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A Propulsion System for a Scientific Micro/NanospacecraftA preliminary propulsion system design for a 10-100 kg. micro/nanospacecraft for generic scientific missions is described. The design drivers resulting in this proposed system are discussed as well as current technology developments.
Document ID
20000056047
Acquisition Source
Headquarters
Document Type
Other
Authors
Lewis, Joseph C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Yankura, George A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Bame, David P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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