Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Curtiss P-304-4 (Type I) Single-Seat, Single-Engine Jet-Powered Fighter Proposal.
1 x General Electric TG-180 turbojet engine developing 4,000lb of thrust.
Propulsion
621 mph
1,000 kph | 540 kts
Max Speed
36,089 ft
11,000 m | 7 miles
Service Ceiling
500 miles
805 km | 435 nm
Operational Range
5,530 ft/min
1,686 m/min
Rate-of-Climb