Israel Aircraft Industries (IAI) - Israel
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
Maximum Take-Off Weight
1 x SNECMA Atar 9K-50 turbojet engine developing 15,870lb thrust with afterburner (11,055lb dry) OR 1 x Volvo Flygmotor RM12 (General Electric F404) turbofan engine developing 18,140lb thrust with afterburner (12,500lb dry).
(2,337 kph | 1,262 knots)
(17,700 m | 11 miles)
(1,382 km | 746 nm)
MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
2 x 30mm DEFA internal cannons
Up to 13,790lb of externally-held stores to include AAMs and ASMs as well as conventional drop stores and rockets.
Nammer - Base Series Name; one example completed.