Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Curtiss P-36G Single-Seat, Single-Engine Monoplane Fighter Aircraft.
1 x Wright R-1820-G205A Cyclone piston radial engine developing 1,200 horsepower driving a three-bladed propeller unit at the nose.
Propulsion
322 mph
518 kph | 280 kts
Max Speed
32,349 ft
9,860 m | 6 miles
Service Ceiling
650 miles
1,046 km | 565 nm
Operational Range
2,500 ft/min
762 m/min
Rate-of-Climb