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Simulation of deployment dynamics of spinning spacecraft.Simulation of deployment dynamics of spinning spacecraft, discussing test methods emphasizing gravity compensating techniques
Document ID
19670039596
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Honeycutt, G. H.
Lang, W. E.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 67-207
Accession Number
67A18325
Distribution Limits
Public
Copyright
Other
Keywords
DYNAMICS
SATELLITE ROTATION
SPACECRAFT CONFIGURATION
COMPUTER SIMULATION
SPIN STABILIZATION
GRAVITATIONAL EFFECT

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