Developed in 1973, the TR-18 turbojet
engine family has expanded with the
development of a derivative whose thrust
covers the 90 (200) to 160 daN (360 lbt)
range.
Particularly engineered to achieve a high
thrust-to-weight ratio, an excellent operating
reliability and a low cost of ownership, its
simplicity enables it to be considered as an
excellent contender for any new application
requiring an off-the-shelf engine in this thrust
range.
Already selected and produced for many
aeronautical platforms, its production has
reached a total of more than 1,000 units to
date.
This engine is particularly used in numerous
countries for target drone applications.
Temperature -30 °C to +50 °C