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Systems constraints imposed on spacecraft utilizing long extendable rods with attached tip masses.Systems constraints imposed on spacecraft utilizing long flexible rods with attached tip masses, specifically deployment and retraction problems
Document ID
19670045028
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Josloff, A. T.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Space Vehicles
Accession Number
67A23757
Distribution Limits
Public
Copyright
Other
Keywords
SYSTEMS ANALYSIS
ROD
TIP CONTROL
SPACECRAFT STABILITY
FLEXIBLE BODY

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