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Air Force space power technology programThe military spacecraft power subsystem design requirements, developments goals, and planned technology efforts are summarized. The mission drivers of performance (weight and volume), hardening (survivability), autonomy, reliability, and miniaturization influence space mission effectiveness are outlined. The anticipated performance versus power level trends for reactor static conversion systems are illustrated. A conceptual design for a space based radar system is also given.
Document ID
19800024960
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barthelemy, R.
(Air Force Wright Aeronautical Labs. Wright-Patterson AFB, OH, United States)
Mahefkey, T.
(Air Force Wright Aeronautical Labs. Wright-Patterson AFB, OH, United States)
Hebblewaite, T.
(Air Force Wright Aeronautical Labs. Wright-Patterson AFB, OH, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1980
Publication Information
Publication: NASA. Lewis Space Flight Center Synchronous Energy Technol.
Subject Category
Spacecraft Propulsion And Power
Accession Number
80N33468
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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