Microspacecraft: A Concept

Jones, R. M.

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