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The paper deals with the design, working and integration of the mechanical systems division of a small spacecraft bound for a lunar mission. It provides a detailed study on the type of structure used, the material selection criterion and an overview of the propulsion system selection among other aspects.

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This page is a summary of: Mechanical Systems of SRMSAT - 2, September 2016, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2016-5241.
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