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Effects of soft foam insulation impactHigh temperature reusable surface insulation (HTRSI) tiles were impacted by a variety of foam insulation materials typical of the debris expected to strike the shuttle orbiter during the initial phases of flight. Failure of the HIRSI coating was strongly dependent on the density and size of the projectile. The failure threshold was as low as 140 ft/sec for rubber and as high as 740 ft/sec for styrofoam. In addition, the impact pressure was measured for a variety of debris materials as a function of velocity.
Document ID
19800005217
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rand, J. L.
(Texas A&M Univ. College Station, TX, United States)
Norton, D. J.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1979
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-160400
Report Number: NASA-CR-160400
Accession Number
80N13472
Funding Number(s)
CONTRACT_GRANT: NAS9-15962
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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