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A Propulsion System for a Scientific Micro/NanospacecraftA preliminary propulsion system design for a 10-100kg. micro/nanospacecraft for generic scientific missions is described. The design drives resulting in this proposed system are discussed as well as current technology developments.
Document ID
20210002803
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/17052
Authors
Bame, D.
Yankura, G.
Lewis, J.
Date Acquired
April 11, 1999
Publication Date
April 11, 1999
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Microspacecraft
Nanospacecraft
propulsion
hot
helium
warm
gas

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