NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Adjustable high emittance gap fillerA flexible, adjustable refractory filler is disclosed for filling gaps between ceramic tiles forming the heat shield of a space shuttle vehicle, to protect its aluminum skin during atmospheric reentry. The easily installed and replaced filler consists essentially of a strip of ceramic cloth coated, at least along both its longitudinal edges with a room temperature vulcanizable silicone rubber compound with a high emittance colored pigment. The filler may have one or more layers as the gap width requires. Preferred materials are basket weave aluminoborosilicate cloth, and a rubber compounded with silicon tetraboride as the emittance agent and finely divided borosilicate glass containing about 7.5% B2O3 as high temperature binder. The filler cloth strip or tape is cut to proper width and length, inserted into the gap, and fastened with previously applied drops of silicone rubber adhesive.
Document ID
19820016463
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Leiser, D. B.
(Stanford Univ. Calif., United States)
Stewart, D. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Smith, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Estrella, C. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Goldstein, H. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
December 29, 1981
Subject Category
Nonmetallic Materials
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-147700
Patent Number: NASA-CASE-ARC-11310-1
Patent Number: US-PATENT-4,308,309
Accession Number
82N24339
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-ARC-11310-1|US-PATENT-4,308,309
Patent Application
US-PATENT-APPL-SN-147700
No Preview Available