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NASA NTRS ยท 19800005924

Thermal protection system repair kit program

Abstract

The feasibility and conceptual design aspects of repair materials and procedures for in orbit repair of the space shuttle orbiter TPS tiles are investigated. Material studies to investigate cure in place materials are described including catalyst and cure studies, ablation tests and evaluations, and support mixing and applicator design. The feasibility of the repair procedures, the storage of the TPS, dispensing, and cure problems are addressed.

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BibTeXRIS

1979-11-28. Thermal protection system repair kit program. https://ntrs.nasa.gov/citations/19800005924

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