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Shuttle/Agena study. Annex A: Ascent agena configurationDetails are presented on the Agena rocket vehicle description, vehicle interfaces, environmental constraints and test requirements, software programs, and ground support equipment. The basic design concept for the Ascent Agena is identified as optimization of reliability, flexibility, performance capabilities, and economy through the use of tested and flight-proven hardware. The development history of the Agenas A, B, and D is outlined and space applications are described.
Document ID
19720013179
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
February 15, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-115485
LMSC-D152635-SER-1-ANNEX-A
Accession Number
72N20829
Funding Number(s)
CONTRACT_GRANT: NAS9-11949
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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