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NASA NTRS ยท 19990008956

Cathodic Protection Deployment on Space Shuttle Solid Rocket Boosters

Abstract

Corrosion 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.

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BibTeXRIS

Zook, Lee M.. 1998-01-01. Cathodic Protection Deployment on Space Shuttle Solid Rocket Boosters. https://ntrs.nasa.gov/citations/19990008956

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