Title: PRO/MECHANICA-based structural and random vibration analysis of picosatellite structure

Authors: Sanjay Jayaram; Mark McQuilling; Sridhar Condoor

Addresses: Aerospace and Mechanical Engineering Department, Saint Louis University, Saint Louis, Missouri 63021, USA. ' Aerospace and Mechanical Engineering Department, Saint Louis University, Saint Louis, Missouri 63021, USA. ' Aerospace and Mechanical Engineering Department, Saint Louis University, Saint Louis, Missouri 63021, USA

Abstract: This paper focuses on the structural and vibration analysis of a low-cost picosatellite structure to the launch load environment. This picosatellite complies with the CubeSat program design specifications, where the satellite is less than one kilogram in mass with a dimension of 10 cm³. The satellite structure is treated as a combination of beams and thin plate elements. A detailed finite element model is developed to observe its responses to the quasi-static accelerations induced by the launch vehicle. The natural frequencies of the prototype were computed numerically through finite element based methods and compared with the natural frequencies induced by the launch vehicle. It was also found that the maximum stress experienced by the structure during launch was well within the stress limits of the material.

Keywords: picosatellites; power spectral density; PRO/Mechanica; random vibration; computer aided engineering; structural analysis; vibration analysis; launch load; stress; finite element method; FEM; modelling.

DOI: 10.1504/IJCAET.2012.044585

International Journal of Computer Aided Engineering and Technology, 2012 Vol.4 No.1, pp.90 - 100

Published online: 16 Aug 2014 *

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