L-133
The Lockheed L-133 was an exotic design started in 1939 which was proposed to be the first jet fighter of the United States Army Air Forces (USAAF) during World War II. The radical design was to be powered by two axial-flow turbojets with an unusual blended wing-body canard design capable of 612 mph (985 km/h) in level flight. The USAAF passed on the 1942 proposal, but the effort speeded the development of the USAAF's first successful operational jet fighter, the P-80 Shooting Star which did see limited service near the end of war. The P-80 was a less radical design with a single British-based Allison J33 engine, with a conventional tail, but it retained a wing which was the same shape as the outer wing sections of the P-38 Lightning.
Specifications
General Characteristics
- Successors 1 airplane(s)
- Created On iOS
- Wingspan 42.4ft (12.9m)
- Length 36.4ft (11.1m)
- Height 11.6ft (3.5m)
- Empty Weight 6,106lbs (2,770kg)
- Loaded Weight 10,753lbs (4,877kg)
Performance
- Power/Weight Ratio 2.089
- Wing Loading 25.3lbs/ft2 (123.4kg/m2)
- Wing Area 425.4ft2 (39.5m2)
- Drag Points 1820
Parts
- Number of Parts 33
- Control Surfaces 5
- Performance Cost 206