Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Armstrong Whitworth AW.169 High-Altitude Mach 2 Interceptor Proposal.
4 x de Havilland Gyron Junior PS.53 turbojet engines (wing-mounted); 1 x Spectre rocket (fuselage-mounted); Up to 15,000lb of combined thrust output.
Propulsion
1,553 mph
2,500 kph | 1,350 kts
Max Speed
60,039 ft
18,300 m | 11 miles
Service Ceiling
55,000 ft/min
16,764 m/min
Rate-of-Climb