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Fabrication process scale-up and optimization for a boron-aluminum composite radiatorDesign approaches to a practical utilization of a boron-aluminum radiator for the space shuttle orbiter are presented. The program includes studies of laboratory composite material processes to determine the feasibility of a structural and functional composite radiator panel, and to estimate the cost of its fabrication. The objective is the incorporation of boron-aluminum modulator radiator on the space shuttle.
Document ID
19730010741
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Okelly, K. P.
(LTV Aerospace Corp. Dallas, TX, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Machine Elements And Processes
Report/Patent Number
REPT-00-1579
NASA-CR-128805
Accession Number
73N19468
Funding Number(s)
CONTRACT_GRANT: NAS9-8260
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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