Douglas X-3 Stiletto
The Douglas X-3 Stiletto was a 1950s United States experimental jet aircraft with a slender fuselage and a long tapered nose, manufactured by the Douglas Aircraft Company. Its primary mission was to investigate the design features of an aircraft suitable for sustained supersonic speeds, which included the first use of titanium in major airframe components. Douglas designed the X-3 with the goal of a maximum speed of approximately 2,000 m.p.h,[2] but it was, however, seriously underpowered for this purpose and could not even exceed Mach 1 in level flight.[3] Although the research aircraft was a disappointment, Lockheed designers used data from the X-3 tests for the Lockheed F-104 Starfighter which used a similar trapezoidal wing design in a successful Mach number 2 fighter.
Specifications
General Characteristics
- Created On Mac
- Wingspan 26.0ft (7.9m)
- Length 41.6ft (12.7m)
- Height 13.3ft (4.0m)
- Empty Weight 10,284lbs (4,664kg)
- Loaded Weight 15,235lbs (6,910kg)
Performance
- Power/Weight Ratio 4.425
- Wing Loading 104.4lbs/ft2 (509.5kg/m2)
- Wing Area 146.0ft2 (13.6m2)
- Drag Points 2705
Parts
- Number of Parts 49
- Control Surfaces 5
- Performance Cost 342