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Power System Designs and Technologies for Small Planetary SpacecraftCurrent Trends. Spacecraft Miniaturization (while maintaining reliability), Rapid, Low Cost Implementation, Low Cost Mission Operations, Less Dependence on Nuclear Fuel, Technology Commercialization.
Document ID
20060038375
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/33913
Authors
Bankston, C. P.
Date Acquired
August 23, 2013
Publication Date
April 1, 1994
Distribution Limits
Public
Copyright
Other
Keywords
low cost implementation nuclear fuel

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