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Space Shuttle Main Engine (SSME) EvolutionThe SSME when developed in the 1970's was a technological leap in space launch propulsion system design. The engine has safely supported the space shuttle for the last two decades and will be required for at least another decade to support human space flight to the international space station. This paper discusses the continued improvements and maturing of the system to its current state and future considerations for its critical role in the nations space program. Discussed are the initiatives of the late 1980's, which lead to three major upgrades through the 1990's. The current capabilities of the propulsion system are defined in the areas of highest programmatic importance: ascent risk, in-flight abort thrust, reusability, and operability. Future initiatives for improved shuttle safety, the paramount priority of the Space Shuttle program are discussed.
Document ID
20020022303
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Worlund, Len A.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Hastings, J. H.
(NASA Marshall Space Flight Center Huntsville, AL United States)
McCool, Alex
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: AIAA Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 8, 2002
End Date: July 11, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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