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Microelectromechanical Systems (MEMS) Technology Integration Into Microspacecraft

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dc.contributor.author Muller, L. en_US
dc.date.accessioned 2004-10-03T04:23:41Z
dc.date.available 2004-10-03T04:23:41Z
dc.date.issued 1995-09 en_US
dc.identifier.citation Logan, UT en_US
dc.identifier.clearanceno 95-1065 en_US
dc.identifier.uri http://hdl.handle.net/2014/31204
dc.description.abstract The need to significantly reduce the mass, power, and volume of future scientific spacecraft has resulted in an increased interest on the part of NASA in the relatively new technology of microelectro- mechanical systems (MEMS). In addition to being light, compact and low-power-consuming, this technology offers other advantages to space applications, such as high performance solid-state reliability. en_US
dc.format.extent 440393 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other microelectromechanical systems MEMS microspacecraft en_US
dc.title Microelectromechanical Systems (MEMS) Technology Integration Into Microspacecraft en_US


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