Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the McDonnell Model 90 Carrierborne Supersonic Fighter Proposal.
1 x Pratt & Whitney J57 afterburning turbojet engine developing 10,200lb thrust dry and 16,000lb of thrust with reheat.
Propulsion
1,056 mph
1,700 kph | 918 kts
Max Speed
59,055 ft
18,000 m | 11 miles
Service Ceiling
544 miles
875 km | 472 nm
Operational Range
35,000 ft/min
10,668 m/min
Rate-of-Climb