Tumansky RD-9

Turbojet · Shenyang
Reaction Turbines
Maximum Takeoff Thrust
29 kN
Diameter
668 mm
Length
5560 mm
Dry Weight
725 kg
Thrust To Weight
5.2

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 —
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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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Yakovlev Yak-140 Tumansky RD-9 1 13.34 7.395
Yakovlev Yak-26 Tumansky RD-9 2 17.16 10.96

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
AE3007C Rolls-Royce 28.6 5.3 16.2 Compare
HTF7500E (AS907-3-1E-A1) Honeywell 29.4 4.2 21.05 Compare
AS907-3-1E-A1 (HTF7500E) Honeywell 29.4 4.2 21.05 Compare
PW307A Pratt & Whitney Canada 28.49 4.2 20.21 Compare
Rybinsk RD-36-35 Rybinsk Motor Factory 28.45 Compare
ALF 502R-3 Textron Lycoming 29.8 5.7 11.4 Compare
All data (15 fields)
Name
Tumansky RD-9
Aircraft Engine Manufacturer
Shenyang
Aircraft Engine Type
Turbojet
Dry Weight (kg)
725
Diameter (mm)
668
Length (mm)
5560
Wikipedia Article (URL)
en.wikipedia.org/wiki/Tumansky_RD-9
Geared Fan
No
Afterburner
Yes
Streams
1
Maximum Takeoff Thrust (kN)
29
Thrust To Weight
5.2
Afterburner Thrust (kN)
37
Compressor Description
Single-spool 9-stage Axial compressor
Turbine Description
axial flow