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Flexible Plug Repair for Shuttle Wing Leading EdgeIn response to the Columbia Accident Investigation Board report, a plug repair kit has been developed to enable astronauts to repair the space shuttle's wing leading edge (WLE) during orbit. The plug repair kit consists of several 17.78- cm-diameter carbon/silicon carbide (C/SiC) cover plates of various curvatures that can be attached to the refractory carbon-carbon WLE panels using a TZM refractory metal attach mechanism. The attach mechanism is inserted through the damage in the WLE panel and, as it is tightened, the cover plate flexes to conform to the curvature of the WLE panel within 0.050 mm. An astronaut installs the repair during an extravehicular activity (EVA). After installing the plug repair, edge gaps are checked and the perimeter of the repair is sealed using a proprietary material, developed to fill cracks and small holes in the WLE.
Document ID
20120007489
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Camarda, Charles J.
(NASA Headquarters Washington, DC United States)
Sikora, Joseph
(NASA Headquarters Washington, DC United States)
Smith, Russel
(NASA United States)
Rivers, H.
(NASA Headquarters Washington, DC United States)
Scotti, Stephen J.
(NASA Headquarters Washington, DC United States)
Fuller, Alan M.
(United Space Alliance United States)
Klacka, Robert
(General Electric Ceramic Composites, LLC United States)
Reinders, Martin
(Boeing Co. United States)
Schwind, Francis
(Carbon Carbon Advanced Technologies, Inc. Kennedale, TX, United States)
Sullivan, Brian
(Materials Research and Design, Inc. United States)
Lester, Dean
(ATK-Thiokol Propulsion United States)
Date Acquired
August 25, 2013
Publication Date
February 1, 2012
Publication Information
Publication: NASA Tech Briefs, February 2012
Subject Category
Space Transportation And Safety
Report/Patent Number
MSC-24347-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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