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Space Shuttle STS-1 SRB damage investigationThe physical damage incurred by the solid rocket boosters during reentry on the initial space shuttle flight raised the question of whether the hardware, as designed, would yield the low cost per flight desired. The damage was quantified, the cause determined and specific design changes recommended which would preclude recurrence. Flight data, postflight analyses, and laboratory hardware examinations were used. The resultant findings pointed to two principal causes: failure of the aft skirt thermal curtain at the onset of reentry aerodynamic heating, and overloading of the aft shirt stiffening rings during water impact. Design changes were recommended on both the thermal curtain and the aft skirt structural members to prevent similar damage on future missions.
Document ID
19820012361
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Nevins, C. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Space Transportation
Report/Patent Number
NASA-TM-82461
NAS 1.15:82461
Report Number: NASA-TM-82461
Report Number: NAS 1.15:82461
Accession Number
82N20235
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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