Description:
The JET CENTRAL TURBINE ENGINES are in its own right a single stage centrifugal flow gas turbine engine, configured to operate as a TURBOJET ENGINE for use mainly, but not exclusively, in remotely piloted fixed wing aircraft. Such aircraft and their control systems must be appropriately designed and constructed to be compatible with the performance of the TURBOJET ENGINE.
Specifications:
- Thrust: 20.4 Kg (45 Lbs.) @ 117,000 RPM
- Idle Thrust: 0.59 Kg (1.3 Lbs)
- RPM Range: 30,000-117,000 RPM
- Weight: 1974 Kg (4.35 Lbs) with starter
- Diameter: 111 mm (4.37 inches)
- Length: 325 mm (12.8 inches), with starter
- Exhaust Temperature: 500°C-720°C (932°F - 1292°F)
- Fuel: Jet A1, 1 -K Kerosene, Diesel
- Fuel Consumption: 0.52 Lt/min (17.5 oz/min) average
- Lubrication: 2.5% Turbine Oil mixed In the fuel
- Maintenance Interval: 25 hours
