Abstract
Nano-satellite going to perform a predominant roll in a future of space industry. These artificial structures move in a closed loop to rationalize the information about the planets for a further study, more over its use in communication and navigation are exceptional. To maintain the steadfast of the signals of the satellites, the external structure needs to have unique properties, because sudden guest launch in the satellites impacts more harmonic load and static structural load to the satellites. So, the Satellite design and the materials decide the strength and lifespan of the Nano-satellites, so that it can able to withstand the space atmospheric condition. In this study, improvement of Nano-satellite design with different composite materials has been analyzed, and the values have been tabulated. The following Nano-satellites structure has been designed, and Static Structural analysis, deformation figured out using Ansys.
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Balaji, R., Talasila, E.R., Oblisamy, L., Ajith, V.S., Basithrahman, A. (2022). Design and Structural Analysis of Nano-satellite. In: Natarajan, S.K., Prakash, R., Sankaranarayanasamy, K. (eds) Recent Advances in Manufacturing, Automation, Design and Energy Technologies. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-16-4222-7_58
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DOI: https://doi.org/10.1007/978-981-16-4222-7_58
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