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Advanced space engine component developmentsThe principal components of a high-performance advanced space engine are being fabricated and tested at Rocketdyne under NASA contracts. Effort is in progress on the main liquid hydrogen and liquid oxygen turbopumps, thrust chamber, and injector. A description of the primary design and performance parameters, and the mechanical arrangement of each component is presented. Fabrication techniques used in producing test hardware are related and test results and plans are outlined.
Document ID
19760028205
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yost, M.
(Rockwell International Corp. Canoga Park, CA, United States)
Csomor, A.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1975
Subject Category
Spacecraft Propulsion And Power
Accession Number
76A11171
Funding Number(s)
CONTRACT_GRANT: NAS3-16751
Distribution Limits
Public
Copyright
Other

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