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[Engine Performance] Pratt & Whitney F100‑PW‑220 in the F-16As

Engine
Engine name Number Basic mass Wing loading
Pratt & Whitney F100-PW-220 1 7,970 kg 404 kg/m2
Payload weight:
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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