Lyulka TR-1

Turbojet · Lyulka-Saturn
Reaction Turbines
Maximum Takeoff Thrust
12.8 kN
Dry Weight
885 kg
Thrust To Weight
1.47
Specific Fuel Consumption
3653.925 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 —
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

No pictures yet for this family.

Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Alekseyev I-21 Lyulka TR-1 2 11.54 12.25
Ilyushin Il-22 Lyulka TR-1 4 21.05 23.06

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
JT15D-5, -5A, -5B Pratt & Whitney Canada 12.9 2.1 12.3 Compare
Heinkel HeS 011 Heinkel-Hirth 12.7 Compare
BMW 109-718 BMW 12.2625 Compare
Armstrong Siddeley Viper Armstrong Siddeley 12 Compare
Ishikawajima-Harima J3 IHI Corporation 13.7 Compare
JT15D-5C Pratt & Whitney Canada 14.19 2.1 13.3 Compare
All data (13 fields)
Name
Lyulka TR-1
Aircraft Engine Manufacturer
Lyulka-Saturn
Aircraft Engine Type
Turbojet
Dry Weight (kg)
885
Wikipedia Article (URL)
en.wikipedia.org/wiki/Lyulka_TR-1
Geared Fan
No
Afterburner
No
Streams
1
Maximum Takeoff Thrust (kN)
12.8
Thrust To Weight
1.47
Specific Fuel Consumption (g/(kN·s))
3653.925
Compressor Description
eight-stage axial-flow
Turbine Description
single stage