Klimov RD-500

Maximum Takeoff Thrust
15.9 kN
Diameter
1090 mm
Length
2110 mm
Dry Weight
580.7 kg
Thrust To Weight
2.73

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
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)
Lavochkin La-15 Klimov RD-500 1 9.56 8.83
Shenyang JJ-1 Klimov RD-500 1 10.56 11.43
Yakovlev Yak-1000 Klimov RD-500 1 11.69 4.59
Yakovlev Yak-23 Klimov RD-500 1 8.13 8.73
Yakovlev Yak-30 (1948) Klimov RD-500 1 8.58 8.65

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
TFE731-2-2B Allied Signal 15.6 2.64 13.9 Compare
TFE731-3 Allied Signal 16.5 2.64 14.3 Compare
Westinghouse J34 Westinghouse 15.12 Compare
JT15D-5C Pratt & Whitney Canada 14.19 2.1 13.3 Compare
Ishikawajima-Harima J3 IHI Corporation 13.7 Compare
All data (15 fields)
Name
Klimov RD-500
Aircraft Engine Manufacturer
Klimov
Aircraft Engine Type
Turbojet
Dry Weight (kg)
580.7
Diameter (mm)
1090
Length (mm)
2110
Wikipedia Article (URL)
en.wikipedia.org/wiki/Klimov_RD-500
Geared Fan
No
Combustion Chamber
Nine
Afterburner
No
Streams
1
Maximum Takeoff Thrust (kN)
15.9
Thrust To Weight
2.73
Compressor Description
Single-stage centrifugal compressor
Turbine Description
Single-stage