Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Nakajima G10N Fugaku (Mount Fuji) Very-Long-Range Heavy Bomber Proposal.
6 x Nakajima NK11A 18-cylinder air-cooled radial piston engines developing 2,500 horsepower and driving four-bladed propellers in contra-rotating fashion.
Propulsion
485 mph
780 kph | 421 kts
Max Speed
49,213 ft
15,000 m | 9 miles
Service Ceiling
12,055 miles
19,400 km | 10,475 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).