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Space Shuttle Main Propulsion SystemThe Space Shuttle Main Propulsion System provides the impulse to transfer the reusable Orbiter of the Space Shuttle Transportation system and its payload from earth to earth orbit. Both cryogenic and solid rocket propulsion systems are utilized. The selected systems are characterized by (1) reusability wherever possible to reduce program cost, (2) design pressures, and other important design parameters, for the liquid propellant engine significantly higher than past programs for increased performance, and (3) advanced materials and manufacturing processes to withstand the extreme environments. The approaches for solution of these varied problems are emphasized.
Document ID
19760063103
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wood, C. C.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Date Acquired
August 8, 2013
Publication Date
October 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
IAF PAPER 76-170
Meeting Information
Meeting: International Astronautical Congress
Location: Anaheim, CA
Start Date: October 10, 1976
End Date: October 16, 1976
Sponsors: International Astronautical Federation
Accession Number
76A46069
Distribution Limits
Public
Copyright
Other

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