Powerplant:
Model: Pratt & Whitney J57-P-25
Type: Afterburning turbojet
Number: One
Dry Thrust: 11,700 lb.
With Afterburner: 17,200 lb.
Dimensions:
Length: 68 ft 4 in (20.83 m)
Wingspan: 38 ft 1 in (11.61 m)
Height: 21 ft 2 in (6.45 m)
Wing area: 695 ft² (64.57 m²)
Airfoil: NACA 0004-65 mod root and tip
Internal Fuel: 1,085 US gal (4,107 l)
Weights:
Empty: 19,350 lb (8,777 kg)
Loaded: 24,500 lb (11,100 kg)
Max takeoff: 31,500 lb (14,300 kg)
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Performance:
Maximum speed:
– 825 mph (1,304 kph) @ 40,000 ft
Cruise Speed: N/A
Range: 1,350 mi (2,175 km)
Service ceiling: 53,400 ft (16,300 m)
Rate of climb: 13,000 ft/min (66 m/s)
Wing loading: 35 lb/ft² (172 kg/m²)
Thrust/weight: 0.70
Armament
Rockets:
24× 2.75 in (70 mm) unguided rockets in missile bay doors
Missiles:
– 6× AIM-4 Falcon air-to-air missiles or
– 3× AIM-4 Falcon
– 1× AIM-26 Falcon with conventional
or nuclear warhead
Avionics
– MG-10 fire control system
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