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Design, fabrication, and tests of a metallic shell tile thermal protection system for space transportationA thermal protection tile for earth-to-orbit transports is described. The tiles consist of a rigid external shell filled with a flexible insulation. The tiles tend to be thicker than the current Shuttle rigidized silica tiles for the same entry heat load but are projected to be more durable and lighter. The tiles were thermally tested for several simulated entry trajectories.
Document ID
19910014916
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Macconochie, Ian O.
(NASA Langley Research Center Hampton, VA, United States)
Kelly, H. Neale
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1989
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-101537
NAS 1.15:101537
Report Number: NASA-TM-101537
Report Number: NAS 1.15:101537
Accession Number
91N24229
Funding Number(s)
PROJECT: RTOP 506-49-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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