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Magnetic control systems for large spacecraft with applications to space telescopeMagnetic control systems for large space vehicles offer the advantage of a simple, reliable, low cost augmentation to the primary control system. When used for momentum management, a magnetic torque source offers a long life and noncontaminant environment when compared to a mass expulsion torque source. These qualities make such systems suitable for employment with the Space Telescope, which is a long life, high performance vehicle with optics and scientific instruments which would be degraded by contamination due to mass expulsion products. The various applications of magnetic systems on the Space Telescope are considered. The future trend in magnetic control of large space vehicles lies in providing a known three axis reference for backup operations, such as recovery of the primary control mode.
Document ID
19810048477
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dougherty, H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Machnick, J.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, Calif., United States)
Nakashima, A.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Henry, J.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Tompetrini, K.
(Bendix Corp. Guidance Systems Div., Teterboro, N.J., United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 81-005
Meeting Information
Meeting: Annual Rocky Mountain Guidance and Control Conference
Location: Keystone, CO
Start Date: January 31, 1981
End Date: February 4, 1981
Sponsors: American Astronautical Society
Accession Number
81A32881
Funding Number(s)
CONTRACT_GRANT: NAS8-32697
Distribution Limits
Public
Copyright
Other

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