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STME - Streamlining the engine of changeThe key to the success of the NASA Space Transportation Main Engine (STME) is its enhanced reliability and reduced costs, rather than enhanced performance and reduced weight. Reliability and cost improvements derive from the design of an engine with fewer components, wider operating margins, conventional materials, and innovative manufacturing techniques; this is exemplified by the STME's combustion chamber, in which the structural jacket and all minifolds are cast as a single piece. 'Platelet' technology is under active consideration as a basis for the nozzle design. The use of hydrostatic bearings in both the turbine and pump ends of the STME turbopump will eliminate bearing-life limitations.
Document ID
19920065758
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Smelser, Jerry W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Constantine, Marc T.
(Aerojet, Propulsion Div., Sacramento CA, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Publication Information
Publication: Aerospace America
Volume: 30
Issue: 7, Ju
ISSN: 0740-722X
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
ISSN: 0740-722X
Accession Number
92A48382
Distribution Limits
Public
Copyright
Other

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