Dynamic stability derivatives of large angle blunted conical spacecraft near transonic speed in simulated Mars environment for various angles of attack
Damping derivatives of 120 deg conical spacecraft from flights in a low-density environment.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING ; 1969 ; NEW YORK, NY
1969-08-01
Sonstige
Keine Angabe
Englisch
Maintainability of manned spacecraft for long-duration flights
Engineering Index Backfile | 1968