Heating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamber. Correlation data on windward laminar and turbulent boundary layers and leeside surfaces of the space shuttle orbiter are included.
Aerodynamic and base heating studies on space shuttle configurations
1974-11-01
Report
No indication
English
AIAA | 1984
|NTRS | 1984
|NTRS | 1983
|AIAA | 1983
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