Lockheed Martin - USA / Elbit Systems; Israel Aerospace Industries - Israel
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Israel
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
32.2 ft
(9.80 m)
Empty Wgt
19,842 lb
(9,000 kg)
MTOW
37,479 lb
(17,000 kg)
Wgt Diff
+17,637 lb
(+8,000 kg)
(Showcased structural values pertain to the Lockheed F-16I production variant)
Installed:
1 x Pratt & Whitney F100-PW-229 afterburning turbofan engine developing 27,000lb of thrust.
Max Speed
1,501 mph
(2,415 kph | 1,304 kts)
Ceiling
52,493 ft
(16,000 m | 10 mi)
Range
2,001 mi
(3,220 km | 5,963 nm)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
STANDARD, FIXED:
1 x 20mm M61A1 internal automatic cannon.
2 x Short-range, air-to-air missiles on wingtip launchers.
Approximately 17,000lb of externally-held drop/launch stores across nine total hardpoints (three under each wing, three under the fuselage). Supported weapon systems include additional short-range or medium-range air-to-air missiles, air-to-surface missiles, precision-guided bombs, conventional drop bombs, and rocket pods. Also supported are 3 x Jettisonable drop tanks.
(Not all ordnance types may be represented in the showcase above)
F-16I "Sufa" - Base Series Designation.
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.