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Fused slurry silicide coatings for columbium alloys reentry heat shields. Volume 1: Evaluation analysisThe R-512E (Si-20Cr-20Fe) fused slurry silicide coating process was optimized to coat full size (20in x 20in) single face rib and corrugation stiffened panels fabricated from FS-85 columbium alloy for 100 mission space shuttle heat shield applications. Structural life under simulated space shuttle lift-off stresses and reentry conditions demonstrated reuse capability well beyond 100 flights for R-512E coated FS-85 columbium heat shield panels. Demonstrated coating damage tolerance showed no immediate structural failure on exposure. The FS-85 columbium alloy was selected from five candidate alloys (Cb-752, C-129Y, WC-3015, B-66 and FS-85) based on the evaluation tests which have designed to determine: (1) change in material properties due to coating and reuse; (2) alloy tolerance to coating damage; (3) coating emittance characteristics under reuse conditions; and (4) new coating chemistries for improved coating life.
Document ID
19730024093
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fitzgerald, B.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1973
Subject Category
Thermodynamics And Combustion
Report/Patent Number
MDC-E0784-VOL-1
NASA-CR-121216
Report Number: MDC-E0784-VOL-1
Report Number: NASA-CR-121216
Accession Number
73N32826
Funding Number(s)
CONTRACT_GRANT: NAS3-14307
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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