Computer simulated physical characteristics of electrically propelled spacecraft for selecting and designing attitude control system
Attitude control of an electrically propelled spacecraft utilizing the primary thrust system.
ANNUAL AVIATION AND SPACE CONFERENCE ; 1968 ; BEVERLY HILLS, CA
1968-01-01
Conference paper
No indication
English
Attitude control of electrically propelled spacecraft utilizing primary thrust system
Engineering Index Backfile | 1968
|