Turboprop engine TP 100
Newly developed turboprop engine TP 100 with output shaft power 180 kW is the continuation of development of small turbojet engine TJ100, which has the core role of gas generator in this new application. Exhaust gases from gas generator drives single stage power turbine, power is subsequently transmitted through gearbox on three blades propeller AV723 type with constant speed.
Main advantages of the engine are small installation dimensions, low weight and high static thrust.
TP 100Technical data
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 | 2158 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 | |