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Space Transportation Main EngineThe topics are presented in viewgraph form and include the following: Space Transportation Main Engine (STME) definition, design philosophy, robust design, maximum design condition, casting vs. machined and welded forgings, operability considerations, high reliability design philosophy, engine reliability enhancement, low cost design philosophy, engine systems requirements, STME schematic, fuel turbopump, liquid oxygen turbopump, main injector, and gas generator. The major engine components of the STME and the Space Shuttle Main Engine are compared.
Document ID
19920023037
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jan C. Monk (Consolidated Program Support Services (CPSS PP&C) Redstone Arsenal, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: NASA. Goddard Space Flight Center, Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
Location: Huntsville, AL
Country: US
Start Date: April 28, 1992
End Date: April 30, 1992
Sponsors: Marshall Space Flight Center
Accession Number
92N32281
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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