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Space shuttle propulsion systemsThis is a presentation of view graphs. The design parameters are given for the redesigned solid rocket motor (RSRM), the Advanced Solid Rocket Motor (ASRM), Space Shuttle Main Engine (SSME), Solid Rocket Booster (SRB) separation motor, Orbit Maneuvering System (OMS), and the Reaction Control System (RCS) primary and Vernier thrusters. Space shuttle propulsion issues are outlined along with ASA program definition, ASA program selection methodology, its priorities, candidates, and categories.
Document ID
19910018886
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bardos, Russell
(NASA Headquarters Washington, DC United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: Space Transportation Propulsion Technology Symposium. Volume 2: Symposium Proceedings
Subject Category
Spacecraft Propulsion And Power
Accession Number
91N28200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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