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Attitude control subsystem study for the Land Mobile Satellite System SpacecraftThis Attitude Control Subsystem study applies the generic antenna control technology to the specific requirements of the Land Mobile Satellite System mission and defines suitable attitude control subsystem designs for both the wrap/rib and hoop/column antenna configurations. The technology developments required to establish technology readiness by 1987 are also identified.
Document ID
19820011407
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tolivar, A. F. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: NASA. Langley Research Center Large Space Systems Technol., Pt. 2, 1981
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
82N19281
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19820011383Collected WorksLarge Space Systems Technology, Part 2, 1981
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