Apollo command module aero-thermodynamic characteristics at hyperbolic earth entry velocities
2nd Annual Meeting ; 1965 ; San Francisco , CA , U.S.A.
1965-01-01
Conference paper
Electronic Resource
English
Earth entry at hyperbolic velocities
AIAA | 1968
|Manned earth entry at hyperbolic velocities
Engineering Index Backfile | 1968
|Manned earth entry at hyperbolic velocities.
AIAA | 1968
|Stability characteristics of the Apollo command module
TIBKAT | 1967
|