Klimov VK-1

Turbojet · Klimov
Reaction Turbines
Maximum Takeoff Thrust
26.5 kN
Diameter
1300 mm
Length
2600 mm
Dry Weight
872 kg
Thrust To Weight
3.1
Specific Fuel Consumption
3090.257 g/(kN·s)

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 Nine can combustion chambers
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 No

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Beriev R-1 Klimov VK-1 2 19.9 20
Lavochkin La-168 Klimov VK-1 1 10.56 9.5
Lavochkin La-200 Klimov VK-1 2 16.351 12.96
Mikoyan-Gurevich I-320 Klimov VK-1 2 15.775 14.2
Mikoyan-Gurevich MiG-15 Klimov VK-1 1 10.102 10.085
Tupolev Tu-14 Klimov VK-1 2 21.95 21.69
Tupolev Tu-82 Klimov VK-1 2 17.57 17.81
Yakovlev Yak-50 (1949) Klimov VK-1 1 11.12 8.01

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
CFE CFE738 General Electric Company 26.3 5.3 Compare
TEI-TF6000 TEI 26.7 1.08 22 Compare
PW306A Pratt & Whitney Canada 26.87 4.5 20 Compare
PW306B Pratt & Whitney Canada 26.91 4.5 20 Compare
Junkers Jumo 012 Junkers 27.3 Compare
HAL HTFE-25 Hindustan Aeronautics Limited 25 0.5 Compare
All data (16 fields)
Name
Klimov VK-1
Aircraft Engine Manufacturer
Klimov
Aircraft Engine Type
Turbojet
Dry Weight (kg)
872
Diameter (mm)
1300
Length (mm)
2600
Wikipedia Article (URL)
en.wikipedia.org/wiki/Klimov_VK-1
Geared Fan
No
Combustion Chamber
Nine can combustion chambers
Afterburner
No
Streams
1
Maximum Takeoff Thrust (kN)
26.5
Thrust To Weight
3.1
Specific Fuel Consumption (g/(kN·s))
3090.257
Compressor Description
Centrifugal compressor
Turbine Description
single stage axial