Primary Function: A-10 -- close air support, OA-10 - airborne forward air control
Contractor: Fairchild Republic Co.
Power Plant: Two General Electric TF34-GE-100 turbofans
Thrust: 9,065 pounds each engine
Length: 53 feet, 4 inches (16.16 meters)
Height: 14 feet, 8 inches (4.42 meters)
Wingspan: 57 feet, 6 inches (17.42 meters)
Speed: 420 miles per hour (Mach 0.56)
Ceiling: 45,000 feet (13,636 meters)
Maximum Takeoff Weight: 51,000 pounds (22,950 kilograms)
Range: 800 miles (695 nautical miles)
Me262
Engine: Two 900 kg (1,986 lb) thrust Junkers Jumo 004 B axial flow Turbojets
Wing Span: 12.5 m (41 ft 1 in)
Length: 10.58 m (34 ft 8.5 in)
Height: 3.83 m (12 ft 6.75 in)
Weight: Empty 4,000 kg (8,820 lb)
Loaded 7,045 kg (14,938 lb)
Maximum Speed: A-1a: 870 km/h at 6,000 m (540 mph at 19,685 ft)
A-2a: 755 km/h (470 mph)
B-1a: 800 km/h (497 mph)
Ceiling: 11,450 m (37,664 ft)
Range: 1,050 km (650 miles)
Climb Rate: 1,200 m/min (3,937 ft/min)
Accommodation: 1 Pilot
Armament: A-1a: Four 30 mm MK108 cannons in nose, two with 100 rounds each, two with 80; could also carry 24 R4M 55 mm unguided rockets on underwing racks.
A-2a: As A-1a but with two additional 250 kg (551 lb) bombs on racks under nose.
B-1a: As A-1a
B-2a: As A-1a plus two inclined MK 108 behind the cockpit.
Me262 is much faster than the A-10. With equal pilots, the Me262 would murder the A-10.