TJ80 Turbojet Engine

TJ80 is a small turbojet engine that has been designed for missiles, target drones and UAVs.
Main features:
• Compact design
• Excellent weight/thrust ratio
• Low fuel consumption in the given output category
• Uniform fuel for both the engine and lubrication
• Maintenance-free operation
• Electric start, possibility of in-flight restart
• Integral generator and inverter
• Startability at high altitude and at high speed

Single-stage radial compressor, radial and axial diffuser, annular combustion chamber, and single-stage axial turbine. Rotor bearings are lubricated by autonomous oil system. The engine is controlled by an electronic system. Start of the engine as well as of the fuel and oil pump is electrical. Power supply is ensured by integral generator and DC-DC converter. Ignition system is a low-voltage system.


Technical parameters: Mode:  
Max. thrust (5 min.) 100% 900N
Continuous thrust 97% 800N
Specific fuel consumption (SFC) 100% 0.122kg/N/h
RPM 100% 58,000
Aiflow 100% 1.47kg/sec.
Electric power output   1,000W
Dimensions and weight    
Max. diameter 235 mm  
Length 512 mm  
Weight w/o working liquids
(with accessories)
10,5 kg  
Operating conditions: Starting envelope: Flight envelope:
Altitude 0 to 6,000 m 0 to 10,000 m
Speed < Mach 0,6 < Mach 0,9
Ambient temperature -40 to +50 °C -50 to +50 °C
Aditional data:    
Engine starting BLDC starter  
Fuel JET-A1, TS-1, RT  
Lubrication 3% oil in fuel (MIL-L-23 699)
Standard accessories (airframe installation)
Engine control unit (ECU), Exciter ignition, Electromagnetic stop valve


PBS_Turbojet-engine_TJ80_EN.pdf

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