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Results of tests of the SRB aft skirt heat shield curtain in the MSFC Hot Gas FacilityDuring the first two space shuttle flights the aft skirt heat shield curtain performed well during ascent but failed during reentry. This exposed the inside of the skirt and its subsystems to reentry heating. The resulting exposure damaged various expensive systems items and therefore a curtain reassessment is required. As a part of this reassessment, tests were conducted in the MSFC Hot Gas Facility (HGF). The purposes of these tests were to determine if the curtain would fail in a manner similar to that in flight and to demonstrate that meaningful tests of the curtain can be conducted in the HGF.
Document ID
19850026910
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
February 1, 1982
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
LMSC-HREC-TM-D784643
NASA-CR-170888
NAS 1.26:170888
Report Number: LMSC-HREC-TM-D784643
Report Number: NASA-CR-170888
Report Number: NAS 1.26:170888
Accession Number
85N35223
Funding Number(s)
CONTRACT_GRANT: NAS8-32982
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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