Shenzhen Nuobashi Trading Co.,Ltd

This is a micro turbojet engine specially developed for target drones and small tactical missiles.

Design Features
Compressor: 1-stage centrifugal type with a boost ratio of 3.9.
Combustion chamber: annular baffle combustion chamber.
Turbine: 1-stage centripetal.
Nozzle: Simple Converging Nozzle.
Control system: digital electronic control system.
Fuel system: Use RP-3 fuel.
Lubricating oil system: 4010 lubricating oil is used.
Ignition system: motor start or compressed air start, spark plug or electric igniter ignition.
Accessories: starter motor, brushless electric fuel pump.

Technical data
Dimensions
Length: 345mm
Diameter: 158mm

weight
Dry mass: 23kg

Performance
Takeoff thrust: ≥0.42kN
Cruising thrust (H=0, Ma0.3): ≥0.28kN
fuel consumption
Take-off state: 156kg/(kN h)
Life: 20h