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Results of tests on a specimen of the SRB aft skirt heat shield curtain in the MSFC LRLFA full scale segment of the actual Solid Rocket Booster aft skirt heat shield curtain was tested in the Large Radiant Lamp Facility (LRLF) at Marshall Space Flight Center. The curtain was mounted in the horizontal position in the same manner as it is to be mounted on the SRB. A shaker rig was designed and used to provide a motion of the curtain, simulating that to be caused in flight by vehicle acoustics. Thermocouples were used to monitor curtain materials temperatures. Both ascent and reentry heat loads were applied to the test specimen. All aspects of the test setup performed as expected, and the test was declared successful.
Document ID
19850026908
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dean, W. G.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:170883
LMSC-HREC-TM-D697896
NASA-CR-170883
Report Number: NAS 1.26:170883
Report Number: LMSC-HREC-TM-D697896
Report Number: NASA-CR-170883
Accession Number
85N35221
Funding Number(s)
CONTRACT_GRANT: NAS8-32982
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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