Motion of a spinning satellite during the deployment of asymmetricalappendages.
GALE, E. H. /TRW, INC., TRW SYSTEMS GROUP, INTEGRATION ENGINEERING LAB., REDONDO BEACH, CALIF./., GLUCK, R. /TRW, INC., TRW SYSTEMS GROUP,ENGINEERING MECHANICS LAB., REDONDO BEACH, CALIF./
JOURNAL OF SPACECRAFT AND ROCKETS ; 3 , 10 ; 1463-1469
1966
Article (Journal)
Electronic Resource
English
Attitude Stability of a Spinning Spacecraft During Appendage Deployment/Retraction
British Library Conference Proceedings | 1994
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