ISENGARD
Gas turbine systems
TJ-40
TJ-40 turbine
Compact class 40.
A single-spool turbojet for unmanned aerial vehicles and defense platforms - a balance of thrust, efficiency, and rugged reliability in a tightly packaged, airframe-ready envelope.
Specification
TJ-40 datasheet.
Max thrust @ 100% RPM392 N / 40 kgf88.2 lbf
Dry weight3.7 kg8.16 lb
Max rotational speed98,000 rpmidle 40,800 rpm
Compressor pressure ratio3.8 : 1single-spool
Thrust-to-weight10.8 : 1dry
Outer diameter148 mm5.83 in
Overall length370 mm14.57 in
Recommended fuelJet A-1 / Kerosene1.2 lpm
Gallery
Every angle.
TJ-40 turbine
Request the propulsion datasheet.
Full TJ-40 performance and integration data are available to allied governments, primes, and qualified partners.