Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Mitsubishi Ki-83 Twin-Engine Heavy Fighter Prototype.
2 x Mitsubishi Ha-211 Ru (Ha-43) 18-cylinder air-cooled radial piston engines developing 2,070 horsepower each driving four-bladed propeller units.
Propulsion
438 mph
705 kph | 381 kts
Max Speed
41,339 ft
12,600 m | 8 miles
Service Ceiling
1,215 miles
1,955 km | 1,056 nm
Operational Range
3,280 ft/min
1,000 m/min
Rate-of-Climb
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).