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The 25 kW power module evolution study. Part 1: Payload requirements and growth scenariosPayload power level requirements and their general impact on the baseline and growth versions of the 25 kW power module during the 1983 to 1990 period are discussed. Extended duration Orbiter sortie flight, supported by a power module, with increased payload power requirements per flight, and free-flyer payload missions are included. Other payload disciplines considered, but not emphasized for the 1983 to 1986 period include astrophysics/astronomy, earth observations, solar power satellite, and life sciences. Of these, only the solar power satellite is a prime driver for the power module.
Document ID
19790009716
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
August 1, 1978
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-161143
LMSC-D614921-A-PT-1
Accession Number
79N17887
Funding Number(s)
CONTRACT_GRANT: NAS8-32928
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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