Heinkel HeS 011

Turbojet · Heinkel-Hirth
Reaction Turbines
Maximum Takeoff Thrust
12.7 kN
Diameter
875 mm
Length
3405 mm
Dry Weight
950 kg
Thrust To Weight
1.38

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 16 chamber annular
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)
Focke-Wulf Flitzer Heinkel HeS 011 1 10.55 8
Focke-Wulf Ta 183 Heinkel HeS 011 1 9.4 10
Heinkel He 343 Heinkel HeS 011 4 15.5 18
Lippisch P.15 Heinkel HeS 011 1 6.4 10.08

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
Lyulka TR-1 Lyulka-Saturn 12.8 Compare
JT15D-5, -5A, -5B Pratt & Whitney Canada 12.9 2.1 12.3 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 (15 fields)
Name
Heinkel HeS 011
Aircraft Engine Manufacturer
Heinkel-Hirth
Aircraft Engine Type
Turbojet
Dry Weight (kg)
950
Diameter (mm)
875
Length (mm)
3405
Wikipedia Article (URL)
en.wikipedia.org/wiki/Heinkel_HeS_011
Geared Fan
No
Combustion Chamber
16 chamber annular
Afterburner
No
Streams
1
Maximum Takeoff Thrust (kN)
12.7
Thrust To Weight
1.38
Compressor Description
Diagonal + 3-stage axial
Turbine Description
2-stage axial