Time Period: Post-WW2
Country of Origin: United States
Type: Prototypes and Experimental
Manufacturer: Douglas Aircraft Company
Douglas X-3 Stiletto Aircraft Overview
The Douglas X-3 Stiletto was an experimental aircraft developed by the Douglas Aircraft Company in the 1950s for the United States Air Force. The X-3 was designed to test advanced aerodynamic concepts and technologies, including supersonic flight and swept-wing configurations.
The X-3 was a sleek, jet-powered aircraft with a distinctive, needle-like fuselage and thin, straight wings. It was powered by two Westinghouse J34 turbojet engines, which gave it a top speed of Mach 1.2. The aircraft was also equipped with a variety of experimental sensors and instruments, including a nose-mounted camera for recording flight data.
Despite its advanced design and technology, the X-3 suffered from a number of technical problems during its development and testing. Its straight wings proved to be less efficient at high speeds than the swept-wing configurations that would become standard on supersonic aircraft. The aircraft also had a relatively short service life, flying only a few test flights before being retired from active service.
Despite its limited success, the X-3 Stiletto contributed valuable data to the development of supersonic aircraft and advanced aerodynamic concepts.
Douglas X-3 Stiletto Specifications
- Crew: 1
- Length: 66 ft 9 in (20.35 m)
- Wingspan: 22 ft 8 in (6.91 m)
- Height: 12 ft 6 in (3.82 m)
- Wing area: 166.5 sq ft (15.47 m2)
- Aspect ratio: 3
- Empty weight: 14,345 lb (6,507 kg)
- Gross weight: 20,800 lb (9,435 kg)
- Max takeoff weight: 22,400 lb (10,160 kg)
- Powerplant: 2 × Westinghouse XJ34-WE-17 afterburning turbojets, 3,370 lbf (15.0 kN) thrust each dry, 4,900 lbf (22 kN) with afterburner
Douglas X-3 Stiletto Performance
- Maximum speed: 613.5 kn (706.0 mph, 1,136.2 km/h) at 20,000 ft (6,100 m)
- Maximum speed: Mach 0.987
- Range: 432 nmi (497 mi, 800 km)
- Endurance: 1 hour at 512.7 kn (590.0 mph; 949.5 km/h)at 30,000 ft (9,100 m)
- Service ceiling: 38,000 ft (12,000 m) absolute
- Rate of climb: 19,000 ft/min (97 m/s)
- Wing loading: 124.9 lb/sq ft (610 kg/m2)
- Thrust/weight: 0.476