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A 3-D CFD Analysis of the Space Shuttle RSRM with Propellant Fins at 1 sec. Burnback
Author(s) -
ROGER MORSTADT
Publication year - 2003
Publication title -
36th aiaa/asme/sae/asee joint propulsion conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2003-5105
Subject(s) - propellant , space shuttle , computational fluid dynamics , aerospace engineering , space (punctuation) , physics , mechanics , mechanical engineering , materials science , computer science , engineering , operating system

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