag of INDIA
berhampur, india
$21 USD / hour
56%
Jobs Completed
81%
On Budget
63%
On Time
7%
Repeat Hire Rate

Mechanical-Aerospace Engineer

I am a graduate in Mechanical Engineering and post-graduate diploma in Aerospace Manufacturing. Highly skilled and experience in CAD modelling and CAM tasks using SOLIDWORKS, CATIA, Master-CAM, FUSION 360 and NX. Expertise in CAE (FEA, CFD, Thermal, Vibrations, Shock, etc.) analysis & simulations using ANSYS, ABAQUS, MSC PATRAN, MATLAB and HYPERWORKS. Keen towards Rocket Propulsion and filled with curiosity to learn and implement. Enhanced knowledge on: - Launch Vehicles and Space Systems - Space Mission Engineering - Engineering Design and Optimization - Engineering Materials - Manufacturing & Production (GD&T, Technical Drawing & Process Planning) Core understanding of Mathematics & Physics and versatile to work with fields like: - Robotics - Product Development - Industrial and Space Application projects.
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Portfolio

9514114
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
9514058
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
CUBESAT (Design & Analysis)
9509230
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
E-Scooter (Product Design & Development)
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
9508760
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
9508642
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
9508612
Complete assembly of knuckle joint mechanism is designed using SolidWorks and Engineering Drawing sheets are generated as well.
Knuckle Joint - Design & Drawing
Complete assembly of knuckle joint mechanism is designed using SolidWorks and Engineering Drawing sheets are generated as well.
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing
9514114
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations. Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
9514058
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite. The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules: 1. Quasi-Static Structural Analysis 2. Random Vibration Loading Analysis 3. Harmonic Analysis (Sine Vibration Analysis) 4. Modal Analysis (Natural Frequencies) 5. Response Spectrum Analysis (Shock Vibration Analysis) All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
CUBESAT (Design & Analysis)
9509230
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
E-Scooter (Product Design & Development)
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads. Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
9508760
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model. The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
9508642
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
9508612
Complete assembly of knuckle joint mechanism is designed using SolidWorks and Engineering Drawing sheets are generated as well.
Knuckle Joint - Design & Drawing
Complete assembly of knuckle joint mechanism is designed using SolidWorks and Engineering Drawing sheets are generated as well.
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing

Reviews

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Showing 1 - 5 out of 8 reviews
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1.0
₹3,000.00 INR
Project for Devbrat N.
Work was submitted delayed and the whole work was plagiarised. He was directly copy pasting text from other sources.
Matlab and Mathematica
Mechanical Engineering
Mathematics
Aerospace Engineering
+1 more
T
Flag of Mervin A.
@Thomas192
•
1 year ago
1.0
₹3,000.00 INR
sudden contraction of pipe
He delivered Plagiarismed work and wasted a lot of time
Matlab and Mathematica
CAD/CAM
Mechanical Engineering
Product Design
Mathematics
+1 more
T
Flag of Mervin A.
@Thomas192
•
2 years ago
1.0
$50.00 USD
Abaqus Software Work+Research Writings -- 2
Not delivered within deadline!
Mechanical Engineering
Abaqus
User Avatar
Flag of Sabyasachi D.
@debsabyasachi
•
2 years ago
0.0
₹2,000.00 INR
PPT Project
The project is not completed according to the dispute
User Avatar
Flag of Ankit B.
@andyhelp23
•
2 years ago
5.0
$15.00 USD
Project for Devbrat N.
very very great work and on time! would really recommend
Matlab and Mathematica
Solidworks
Mechanical Engineering
Product Design
Mathematics
+1 more
A
Flag of A A.
@alialfadalaqa
•
2 years ago

Experience

Trainee Engineer

Central Tool Room & Training Centre
Jul 2019 - Jul 2020 (1 year)
- CAD applications: SolidWorks / CATIA / PTC Creo / Fusion 360 / AutoCAD - CAM applications: NX / HyperMILL / MasterCAM - CAE applications: ANSYS / ABAQUS Performing CAD, CAM and CAE tasks for highly quality aerospace manufacturing & production as per aerospace standards AS9100.

Education

Bachelor of Technology (Mechanical Engineering)

Biju Pattnaik University of Technology, India 2015 - 2019
(4 years)

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Matlab and Mathematica 3
Mechanical Engineering 3
Product Design 3
Mathematics 3
Solidworks 2

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