Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the North American X-10 Unmanned Cruise Missile Technology Demonstrator Aircraft.
2 x Westinghouse XJ40-WE-1 turbojet engines developing 10,900 lb of thrust each.
Propulsion
1,299 mph
2,090 kph | 1,129 kts
Max Speed
45,013 ft
13,720 m | 9 miles
Service Ceiling
818 miles
1,316 km | 711 nm
Operational Range
5,224 ft/min
1,592 m/min
Rate-of-Climb
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).