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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
David C Cunningham (Sperry Rand Corporation Phoenix, AZ, United States)
Glen W Driskill (Sperry Rand Corporation Phoenix, AZ, United States)
Date Acquired
August 6, 2013
Subject Category
Navigation
Meeting Information
Meeting: 6th Aerospace Mechanisms Symposium
Location: Moffett Field, CA
Country: US
Start Date: September 9, 1971
End Date: September 10, 1971
Sponsors: Ames Research Center
Accession Number
72N26395
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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