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Turbojet engine · PA-KO product

KJ-400

Polish technology.
Compact propulsion.

A compact 400 N turbojet engine for unmanned aerial vehicles. A finished PA-KO propulsion solution with digital engine management and two fuel-system configurations.

Maximum static thrust at STP
400 N
Dry mass
3.7 kg
Fuel-system configurations
2
KJ-400 turbojet engine

KJ-400 · PA-KO technology

Polish technology

Compact engine.
Complete solution.

KJ-400 is a Polish turbojet engine for unmanned aerial vehicles. It combines 400 N of thrust with a compact design and digital ECU control.

Standard and Integrated Pump configurations allow the fuel system to suit the installation. The variants differ in pump location: external to the engine or mounted directly on its casing.

Two configurations

One engine.
Two fuel-system options.

KJ-400 is available in two fuel-system configurations to suit different installation requirements.

Standard

External fuel pump

A configuration with an external brushless fuel pump. The separate component allows its position to be adapted to the platform.

Integrated Pump

Engine-mounted fuel pump

A configuration with a brushless pump mounted directly on the engine casing. The integrated layout simplifies installation and reduces external components.

Digital engine management

The ECU provides automatic start, shutdown and in-flight restart. It supports barometric compensation and PWM / RS232 control and telemetry.

Technical data

KJ-400 in numbers.

Technical specifications of the KJ-400 engine. Two fuel-system configurations: Standard and Integrated Pump.

KJ-400 — Technical data
ParameterValue
Maximum static thrust400 N at STP
Pressure ratio3.8:1
Air mass flow0.65–0.70 kg/s
Idle / maximum speed30,000 / 96,000 rpm
Maximum fuel use1,100 g/min
FuelJet A-1 / kerosene
Maximum exhaust gas temperature (EGT)750°C
Core engine envelope350–390 × 148–150 mm
Dry mass3.7 kg
Fuel pumpExternal or casing-mounted brushless pump
Start systemAutomatic kerosene start
ECU functionsAuto start / stop / restart
Control / telemetryPWM / RS232
Power supply3S LiPo / XT60
Altitude compensationBarometric sensor

Enquire about KJ-400

Let’s talk about
KJ-400 propulsion.

Looking to select an engine configuration or discuss delivery terms? Contact the PA-KO team.

PA-KO catalogue

2026 / 2027 · EN

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