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Deployable radiators for waste heat dissipation from Shuttle payloadsPrototypes of two types of modularized, deployable radiator systems with a high degree of configuration and component commonality to minimize design, development and fabrication costs are currently under development for Shuttle payloads with high waste heat: a rigid radiator system which utilizes aluminum honeycomb panels that are deployed by a scissors mechanism; and two 'flexible' radiator systems which use panels constructed from flexible metal/dielectric composite materials that are deployed by 'unrolling' or 'extending' in orbit. Detail descriptions of these deployable radiator systems along with design and performance features are presented.
Document ID
19770028965
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Cox, R. L.
(Vought Corp. Dallas, TX, United States)
Dietz, J. B.
(Vought Corp. Dallas, TX, United States)
Leach, J. W.
(Vought Corp. Dallas, Tex., United States)
Date Acquired
August 8, 2013
Publication Date
October 1, 1976
Publication Information
Publication: Raumfahrtforschung
Volume: 20
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
77A11817
Funding Number(s)
CONTRACT_GRANT: NAS9-13346
CONTRACT_GRANT: NAS9-14408
Distribution Limits
Public
Copyright
Other

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