Turbojet engine Р27Ф2М-300

Available for sale turbojet engine with afterburner Р27Ф2М-300. 

1 PCs

Year of 1995

the First of the engines within the family Р29-300 — the engine Р27Ф2-300. Installed on MiG-23УБ modification Р27Ф2М-300 converted 1st and 2nd compressor stage, the gas temperature before the turbine, changed the program of automatic control and the design of the jet nozzle. To increase the stock of gas-dynamic stability of compressor was introduced the by-pass air before the impeller of the 1st stage.

specifications

Thrust at full afterburner - 10200 kgs

Specific fuel consumption for forced mode - of 2.09, kg/kgf.h.

the air Consumption is 95 kg/s

the pressure ratio of 10.9

the gas Temperature before the turbine - 1373 To

Dry weight: 1725 kg

• State: Used

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