NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Development of Coatings for Tantalum Alloy Nozzle VanesA group of silicide coatings developed for the T222 tantalum-base alloy have afforded over 600 hours of protection at 1600 and 2400 F during cyclic exposure in air. These coatings were applied in two steps. A modifier alloy was applied by slurry techniques and was sintered in vacuum prior to siliciding by pack cementation in argon. Application of the modifier alloy by pack cementation was found to be much less effective. The addition of titanium and vanadium to molybdenum and tungsten yielded beneficial modifier alloys, whereas the addition of chromium showed no improvement. After siliciding, the 15Ti- 35W-15V-35Mo modifier alloy exhibited the best performance; one sample survived 1064 hours of oxidation at 2400 F. This same coating was the only coating to reproducibly provide 600 hours of protection at both 1600 and 2400 F; in the second and third of three experiments, involving oxidation of three to five specimens at each temperature in each experiment, no failures were observed in 600 hours of testing. The slurry coatings were also shown to protect the Cb752 and D43 columbium-base alloys.
Document ID
19670026830
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stetson, A. R.
(International Harvester Co. San Diego, CA, United States)
Wimber, R. T.
(International Harvester Co. San Diego, CA, United States)
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Materials, Metallic
Report/Patent Number
RDR-1396-3
NASA-CR-54529
Report Number: RDR-1396-3
Report Number: NASA-CR-54529
Accession Number
67N36159
Funding Number(s)
CONTRACT_GRANT: NAS3-7276
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROTECTIVE COATING
TANTALUM ALLOY
THERMAL PROPERTY
NOZZLE WALL
TEST METHOD
No Preview Available