A 3-D CFD Analysis of the Space Shuttle RSRM with Propellant Fins at 1 sec. Burnback
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
01.01.2003
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A 3-D CFD Analysis of the Space Shuttle RSRM with Propellant Fins @ 1s Burn-back
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