The Northrop/McDonnell Douglas YF-23 is an American single-seat, twin-engine stealth fighter aircraft technology demonstrator designed for the United States Air Force (USAF). The design was a finalist in the USAF's Advanced Tactical Fighter (ATF) competition, battling the Lockheed YF-22 for a production contract. Two YF-23 prototype air vehicles were built.
Payload
GAU-12
Aim-9 Sidewinder
Aim-7F
Specifications
General Characteristics
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- Wingspan 29.3ft (8.9m)
- Length 39.0ft (11.9m)
- Height 8.8ft (2.7m)
- Empty Weight N/A
- Loaded Weight 12,443lbs (5,644kg)
Performance
- Power/Weight Ratio 5.417
- Wing Loading 33.2lbs/ft2 (162.0kg/m2)
- Wing Area 375.0ft2 (34.8m2)
- Drag Points 3660
Parts
- Number of Parts 55
- Control Surfaces 5
- Performance Cost 353
