X-31 Enhanced Fighter Maneuverability Demonstrator
| Specifications | |
|---|---|
| Contractors | Rockwell Aerospace, North American Aircraft and Deutsche Aerospace |
| Crew | single seat |
| wing span | 23.83 feet (7.3 m) |
| fuselage length | 43.33 feet (1 2.8 m) |
| Engine | single General Electric P404-GE-400 turbofan engine 16,000 pounds (71,168 N) thrust in afterburner |
| takeoff weight | 16,100 pounds (7,303 kg) |
| speed | up to Mach 1.28 at 35,000 feet |
| altitude | 40,000 feet (12,200 m) |
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