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RTF Analysis-Shuttle Debris TransportThis demo will rewew the findings of the Shuttle's Debris Transport analysis. The demo focuses on aero analysis of the entlre vehicle in ascent (orbiter, SRB and ET together at low Mach number) for debris transoort and determining maximum allowable debris sizes from various sources. We will present analysis results along with performance data of the simulation runs on Supercomputers such as Columbia.
Document ID
20050182945
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Aftosmis, Michael (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Supercomputing 2004
Location: Pittsburgh, PA
Country: United States
Start Date: November 6, 2004
End Date: November 12, 2004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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