General characteristics of actual aircraft, Crew: 3 (2 pilots and 1 flight engineer)Capacity: 92–120 passengers (128 in high-density layout)[N 9]Length: 202 ft 4 in (61.66 m)Wingspan: 84 ft 0 in (25.6 m)Height: 40 ft 0 in (12.2 m)Wing area: 3,856 sq ft (358.25 m2)Empty weight: 173,500 lb (78,700 kg)Gross weight: 245,000 lb (111,130 kg)Max takeoff weight: 408,000 lb (185,070 kg)Fuel capacity: 210,940 lb (95,680 kg)Fuselage internal length: 129 ft 0 in (39.32 m)Fuselage width: maximum of 9 ft 5 in (2.87 m) external 8 ft 7 in (2.62 m) internalFuselage height: maximum of 10 ft 10 in (3.30 m) external 6 ft 5 in (1.96 m) internalMaximum taxiing weight: 412,000 lb (187,000 kg)Powerplant: 4 × Rolls-Royce/Snecma Olympus 593 Mk 610 Afterburning turbojets, 32,000 lbf (140 kN) thrust each dry, 38,050 lbf (169.3 kN) with afterburnerPerformanceMaximum speed: 1,354 mph (2,179 km/h, 1,176 kn)Maximum speed: Mach 2.04Cruise speed: 1,340 mph (2,158 km/h, 1,164 kn)Range: 4,488.04 mi (7,222.8 km, 3,900 nmi)Service ceiling: 60,000 ft (18,300 m)Rate of climb: 3,500–5,000 ft/min (17–25 m/s) at sea level[325][326]Lift-to-drag: Low speed– 3.94, Approach– 4.35, 250 kn, 10,000 ft– 9.27, Mach 0.94– 11.47, Mach 2.04– 7.14Fuel consumption: 46.85 lb/mi (13.2 kg/km)Thrust/weight: 0.373Maximum nose tip temperature: 260 °F (130 °C)Runway requirement (with maximum load): 3,600 m (11,800 ft)[327]