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small buildup dimensions
low weight
high static thrust
TP100 is based on the proven TJ100 turbojet engine. TJ100 is used as a gas generator that generates combustion gases for powering the free turbine and, via a gearbox (reducer), the propeller. The system is designed for use in both push and tractor configuration depending on its mounting position on the aircraft. Thanks to its low weight and 180 kW output the engine is an ideal solution for powering ultralight manned and unmanned aerial vehicles (UAV).
Form for providing information on the engine TP100
Parameters Download
Valid for ISA: p0 = 101.325 kPa, t0 = 15 °C, v0 = 0 km/h, h=0m
Shaft output 180 kW
Propeller speed 2158 min-1
Torque 797 Nm
Dimensions and weight
Weight w/o working liquids 61,6 kg
Engine length 887 mm
Width × depth (w/o exhaust) 330 x 398 mm
Other data
Maximum flight altitude 9 000 m
Maximum starting altitude 6 000 m
Requirements
Fuel TS-1, T2, RT according to GOST 10227 – 86
JET A, JET A-1, JET B according to DERD 2494
Lubrication Turbine oil MOBIL JET OIL II according to MIL-L-23699
AEROSHELL TURBINE OIL 560 according to DEF STAN 91-94