F-233B
A fighter developed by a country. Development began in 1979, with successful test flights in 1986 and service in 1991. The aircraft was originally designed to replace the F-233A fighter, which has been in service for more than 30 years and has lagged behind in comprehensive performance, and was named the F-233B fighter. It is a single-engine, single-seat, high-mobility, multifunctional fighter designed by a country for its naval aviation. The aircraft can perform air-to-air, air-to-ground, and air-to-sea attack missions. It can also be used as a naval carrier-based aircraft and can even throw nuclear bombs. The maximum attack radius is 1100 km. This aircraft has attack aircraft, advanced trainer aircraft, fighter bomber and other modifications.
Specifications
General Characteristics
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- Wingspan 34.2ft (10.4m)
- Length 42.6ft (13.0m)
- Height 14.9ft (4.5m)
- Empty Weight 9,115lbs (4,134kg)
- Loaded Weight 19,193lbs (8,705kg)
Performance
- Power/Weight Ratio 1.756
- Wing Loading 56.3lbs/ft2 (274.7kg/m2)
- Wing Area 341.1ft2 (31.7m2)
- Drag Points 2730
Parts
- Number of Parts 75
- Control Surfaces 3
- Performance Cost 475