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Cryogenic upper stage propulsion: RL10 and derivative enginesThe capabilities and characteristics of the RL10 rocket engine are examined. The engine model history is presented. The RL10 derivatives are also outlined. The presentation is represented by viewgraphs.
Document ID
19910018888
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, James R. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: NASA, Washington, Space Transportation Propulsion Technology Symposium. Volume 2: Symposium Proceedings
Subject Category
Spacecraft Propulsion And Power
Accession Number
91N28202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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