TJ80 Turbojet Engine

The turbojet engine TJ100 is especially suitable for unmanned aerial vehicles,
target drones, missiles, micro jets and powered gliders. The TJ100 engine has compact design and has an excellent power-to-weight ratio up to 1,300 N with low fuel consumption for
its power category. This engine is also suitable for water landing. It has classic design - radial compressor, radial and axial diffuser, annular combustion chamber, axial turbine and fixed output nozzle.
Main features:
• Compact design
• Excellent thrust-to-weight ratio and low fuel consumption for its power category
• Integrated starter-generator supplies electricity to the vehicle's on-board wiring and cools the  engine after shutdown
• Variations according to customer's request

•Standard assembly:  internal fuel-oil system, control system (FADEC), ignition unit, interconnecting cable
• Optional accessories: electromagnetic stop valve, fuel filter, control lever, signalling panel, boost pump, reduction valve, interface CAN, user software, front and exhaust cover

Technical parameters    
Max. thrust 1,300 N 292 lbf
Power supply 28 V DC 28 V DC
Electrical power output 650 W 650 W
Specific fuel consumption 0.116 kg/N/h 1.1376 lb/lbf/hr
Fuel consumption - idle / max. thrust 700 / 3,120 ml/min 23,67 / 105,5 fl oz/min
Dimensions and weight    
Outside diameter 272 mm  10.7 in
Length 625 mm  24.6 in
Weight 19.5 kg 43 lb
Weight of accessories 1.05 kg 2.32 lb
Other parameters    
Max. engine speed 60,600 RPM  60,600 RPM
Fuel JET A, A-1, B  according to DERD 2494 standard,
 TS-1, T2, RT according to GOST 10227-86 standard
Oil Mobil Jet Oil II / AEROSHELL 560 according to MIL-L-23699
Operating range - engine operation    
Altitude 0 m to 10,000 m 0 ft to 32,808 ft
Speed 0 to 0.8 M 0 to 0.8 M
Ambient temperature -50°C to +50°C -58°F to +122°F
Operating range - engine start    
Altitude 0 m to 6,000 m 0 ft to 19,685 ft
Speed 0 to 0.6 M 0 to 0.6 M
Ambient temperature -40°C to +50°C -40°F to +122°F


The engine can be equipped with optional accessories, e.g. electromagnetic fuel valve, fuel filter, gas control lever, user SW, front and rear cowl, altitude sensor, annunciator panel, etc. - contact us for more information. 

Turbojet engine TJ80