Mass expulsion and momentum systems for orbiting space station attitude control optimized, considering reaction jet and control moment gyro systems
Attitude control of a manned earth orbiting space station.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, GUIDANCE, CONTROL, AND FLIGHT MECHANICS CONFERENCE ; 1969 ; PRINCETON, NJ
01.08.1969
Aufsatz (Konferenz)
Keine Angabe
Englisch