• Executed processes like benchmarking, writing requirements, satellite architecture design, testing and quality assurance

• Designed a configuration to stack the sensor, onboard electronics - FPGA, μC within 5×5×10 cm3 in SolidWorks

• Simulated the structure in ANSYS FEM at acceleration of 7g (g = 9.8m/s2) to compute mode shapes & stress levels

• Manufactured AL6061 prototypes and conducted vibration table, and thermal chamber tests for design verification