Structural and Vibration Analysis of 1U Pico –satellite SWAYAM

Guide : Prof. D. W. Pande (Dean, Research and Development; Dept. of Mechanical Engineering, COEP)

• Carried out Vibration Analysis of the structure to simulate the launch conditions; FEA analysis included static structural, modal, harmonic response analysis and random vibration analysis in ANSYS 14.0
• Experimental validation of the simulation results using shaker table at Defence Research and Development Organization (DRDO), Pune and College of Engineering Pune.
• Responsible for Flight model Assembly and Vibration Testing of the satellite SWAYAM carried out at Indian Space Research Organization’s (ISRO) Satellite Centre, Bangalore (ISAC) (Jan ’15- Feb ’15)