Kowasaki TF2: Difference between revisions
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|ref= | |ref= | ||
|type= Afterburning {{wpl|turbofan}} | |type= Afterburning {{wpl|turbofan}} | ||
|length= | |length= {{convert|4145|mm|in|2|abbr=on}} | ||
|diameter= | |diameter= {{convert|1020|mm|in|2|abbr=on}} | ||
|weight= 1135 kg | |weight= {{convert|1135|kg|lb}} | ||
|compressor= | |compressor= {{wpl|Axial compressor}} with 4 low-pressure and 8 high-pressure stages | ||
|combustion= | |combustion= {{wpl|Combustor#Annular|Annular}} | ||
|turbine= | |turbine= 1 low-pressure and 1 high-pressure stage | ||
|fueltype= | |fueltype= | ||
|oilsystem= | |oilsystem= | ||
|power= | |power= | ||
|thrust= | |thrust= {{convert|56.75|kN}} dry; {{convert|86.37|kN}} with afterburner | ||
|compression= | |compression= 24:1 | ||
|bypass= 0.57 | |bypass= 0.57:1 | ||
|aircon= | |aircon= | ||
|turbinetemp= | |turbinetemp= {{convert|1,377|°C|°F}} | ||
|fuelcon= | |fuelcon= | ||
|specfuelcon= | |specfuelcon= | ||
|power/weight= | |power/weight= | ||
|thrust/weight= | |thrust/weight= 5.1 (dry), 7.8 (afterburning) | ||
}} | }} | ||
Revision as of 03:32, 6 October 2019
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The Kowasaki TF2 is a series of afterburning turbofan jet engines developed by Kowasaki Heavy Industries.
Design and development
Variants
Applications
Specifications (TF2-20)
General characteristics
- Type: Afterburning turbofan
- Length: 4,145 mm (163.19 in)
- Diameter: 1,020 mm (40.16 in)
- Dry weight: 1,135 kilograms (2,502 lb)
Components
- Compressor: Axial compressor with 4 low-pressure and 8 high-pressure stages
- Combustors: Annular
- Turbine: 1 low-pressure and 1 high-pressure stage
Performance
- Maximum thrust: 56.75 kilonewtons (12,760 lbf) dry; 86.37 kilonewtons (19,420 lbf) with afterburner
- Overall pressure ratio: 24:1
- Bypass ratio: 0.57:1
- Turbine inlet temperature: 1,377 °C (2,511 °F)
- Thrust-to-weight ratio: 5.1 (dry), 7.8 (afterburning)