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Materials and processes for shuttle engine, external tank, and solid rocket boosterThe Shuttle flight system is composed of the Orbiter, an External Tank (ET) that contains the ascent propellant to be used by the Space Shuttle Main Engines (SSME), and two Solid Rocket Boosters (SRB). The ET is expended on each launch; the Orbiter and SRB's are reusable. It is the requirement for reuse which poses the exciting new materials and processes challenges in the development of the Space Shuttle. A brief description of the Space Shuttle and the mission profile is given. The Shuttle configuration is then described with emphasis on the SSME, ET, and SRB. The materials selection, tracking, and control system used to assure reliability and to minimize cost are described, and salient features and challenges in materials and processes associated with the SSME, ET, and SRB are subsequently discussed.
Document ID
19770018275
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Schwinghamer, R. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1977
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TN-D-8511
M-223
Report Number: NASA-TN-D-8511
Report Number: M-223
Accession Number
77N25219
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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