FABRICATION AND TESTING FOR NANOSATELLITE DEPLOYABLE MECHANISMS
Journal Title: International Journal of Mechanical and Production Engineering Research and Development (IJMPERD ) - Year 2018, Vol 8, Issue 3
Abstract
This paper deals with the deployable mechanisms of nanosatellite like an antenna, Cubesat deployer. A suitable communication antenna as per the CubeSat standard was considered for QB50. The design and deploying mechanism was modeled. A suitable mechanical design was incorporated to deploy the antennas once in orbit. Also, a CAD model of the Cubesat deployed for the Cubesat as per QB50 standards is modeled by using SOLIDWORKS soft. This CAD model is to be subjected to vibration analysis using ANSYS software to ensure that the CubeSat deployed could withstand the launching conditions. The FEA simulation analysis provides information on the performance of the CubeSat deployer at different static, dynamic and environments.
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