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Hypervelocity impact tests on Space Shuttle Orbiter thermal protection materialHypervelocity impact tests were conducted to simulate the damage that meteoroids will produce in the Shuttle Orbiter leading edge structural subsystem material. The nature and extent of the damage is reported and the probability of encountering meteoroids with sufficient energy to produce such damage is discussed.
Document ID
19770020458
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Humes, D. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1977
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-X-74039
Report Number: NASA-TM-X-74039
Accession Number
77N27402
Funding Number(s)
PROJECT: RTOP 506-16-36-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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