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Microspacecraft: A Concept

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dc.contributor.author Jones, R. M. en_US
dc.date.accessioned 2004-10-06T03:41:41Z
dc.date.available 2004-10-06T03:41:41Z
dc.date.issued 1992-05 en_US
dc.identifier.citation Proceedings of the Microtechnology and Applications to Space Systems Workshop en_US
dc.identifier.citation Pasadena, CA en_US
dc.identifier.clearanceno 93-1045 en_US
dc.identifier.uri http://hdl.handle.net/2014/35447
dc.description.abstract There is need for smaller, faster, more frequent space science missions. Smaller spacecraft may enable such missions. Technology has been developed by the United States' Department of Defense and other government agencies that can enable smaller spacecraft. This author has developed a generic concept for utilizing advanced technology to create a microspacecraft. A microspacecraft would have a mass on the order of 10 kg. This paper will present this microspacecraft concept. en_US
dc.format.extent 22857 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.title Microspacecraft: A Concept en_US


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