Engine |
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---|---|---|---|---|---|---|
Engine name | Number | Basic mass | Wing loading |
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|
|
Pratt & Whitney F100-PW-220 | 1 | 7,970 kg | 404 kg/m2 |
Payload weight:
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Engine characteristics | Mass with fuel |
Max Gross Weight |
||||
Weight (each) | Type | 30% (12m) |
100% (41m)
|
193% (41+38m) | ||
1,470 kg | Afterburning low-bypass turbofan | 8,962 kg | 11,275 kg | 14,349 kg | 15,521 kg | |
Maximum engine thrust @ 0 m (RB/SB) | Thrust to weight ratio @ 0 m (WEP) | |||||
Condition | 100% | WEP | ||||
Stationary | 6,490 kgf | 8,995 kgf | 1.00 | 0.80 | 0.63 | 0.58 |
Optimal | 7,434 kgf (1,555 km/h) |
15,247 kgf (1,400 km/h) |
1.70 | 1.35 | 1.06 | 0.98 |
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