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In-flight rain damage tests of the shuttle thermal protection systemNASA conducted in-flight rain damage tests of the Shuttle thermal protection system (TPS). Most of the tests were conducted on an F-104 aircraft at the Dryden Flight Research Facility of NASA's Ames Research Center, although some tests were conducted by NOAA on a WP-3D aircraft off the eastern coast of southern Florida. The TPS components tested included LI900 and LI2200 tiles, advanced flexible reusable surface insulation, reinforced carbon-carbon, and an advanced tufi tile. The objective of the test was to define the damage threshold of various thermal protection materials during flight through rain. The test hardware, test technique, and results from both F-104 and WP-3D aircraft are described. Results have shown that damage can occur to the Shuttle TPS during flight in rain.
Document ID
19880011857
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meyer, Robert R., Jr.
(NASA Ames Research Center Moffett Field, CA., United States)
Barneburg, Jack
(NASA Lyndon B. Johnson Space Center Houston, Tex., United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 88-2137
NASA-TM-100438
H-1484
NAS 1.15:100438
Report Number: AIAA PAPER 88-2137
Report Number: NASA-TM-100438
Report Number: H-1484
Report Number: NAS 1.15:100438
Accession Number
88N21241
Funding Number(s)
PROJECT: RTOP 505-61-41
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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