Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Mikoyan-Gurevich MiG-21bis (Fishbed) Single-Seat Supersonic Fighter Aircraft.
1 x Tumansky R-25-300 afterburning turbojet engine developing 9,030lb of thrust dry and 15,640lb of thrust with reheat.
Propulsion
1,386 mph
2,230 kph | 1,204 kts
Max Speed
59,055 ft
18,000 m | 11 miles
Service Ceiling
721 miles
1,160 km | 626 nm
Operational Range
58,000 ft/min
17,678 m/min
Rate-of-Climb