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Operational Issues in the Development of a Cost-Effective Reusable LOX/LH2 EngineContents include the following: SLI initiated under NASA Research Announcement (NRA) 8-30. Strategic Objectives. Make spaceflight safer (1 in 10000 mission LOV). Make spaceflight cheaper ($1000/lb payload). Two prototype LOX/LH2 engine systems funded under Cycle-1 of NRA8-30. COBRA (Pratt & Whitney / Aerojet). RS-83 (Rocketdyne).
Document ID
20050217130
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Ballard, Richard O. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Publication Information
Publication: Fifth International Symposium on Liquid Space Propulsion
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20050217123Collected WorksFifth International Symposium on Liquid Space Propulsion
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