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On-Orbit Repair of RCC StructuresOn-orbit repair technologies for reinforced carbon-carbon composite (RCC) structures are critically needed for space shuttle return to flight (RTF) efforts. These technologies are also critically needed for the repair and refurbishment of thermal protection system of future Crew Entry Vehicles (CEV) of space exploration programs. GRABER (Glenn Adhesive Refractory for Bonding and Exterior Repair) has shown multiuse capability for in-space repair of both large repairs and small cracks in space shuttle Reinforced Carbon Carbon (RCC) leading edge material. The concept consists of preparing an adhesive paste and then applying the paste tot he damaged/cracked area of the RCC composites with caulking gun. The adhesive paste cures at 100-120 C and transforms into a high temperature ceramic during vehicle re-entry conditions. Further development and testing are underway to optimize the materials properties and extend the application temperature.
Document ID
20050057089
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Singh, M.
(QSS Group, Inc. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Composite Materials
Meeting Information
Meeting: 7th National Thermal Protection System (TPS) Workshop
Location: Dayton, OH
Country: United States
Start Date: August 31, 2004
End Date: September 2, 2004
Funding Number(s)
CONTRACT_GRANT: NAS3-00145
OTHER: 376-70-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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