Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the TAI Hurjet Twin-Seat, Twin-Engine Supersonic Advanced Jet Trainer Aircraft.
1 x Williams International FJ44-4M non-afterburning turbofan engine developing between 2,000 and 3,500lb of thrust.
Propulsion
920 mph
1,480 kph | 799 kts
Max Speed
44,997 ft
13,715 m | 9 miles
Service Ceiling
1,616 miles
2,600 km | 1,404 nm
Operational Range
35,000 ft/min
10,668 m/min
Rate-of-Climb