Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Pashinin I-21 Single-Seat Monoplane Fighter Protoype.
1 x Klimov M-105P V12 liquid-cooled inline piston engine developing 1,050 horsepower and driving three-bladed propeller unit at the nose.
Propulsion
360 mph
580 kph | 313 kts
Max Speed
34,777 ft
10,600 m | 7 miles
Service Ceiling
472 miles
760 km | 410 nm
Operational Range
4,133 ft/min
1,260 m/min
Rate-of-Climb