Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Dornier Do P.254 Mixed-Propulsion Heavy Fighter Aircraft Proposal.
1 x Daimler-Benz DB603A 12-cylinder inverted engine developing 1,725 horsepower and driving a three-bladed propeller at the nose; 1 x Heinkel-Hirth HeS 011 turbojet engine in aft fuselage developing 2,866lb of thrust.
Propulsion
525 mph
845 kph | 456 kts
Max Speed
40,026 ft
12,200 m | 8 miles
Service Ceiling
932 miles
1,500 km | 810 nm
Operational Range
2,300 ft/min
701 m/min
Rate-of-Climb