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Cathodic Protection Deployment on Space Shuttle Solid Rocket BoostersCorrosion protection of the space shuttle solid rocket boosters incorporates the use of cathodic protection(anodes) in concert with several coatings systems. The SRB design has large carbon/carbon composites(motor nozzle) electrically connected to an aluminum alloy structure. Early in the STS program, the aluminum structures incurred tremendous corrosive attack due primarily to the galvanic couple to the carbon/carbon nozzle at coating damage locations. Also contributing to the galvanic corrosion problem were stainless steel and titanium alloy components housed within the aluminum structures and electrically connected to the aluminum structures. This paper will highlight the evolution in the protection of the aluminum structures, providing historical information and summary data from the operation of the corrosion protection systems. Also, data and information will be included regarding the evaluation and deployment of inorganic zinc rich primers as anode area on the aluminum structures.
Document ID
19990008956
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Zook, Lee M.
(United Space Boosters, Inc. Cocoa Beach, FL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Cathodic Protection
Location: Norfolk, VA
Country: United States
Start Date: November 3, 1998
Sponsors: American Society for Testing and Materials
Funding Number(s)
CONTRACT_GRANT: NAS8-36300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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