Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Curtiss XA-40 Single-Seat, Single-Engine Light Bomber Proposal.
1 x Wright R-3350-8 "Duplex Cyclone" air-cooled radial piston engine developing between 2,200 and 3,200 horsepower while driving a four-bladed propeller unit at the nose.
Propulsion
357 mph
575 kph | 310 kts
Max Speed
26,247 ft
8,000 m | 5 miles
Service Ceiling
1,864 miles
3,000 km | 1,620 nm
Operational Range
2,200 ft/min
671 m/min
Rate-of-Climb