OEM Direct
20 kgf-Thrust Micro Turbojet Engine
A larger-class single-spool micro turbojet delivering up to 20 kgf of thrust with an integrated ECU and built-in fuel pump. Its mature architecture targets big jet-sport RC aircraft, experimental UAV platforms and propulsion research, with a low 1.574 kg/(kgf·h) fuel burn, EGT held to ≤705 °C and a simple 25-hour maintenance cycle for dependable everyday operation.
Specifications
- Fuel
- Jet-A / kerosene / diesel
- Length
- 255 mm
- Battery
- Li-Po 3S
- Diameter
- 106 mm
- Max power
- 15.8 kW
- Max speed
- 125,000 rpm
- Max thrust
- 20 kgf (~200 N)
- Rated speed
- 51,000 rpm
- Air condition
- 1 atm, 15 °C, density 0.812 kg/L
- Air mass flow
- 0.41 kg/s
- Flight weight
- 1,500 g
- Pressure ratio
- 3.7
- ECU / fuel pump
- Built-in
- Fuel consumption
- 90 ml/min idle – 640 ml/min max
- Maintenance interval
- 25 h
- Max exhaust velocity
- 445 m/s
- Exhaust gas temp (EGT)
- ≤705 °C
- Specific fuel consumption
- 1.574 kg/(kgf·h)