Years of Production:
1961 / 1972
Number produced:
1,100 +
Crew:
2 x Instructor / Student
Engines: 2 x General Electric J85-5A (J855R after PMP modification) Afterburning Turbojets Thrust
Dry: 2,050 lbf (9.1 kN) per engine
Afterburner: 2,900 lbf (17.1 kN) per engine
Maximum speed: Mach 1.3 (858 mph / 1,381 km/h)
Range: 1,140 mi (1,835 km)
Rate of climb: 33,600 ft/min (170.7 m/s)
Ceiling: 50,000 ft (15,240 m)
Range: 745 mi (1,200 km)
Wingspan:
25 ft 3 in (7.7 m)
Length: 46 ft 4.5 in (14.14 m)
Height: 12 ft 10.5 in (3.92 m)
Empty weight: 7,200 lb (3,270 kg)
Loaded: 11,820 lb (5,360 kg)
Maximum take-off: 12,093 lb (5,485 kg)