This 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.
RTF Analysis-Shuttle Debris Transport
Supercomputing 2004 ; 2004 ; Pittsburgh, PA, United States
2004-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Space Shuttle Debris Transport
NTRS | 2010
|Space Shuttle Foam Debris Monte Carlo Risk Analysis
AIAA | 2008
|