NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
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.
No Preview Available