Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Apollo entry aerodynamics.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ANNUAL MEETING AND TECHNICAL DISPLAY ; 1968 ; PHILADELPHIA, PA
1969-03-01
Miscellaneous
No indication
English
AIAA | 1969
|AIAA | 1968
|NTRS | 1968
|Entry flight aerodynamics from Apollo mission AS-202
NTRS | 1967
|Entry flight aerodynamics from Apollo Mission AS-202
TIBKAT | 1967
|