Tumansky R-25

Turbojet · Tumansky
Reaction Turbines
Maximum Takeoff Thrust
40.3 kN
Diameter
1191 mm
Length
4615 mm
Dry Weight
1212 kg
Thrust To Weight
5.6

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber Cannular 10 burners
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 1 Bypass Ratio — Overall Pressure Ratio — Afterburner Yes

Pictures

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Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
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CF34-3B GE Aircraft Engines 41.01 6.25 19.3 Compare
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All data (16 fields)
Name
Tumansky R-25
Aircraft Engine Manufacturer
Tumansky
Aircraft Engine Type
Turbojet
Dry Weight (kg)
1212
Diameter (mm)
1191
Length (mm)
4615
Wikipedia Article (URL)
en.wikipedia.org/wiki/Tumansky_R-25
Geared Fan
No
Combustion Chamber
Cannular 10 burners
Afterburner
Yes
Streams
1
Maximum Takeoff Thrust (kN)
40.3
Thrust To Weight
5.6
Afterburner Thrust (kN)
69.6
Compressor Description
Two-spool axial compressor 3 LP stages, 5 HP stages
Turbine Description
1 HP stage, 1 LP stage