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Deployable radiators for waste heat dissipation from Shuttle payloads

Authors :
Cox, R. L
Dietz, J. B
Leach, J. W
Source :
Raumfahrtforschung. 20
Publication Year :
1976
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1976.

Abstract

Prototypes 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.

Details

Language :
English
Volume :
20
Database :
NASA Technical Reports
Journal :
Raumfahrtforschung
Notes :
NAS9-13346, , NAS9-14408
Publication Type :
Report
Accession number :
edsnas.19770028965
Document Type :
Report