Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Curtiss P-1032-11 Hybrid Propulsion Fighter Proposal.
1 x General Electric J31 (I-40) turbojet engine of unknown thrust output power buried within the fuselage; 1 x General Electric T-31 (TG-100) turboprop engine of unknown output power in the nose driving a four-bladed propeller unit in puller arrangement.
Propulsion
553 mph
890 kph | 481 kts
Max Speed
40,354 ft
12,300 m | 8 miles
Service Ceiling
2,299 miles
3,700 km | 1,998 nm
Operational Range
6,050 ft/min
1,844 m/min
Rate-of-Climb