Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Bisnovat SK-2 Single-Seat, Single-Engine Fighter Prototype.
1 x Klimov M-105 (VK-105) 12-cylinder, liquid-cooled inline piston engine developing 1,050 horsepower and driving a three-bladed propeller unit at the nose.
Propulsion
410 mph
660 kph | 356 kts
Max Speed
36,089 ft
11,000 m | 7 miles
Service Ceiling
404 miles
650 km | 351 nm
Operational Range
3,785 ft/min
1,154 m/min
Rate-of-Climb
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).