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A low-power magnetic torquer for satellite attitude controlMagnetic torquer for satellite attitude control consisting of solenoid with hard magnetic material core
Document ID
19710055766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gibson, C. A.
Polites, M. E.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publisher: CANAVERAL COUNCIL OF TECHNICAL SOCIETIES,
Subject Category
Space Vehicles
Meeting Information
Meeting: TECHNOLOGY TODAY AND TOMORROW, SPACE CONGRESS
Location: COCOA BEACH, FL
Start Date: April 19, 1971
End Date: April 23, 1971
Sponsors: CANAVERAL COUNCIL OF TECHNICAL SOCIETIES
Accession Number
71A36463
Distribution Limits
Public
Copyright
Other

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