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Structural tests on space shuttle thermal protection system constructed with nondensified and densified Li 900 and LI 2200 tileStructural tests were conducted on thermal protection systems (TPS) LI 900 and LI 2200 tiles and .41 cm and .23 cm thick strain isolation pads. The bond surface of selected tiles was densified to obtain improved strength. Four basic types of experiments were conducted including tension tests, substrate mismatch (initial imperfection) tests, tension loads eccentrically applied, and pressure loads applied rapidly to the tile top surface. A small initial imperfection mismatch (2.29 m spherical radius on the substrate) did not influence significantly the ultimate failure strength. Densification of the tile bond region improved the strength of TPS constructed both of LI 900 tile and of LI 2200 tile. Pressure shock conditions studied did not significantly affect the TPS strength.
Document ID
19810009885
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Williams, J. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-81903
Accession Number
81N18410
Funding Number(s)
PROJECT: RTOP 506-89-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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