Klimov RD-33

Turbofan · Klimov
Reaction Turbines
Maximum Takeoff Thrust
50 kN
Bypass Ratio
0.49
Diameter
730 mm
Length
4229 mm
Dry Weight
1055 kg
Thrust To Weight
4.82
Specific Fuel Consumption
2124.375 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 annular combustor
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 0.49 Overall Pressure Ratio — Afterburner Yes

Pictures

No pictures yet for this family.

Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
CAC/PAC JF-17 Thunder Klimov RD-33 1 14.33 9.44
HESA Shafaq Klimov RD-33 1 10.84 10.45
Ilyushin Il-102 Klimov RD-33 2 17.5 16.9
Mikoyan MiG-29 Klimov RD-33 2 17.32 11.36

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
IHI Corporation XF5 IHI Corporation 49 Compare
Lyulka AL-5 Lyulka-Saturn 52 Compare
Pratt & Whitney J57 Pratt & Whitney 52 Compare
SPEY Mk511 Rolls-Royce 50.7 0.64 19.9 Compare
Tumansky R-21 Tumansky 46.1 Compare
Snecma M88 SNECMA 50 0.3 Compare
All data (17 fields)
Name
Klimov RD-33
Aircraft Engine Manufacturer
Klimov
Aircraft Engine Type
Turbofan
Dry Weight (kg)
1055
Diameter (mm)
730
Length (mm)
4229
Wikipedia Article (URL)
en.wikipedia.org/wiki/Klimov_RD-33
Geared Fan
No
Combustion Chamber
annular combustor
Afterburner
Yes
Streams
2
Bypass Ratio
0.49
Maximum Takeoff Thrust (kN)
50
Thrust To Weight
4.82
Specific Fuel Consumption (g/(kN·s))
2124.375
Compressor Description
2 spool axial, 4 low pressure stages, 9 high pressure stages
Turbine Description
single stage high pressure, single stage low pressure