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Space shuttle cavity assessment test programIn order to obtain basic radiation properties of the radiator/payload bay door cavity, three tests were conducted on a full-size structural simulator of the cavity. There were three tests conducted: (1) CATA used for determination of exchange factors, absorbed solar flux, and door covering influences, (2) quartz lamp array calibrated to provide IR flux distribution on CATA, and (3) retest with radiometer array for background flux measurement.
Document ID
19770012204
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Scheps, P. B.
(Vought Corp. Dallas, TX, United States)
Date Acquired
September 3, 2013
Publication Date
December 31, 1976
Subject Category
Space Transportation
Report/Patent Number
T169-66
NASA-CR-151221
Report Number: T169-66
Report Number: NASA-CR-151221
Accession Number
77N19148
Funding Number(s)
CONTRACT_GRANT: NAS9-10534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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