Testing was conducted on both plasma-sprayed (PS) and electron beam-physica
l vapor deposited (EB-PVD) Y2O3-stabilized ZrO2 (YSZ) thermal barrier coati
ngs (TBCs) applied directly to oxidation-resistant substrates such as beta-
NiAl, oxide-dispersed FeCrAl, and NiCr. On an alloy that forms a very adher
ent alumina scale, beta-NiAl + Zr, the coating Lifetime of YSZ in furnace c
yclic tests was 6 or more times longer than on state-of-the-art, YSZ coatin
gs on single crystal Ni-base superalloys with MCrAlY or Pt aluminide bond c
oats. Coatings on FeCrAl. alloys appear to be a viable option for applicati
ons such as the external skin of the X-33, single stage to orbit, reusable
launch vehicle. Model chromia-forming bond coat compositions also show prom
ise for power generation applications at temperatures where hot corrosion m
ay be a major problem. In general, while this work examined unique material
s systems, many of the same fundamental failure mechanisms observed in conv
entional TBCs were observed.