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Turboprop engine TP 100 and Turboshaft engine TS 100
Turboprop engine TP 100
Newly developed turboprop engine TP 100 of the output of 180 kW. The basis of TP 100 is the proven engine TJ 100, which fulfils here the function of the gas generator, drives the free turbine and, via a gearbox, a three-bladed propeller with constant speed. The system is designed for use in both push and tractor configuration depending on its mounting on the air vehicle. Thanks to its low weight and output of 185 kW this engine is intended for the category of ultralight both piloted and pilotless air vehicles (UAV).
TP 100Engine availability
The engine is in the stage of prototype tests; the first series will be available in mid-2012.
Turboshaft engine TS 100
Turboshaft engine TS 100 is only a modified variant of the turboprop engine TP 100. The gearbox is modified for the operation with propeller blades. The engine is suitable as a driving unit of the ultralight helicopter.
Engine availability
The engine is in the development stage; first series will be available after the launch of the engine TP 100 on the market, i.e. in mid-2012.
Technical data
Main advantage of these engines are small buildup dimensions, low weight and high static thrust.
Engine parameters |
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| h = 0 m, v0 = 0 km/h | h = 3000 m, v = 350 km/h | |
| Output shaft power | 180 kW | 140 kW |
| Thrust with propeller AV723 | 5394 N | 1357 N |
| Residual thrust | 259 N | 74 N |
| Propeller speed (TP 100) | 2158 ot/min (rpm) | |
| Propeller speed (TS 100) | 6000 ot/min (rpm) | |
Other parameters |
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| Weight (dry) | 55 kg | |
| Engine length | 870 mm | |
| Width x Depth (without exhaust) | 330 x 382 mm | |
| Reducer speed ratio | 20.751 : 1 | |
| Fuel | JET A, A1, B, TS-1, T2, RT | |
| Oil | MIL-L-23699 | |
| Engine ceiling of operation | 9000 m | |
| Engine ceiling for starting | 6000 m | |
