The development of the single crystal casting technology has authorise
d the design of new nickel based superalloys for turbine blades suitab
le for this manufacturing process. The absence of grain boundaries, th
e preferential (001) growth orientation and the microstructural homoge
neity give to these alloys a set of properties significantly higher th
an for the conventionally cast superalloys. Some alloys were developed
at ONERA and are now used in the high-temperature turbines of the fre
nch engine manufacturers SNECMA and TURBOMECA. Other single crystal su
peralloys were also developed for applications in land-based industria
l gas turbines and in rocket engines. The studies of the relationships
between the microstructure and the mechanical properties of these all
oys have revealed some very significant effects of the solidification
parameters, of the size of the strengthening gamma' phase precipitates
and of the cristallographic orientation.