The aerodynamic flight test procedures and results for the Space Shuttle orbiter are presented. The aerodynamic characteristics used in testing were determined from flights STS-1 and through STS-4. Normal force and pitching moment were different than predicted, suggesting an unanticipated aerodynamic force acting upward on the end of the orbiter. However, lateral-directional aerodynamic characteristics were in good management with good predictions. The flight measured aerodynamics are repeatable and show good correlation with angle of attack and angle of sideslip.
Launch vehicle aerodynamic flight test results
1983-10-01
Conference paper
No indication
English
Launch Vehicle Performance Enhancement Using Aerodynamic Lifting During Early Flight
British Library Conference Proceedings | 2008
|Titan III Launch Vehicle Flight Test Experience
SAE Technical Papers | 1968
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