F100 | -220 | -229 | -229A (values depend on system requirements) |
---|---|---|---|
Application | F-15, F-16 | ||
Max Thrust (afterburning) | 23,770 lb | 29,100 lb | 29,100 to 35,000 lb |
Intermediate Thrust | 14,590 lb | 17,800 lb | 17,800 to 22,000 lb |
Weight | 3,234 lb | 3,740 lb | 4,100 lb (with provisions for thrust vectoring) |
Length | 191.2 in | 191.0 in | 191.0 in |
Inlet dia. | 34.8 in | 34.8 in | 36 in |
Max Dia. | 46.5 in | 46.5 in | 46.5 in |
Bypass ratio | 0.6 : 1 | 0.35 : 1 | |
Press. ratio | 25 : 1 | 32 : 1 | |
Year | 1985 | 1991 | 1996? |