80 kgf Turbojet Engine

A one-button electronic-start turbojet delivering 80 kgf of standard thrust in a 202 mm diameter, 10.5 kg package. It runs on RP-3 aviation kerosene from -40 °C to +60 °C and reaches 60,200 rpm. Ideal for model aviation, performance applications and civilian UAV powerplants.

The 80 kgf turbojet engine is a compact propulsion unit delivering a standard thrust of no less than 80 kgf. Measuring 202 mm in diameter and 479 mm in length with a total weight of no more than 10.5 kg including accessories, it is easy to integrate into a wide range of airframes. The speed range spans 30,000 to 60,200 rpm with a rated exhaust temperature of 750 °C and a fuel consumption rate of 1.38 kg/kgf/h. The engine uses RP-3 aviation kerosene with 3%–5% lubricating oil mixture and features one-click electronic starting on a 28 V power supply. It operates reliably from -40 °C to +60 °C, and a regular maintenance cycle of 50 hours keeps operating costs predictable. Typical uses include model aircraft flying, competitions, performances, and civilian purposes such as firefighting support and road drying and cleaning. Each set ships with the engine body including ECU, clamps and mounting joints.

Key specifications: Standard Thrust: ≥ 80 kgf; Diameter: 202 mm; Length: 479 mm; Total Weight (including accessories): ≤ 10.5 kg; Speed Range: 30,000–60,200 rpm; Rated Exhaust Temperature: 750 °C.

Specifications

All specifications are taken from the manufacturer’s current datasheet.