Junkers Jumo 012

Turbojet · Junkers
Reaction Turbines
Maximum Takeoff Thrust
27.3 kN
Diameter
1064 mm
Length
4860 mm
Dry Weight
2000 kg
Thrust To Weight
1.39

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 8 chamber can-type
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)
Junkers EF 132 Junkers Jumo 012 6 30.7848 32.3088

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
PW306B Pratt & Whitney Canada 26.91 4.5 20 Compare
PW306A Pratt & Whitney Canada 26.87 4.5 20 Compare
TEI-TF6000 TEI 26.7 1.08 22 Compare
Honeywell/ITEC F124 Garrett 28 0.49 Compare
Klimov VK-1 Klimov 26.5 Compare
CFE CFE738 General Electric Company 26.3 5.3 Compare
All data (15 fields)
Name
Junkers Jumo 012
Aircraft Engine Manufacturer
Junkers
Aircraft Engine Type
Turbojet
Dry Weight (kg)
2000
Diameter (mm)
1064
Length (mm)
4860
Wikipedia Article (URL)
en.wikipedia.org/wiki/Junkers_Jumo_012
Geared Fan
No
Combustion Chamber
8 chamber can-type
Afterburner
No
Streams
1
Maximum Takeoff Thrust (kN)
27.3
Thrust To Weight
1.39
Compressor Description
11-stage axial compressor
Turbine Description
2-stage