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Lockheed A-10 Thunderbolt II
[ United States Air Force
]
| Specifications | |
|---|---|
| Primary Function: | Close Air Support |
| Manufacturer: | Fairchild Republic Co. (Now Lockheed) |
| Crew: | One |
| Power Plant: | Two General Electric TF34-GE-100 turbofans |
| Max Speed: | 420 miles per hour (Mach 0.56) |
| Thrust: | 9,065 pounds each engine |
| Length: | 53 feet, 4 inches (16.16 metres) |
| Height: | 14 feet, 8 inches (4.42 metres) |
| Wingspan: | 57 feet, 6 inches (17.42 metres) |
| Ceiling: | 45,000 feet (13,636 metres) |
| Maximum Takeoff Weight: | 51,000 pounds (22,950 kilograms) |
| Range: | 800 miles (695 nautical miles) |
| Armament: | One 30 mm GAU-8/A seven-barrel Gatling gun;
Up to 16,000 pounds (7,200 kilograms) of mixed ordnance on eight under-wing and three under-fuselage pylon stations, including: 500 pounds (225 kilograms) of Mk-82 and 2,000 pounds (900 kilograms) of Mk-84 series low/high drag bombs, Combined effects munitions, Mine dispensing munitions, AGM-65 Maverick missiles and laser-guided/electro-optically guided bombs; Infrared countermeasure flares; Electronic countermeasure chaff; Jammer pods; 2.75-inch (6.99 centimeters) rockets; Illumination flares and, AIM-9 Sidewinder missiles. |
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