Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the IAI Nammer (Leopard) 4th Generation Fighter Prototype.
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).
Propulsion
1,452 mph
2,337 kph | 1,262 kts
Max Speed
58,071 ft
17,700 m | 11 miles
Service Ceiling
859 miles
1,382 km | 746 nm
Operational Range
46,500 ft/min
14,173 m/min
Rate-of-Climb