Corrosion tests of a series of heat-resistant nickel alloys were perfo
rmed in a molten 48.7% MgCl2-38.2% KCl-13.1% NaCl ternary eutectic at
500-900 degrees C and with up to 30-h exposure. Chloride corrosion exh
ibits intergranular features and causes weight loss an order of magnit
ude higher than common gaseous oxidation does. Time dependence of the
weight loss is intermediate between parabolic and linear (1 < n < 2),
while the temperature dependence is exponential. The loss is significa
ntly decreased only by alloying with aluminum. The corrosion resistanc
e of NiAl intermetallide is relatively high (it surpasses nickel 60-70
times and commercial heat-resistant alloys 20-30 times). As a functio
n of chromium and titanium contents in binary nickel alloys, corrosion
has minima at 10-12% Cr and 5-7% Ti, respectively; the minimum in mul
ticomponent alloys is located 2-3% lower. Cobalt, molybdenum, and tung
sten affect the chloride corrosion resistance nonadditively, but even
the best variants of alloying are characterized by corrosion of up to
20-30 g/(m(2) h). In order to achieve the required corrosion resistanc
e, commercial high-temperature alloys should be aluminized or protecte
d by a Ni(Co)Al-(beta-phase) intermetallic-based coating.