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Simulated meteoroid penetration of reusable surface insulationMeteoroid impact simulation test results on insulation tiles were used to determine penetration resistance of reusable surface insulation attached to simulated shuttle structures. The probability of no meteoroid damage to a typical shuttle orbiter was determined. Specimens were plasma jet tested to determine effects of various size meteoroid cavities on their thermal performance. None of the tiles failed catastrophically, but large, egg-shaped craters did result from meteoroid penetration. The metallic side of a specimen that was completely penetrated showed a petalled hole typical for thin gage shielded structures.
Document ID
19730024752
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lehman, J. K.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Christensen, H. E.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Publication Information
Publication: NASA. Ames Res. Center Symp. on Reusable Surface Insulation for Space Shuttle, Vol. 2
Subject Category
Materials, Nonmetallic
Accession Number
73N33485
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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