Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Curtiss Proposal II Research Aircraft.
2 x Wright ramjet engines developing 6,000 lb of thrust; 1 x Curtiss auxiliary rocket developing 4,000 lb of additional thrust (for acceleration).
Propulsion
976 mph
1,570 kph | 848 kts
Max Speed
50,000 ft
15,240 m | 9 miles
Service Ceiling