Klimov VK-3

Turbofan · Klimov
Reaction Turbines
Dry Weight
1850 kg
Thrust To Weight
4.56

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 annular combustion chamber
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 2 Bypass Ratio — Overall Pressure Ratio — Afterburner Yes

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Mikoyan-Gurevich I-3 Klimov VK-3 1 15.78 8.98
All data (12 fields)
Name
Klimov VK-3
Aircraft Engine Manufacturer
Klimov
Aircraft Engine Type
Turbofan
Dry Weight (kg)
1850
Wikipedia Article (URL)
en.wikipedia.org/wiki/Klimov_VK-3
Geared Fan
No
Combustion Chamber
annular combustion chamber
Afterburner
Yes
Streams
2
Thrust To Weight
4.56
Compressor Description
10 stage axial
Turbine Description
three-stage