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A torque balance control moment gyroscope assembly for astronaut maneuveringA control moment gyroscope assembly is described for use in an astronaut maneuvering research vehicle. This vehicle (backpack) will be used by astronauts inside the orbiting Skylab for evaluation of various maneuvering systems.
Document ID
19720018745
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cunningham, D. C. (Sperry Rand Corp. Phoenix, AZ, United States)
Driskill, G. W. (Sperry Rand Corp. Phoenix, AZ, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Publication Information
Publication: NASA. Ames Res. Center 6th Aerospace Mech. Symp.
Subject Category
Navigation
Accession Number
72N26395
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19720018727Collected Works6th Aerospace Mechanisms SymposiumN72-26377 17-15Collected Works
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