Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Armstrong Whitworth AW.52 Experimental Flying Wing Aircraft.
2 x Rolls-Royce Nene turbojet engines developing 5,000lb of thrust each.
Propulsion
500 mph
805 kph | 435 kts
Max Speed
36,007 ft
10,975 m | 7 miles
Service Ceiling
1,501 miles
2,415 km | 1,304 nm
Operational Range
4,800 ft/min
1,463 m/min
Rate-of-Climb