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Apollo vehicle propulsion systems.H-1, F-1, J-2 and RL-20 Apollo vehicle propulsion systems must have preflight design maturity due to man-rating requirement
Document ID
19650047004
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Belew, L. F.
Patterson, W. H.
Thomas, J. W., Jr.
Date Acquired
August 2, 2013
Publication Date
July 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 65-303
Report Number: AIAA PAPER 65-303
Accession Number
65A29708
Distribution Limits
Public
Copyright
Other
Keywords
PROPULSION SYSTEM PERFORMANCE
APOLLO SPACECRAFT
RL-10 ROCKET ENGINE
ROCKET ENGINE DESIGN
SPACECRAFT PROPULSION

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