Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Lockheed Martin F-21 4.5 Generation Multirole Fighter Aircraft.
ESTIMATED: 1 x General Electric F110-GE-129 afterburning turbofan engine developing around 18,000lb thrust on dry and near 30,000lb of thrust with reheat.
Propulsion
1,317 mph
2,120 kph | 1,145 kts
Max Speed
50,033 ft
15,250 m | 9 miles
Service Ceiling
2,622 miles
4,220 km | 2,279 nm
Operational Range
50,000 ft/min
15,240 m/min
Rate-of-Climb