The engine is used to propel light aerial vehicles, e.g. ultralight sport aircraft, manned vehicles in the Experimental class, to propel various unmanned aerial vehicles (training aerial targets, UAV/UAS (unmanned aerial vehicles/systems), unmanned combat aerial vehicles (UCAVs) and special applications), or as a propulsion system for motorised gliders.
Engine technology:
Single-stage radial compressor, radial and axial diffuser, annular combustor and single-stage axial turbine. The rotor arrangement is lubricated by an autonomous oil system. The engine is controlled by an electronic system with a low voltage ignition system, the start is electric, as is the oil and fuel pump. Power to the engine is provided by a built-in generator and DC-DC converter.
Optional accessories can be ordered for the engine, e.g. fuel solenoid valve, fuel filter, throttle control lever, user software, front and rear fairing, height sensor, signal panel and other accessories
Manufacturer.
Units produced: about 300 of all versions (TJ 100A and TJ 100C) (from 2008 to December 2011)
Engine thrust:
- Max. 1100 N (247.0 lbf)
Gross weight: 19.5 kg (43.0 lb)
Length: 625 mm (24.6 in)
Max. 272 mm (10.7 in) diameter
Electrical power output: 750 W, 28 V
Flight Envelope:
Altitude: 0 to 8000 m (0 to 26,000 ft)
Speed: Mach 0.8
Launch Envelope:
Altitude: 0 to 4000 m (0 to 13 000 ft)
Speed: Mach 0.4
Temperature range: -30°C to +50°C (-22°F to +122°F)
Fuel: JET A-1, JP-5, JP-8
Oil: 3cST or 5cST
Fuel consumption: ≤ 1.09 kg/daN/h
Source:
http://www.pbsvb.cz/turbinovy-motor-tj-100
Engine technology:
Single-stage radial compressor, radial and axial diffuser, annular combustor and single-stage axial turbine. The rotor arrangement is lubricated by an autonomous oil system. The engine is controlled by an electronic system with a low voltage ignition system, the start is electric, as is the oil and fuel pump. Power to the engine is provided by a built-in generator and DC-DC converter.
Optional accessories can be ordered for the engine, e.g. fuel solenoid valve, fuel filter, throttle control lever, user software, front and rear fairing, height sensor, signal panel and other accessories
Manufacturer.
Units produced: about 300 of all versions (TJ 100A and TJ 100C) (from 2008 to December 2011)
Engine thrust:
- Max. 1100 N (247.0 lbf)
Gross weight: 19.5 kg (43.0 lb)
Length: 625 mm (24.6 in)
Max. 272 mm (10.7 in) diameter
Electrical power output: 750 W, 28 V
Flight Envelope:
Altitude: 0 to 8000 m (0 to 26,000 ft)
Speed: Mach 0.8
Launch Envelope:
Altitude: 0 to 4000 m (0 to 13 000 ft)
Speed: Mach 0.4
Temperature range: -30°C to +50°C (-22°F to +122°F)
Fuel: JET A-1, JP-5, JP-8
Oil: 3cST or 5cST
Fuel consumption: ≤ 1.09 kg/daN/h
Source:
http://www.pbsvb.cz/turbinovy-motor-tj-100
