- Joined
- 27 December 2005
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So, trying to compile some actual information on modern engines. additions and corrections welcome.
* indicates estimates or uncorroborated figures.
Russian Engines
Note: Allegedly no AL-41F prototype got close to 18000kg thrust.
US Engines
European Engines
Chinese Engines
Others
* indicates estimates or uncorroborated figures.
Russian Engines
Designation | Layout | Mass Flow | Comp Ratio | Bypass Ratio | Weight kg | Inlet Dia. m | Max Dia. m | Length m | TET K | Dry Thrust | A/B Thrust kg | Special Thrust kg | SFC Cruise | SFC Mil | SFC A/B | Engine Life h |
AL-41F1? Izdeliye 30 | 3/5/1/1 | 1450* | 2000-2100 | 11000* | 17000* | 18000* | ||||||||||
AL-41F1 Izdeliye 117 | 4/9/1/1 | 1.18* | 4.942* | 9000 | 14500 | 15000 | 0.655 | |||||||||
AL-41F1S Izdeliye 117S | 4/9/1/1 | 122kg/s* | 1604 | 0.932 | 1.18* | 4.942 | 1745 | 8800 | 14000 | 14500 | 0.77 | 1.78 | 4000 | |||
AL-41F Izdeliye 20 | 3/6/1/1* | 135kg/s* | 1600* | 1.28* | 4.990* | 1873 | 18000 | |||||||||
AL-31F | 4/9/1/1 | 110kg/s | 23:1 | 0.59 | 1530 | 0.905 | 1.18 | 4.945 | 1665 | 7770 | 12500 | - | 0.67 | 0.75 | 1.92 | 1500 |
Note: Allegedly no AL-41F prototype got close to 18000kg thrust.
US Engines
Designation | Layout | Mass Flow kg/s | Comp Ratio | Bypass Ratio | Weight kg | Inlet Dia m | Max Dia m | Length m | TET K | Dry Thrust | A/B Thrust | Special Thrust | SFC Cruise | SFC Mil | SFC A/B | Engine Life h |
F135-PW-100 | 3/6/1/2 | 139.6 | 35:1* | 0.57 | 1701 | 1.09 | 1.17 | 5.588 | 2260 | 12700 | 19500 | - | ||||
F119-PW-100 | 3/6/1/1 | 30:1 | 0.3 | 1,800 | 1.2 | 5.16 | 11 | 15875 | - | |||||||
F110-GE--132 | 3/9/1/2 | 124.7 | 0.68 | 1.2 | 4.7 | 14480 | - | |||||||||
F110-GE-129 | 3/9/1/2 | 122.4 | 0.76 | 1.2 | 4.6 | 13154 | - | |||||||||
F100-PW-232 | 3/10/2/2 | |||||||||||||||
F100-PW-229 | 3/10/2/2 | |||||||||||||||
F414 EPE | ||||||||||||||||
F414 | ||||||||||||||||
F404 | 3/7/1/1 |
European Engines
Chinese Engines
Others
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