Powerplant:
Model: Pratt & Whitney J57-P-55
Type: After-burning Turbojet
Number: Two
Dry Thrust: 11,990 lb
W. Afterburner: 16,900 lb
Fuel:
Internal Capacity: 2,053 US gal (7,771 L)
Capacity with 2 external tanks:
– 2,953 US gal (11,178 L)
Dimensions:
Length: 67 ft 5 in (20.55 m)
Wingspan: 39 ft 8 in (12.09 m)
Height: 18 ft 0 in (5.49 m)
Wing area: 368 ft² (34.20 m²)
Airfoil:
NACA 65A007 mod root
NACA 65A006 mod tip
Wing loading: 124 lb/ft² (607 kg/m²)
Thrust/weight: 0.74
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Weights:
Empty: 28,495 lb (12,925 kg)
Loaded: 45,665 lb (20,715 kg)
Max takeoff: 52,400 lb (23,770 kg)
Performance:
Maximum speed:
– 1,134 mph (1,825 kph) at 35,000 ft
Range: 1,520 mi (2,450 km)
Service ceiling: 58,400 ft (17,800 m)
Rate of climb: 49,200 ft/min (250 m/s)
Bombload:
– Four missiles
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