Lockheed Martin - USA / Elbit Systems; Israel Aerospace Industries - Israel
(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the Lockheed F-16I production variant)
1 x Pratt & Whitney F100-PW-229 afterburning turbofan engine developing 27,000lb of thrust.
(2,415 kph | 1,304 kts)
(16,000 m | 10 mi)
(3,220 km | 5,963 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
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.