Lockheed Martin - USA / Hellenic Aerospace Industry - Greece
(Showcased structural values pertain to the Lockheed Martin F-16V production variant)
1 x General Electric GE F110-GE afterburning turbofan engine developing 32,500lb of thrust.
(1,475 kph | 796 kts)
(15,000 m | 9 mi)
(4,215 km | 7,806 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 Vulcan Gatling-style internal cannon.
11 total external hardpoints (2 x Wingtip; 3 x Fuselage; 6 x Underwing) for the carrying of various ordnance types (wingtip mounts reserved for Sidewinder or AMRAAM air-to-air missiles). Up to 17,000lb.
Supported ordnance includes short-range and medium-range air-to-air missiles, laser-guided / precision-guided drop bombs, conventional drop bombs, and rocket pods.
(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 11 (including wingtip mounts).
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.