Liquid rocket booster study. Volume 2, book 4, appendices 6-8 : Reports of Rocketdyne, Pratt and Whitney, and TRW

Published: Jun 8, 1988.
Physical Description: 1 electronic document

Online Version

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Summary

For 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.

Other Subject(s)

SPACECRAFT PROPULSION AND POWER

Collection

NASA Technical Reports Server (NTRS) Collection.

Note

Document ID: 19900000819.
Accession ID: 90N10135.
NASA-CR-183603.
NAS 1.26:183603.

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