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Concept, Design, and Prototyping of XSAS: A High Power Extendable Solar Array for CubeSat ApplicationsCubeSats have proven themselves as a reliable and cost-effective method to perform experiments in space, but they are highly constrained by their specifications and size. One such constraint is the average continuous power, about 5 W, which is available to the typical CubeSat. To improve this constraint, we have developed the eXtendable Solar Array System (XSAS), a deployable solar array prototype in a CubeSat package, which can provide an average 23 W of continuous power. The prototype served as a technology demonstrator for the high risk mechanisms needed to release, deploy, and control the solar array. Aside from this drastic power increase, it is in the integration of each mechanism, their application within the small CubeSat form-factor, and the inherent passive control benefit of the deployed geometry that make XSAS a novel design. In this paper, we discuss the requirements and design process for the XSAS system and mechanical prototype, and provide qualitative and quantitative results from numerical simulations and prototype tests. We also discuss future work, including an upcoming NASA zero-gravity flight campaign, to further improve on XSAS and prepare it for future launch opportunities.
Document ID
20100021926
Document Type
Conference Paper
Authors
Senatore, Patrick (Michigan Univ. Ann Arbor, MI, United States)
Klesh, Andrew (Michigan Univ. Ann Arbor, MI, United States)
Zurbuchen, Thomas H. (Michigan Univ. Ann Arbor, MI, United States)
McKague, Darren (Michigan Univ. Ann Arbor, MI, United States)
Cutler, James (Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
August 29, 2013
Publication Date
May 12, 2010
Publication Information
Publication: Proceedings of the 40th Aerospace Mechanisms Symposium
Subject Category
Space Sciences (General)
Distribution Limits
Public
Copyright
Public Use Permitted.

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IDRelationTitle20100021914Analytic PrimaryProceedings of the 40th Aerospace Mechanisms Symposium