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Effect of venting and leakage torques on attitude control of the Skylab orbital assembly by CMGsVenting and leakage torque effects on attitude control of Skylab orbital assembly by control moment gyros
Document ID
19790072986
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Levidow, W. (Bellcomm, Inc. Washington, DC, United States)
Date Acquired
September 3, 2013
Publication Date
March 2, 1971
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
TM-71-1022-1
NASA-CR-117392
Report Number: TM-71-1022-1
Report Number: NASA-CR-117392
Accession Number
79N72494
Funding Number(s)
CONTRACT_GRANT: NASW-417
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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