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Liquid rocket booster study. Volume 2, book 4, appendices 6-8: Reports of Rocketdyne, Pratt and Whitney, and TRWFor the pressure fed engines, detailed trade studies were conducted defining engine features such as thrust vector control methods, thrust chamber construction, etc. This was followed by engine design layouts and booster propulsion configuration layouts. For the pump fed engines parametric performance and weight data was generated for both O2/H2 and O2/RP-1 engines. Subsequent studies resulted in the selection of both LOX/RP-1 and O2/H2 propellants for the pump fed engines. More detailed analysis of the selected LOX/RP-1 and O2/H2 engines was conducted during the final phase of the study.
Document ID
19900000819
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
June 8, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:183603
NASA-CR-183603
Accession Number
90N10135
Funding Number(s)
CONTRACT_GRANT: NAS8-37137
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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