Specifications of Concorde

General characteristics

public domain by  Arpingstone

Concorde G-BOAB in storage at London (Heathrow) Airport

• Crew: 9
• Capacity: 100 passengers
• Length: 202 ft 4 in^[5] (61.66 m)
• Wingspan: 84 ft 0 in (25.6 m)
• Height: 40 ft 0 in (12.2 m )
• Fuselage internal length: 129 ft 0 in (39.32 m)
• Fuselage max external width: 9 ft 5 in (2.88 m)
• Fuselage max internal width: 8 ft 7 in (2.63 m)
• Fuselage max external height: 10 ft 10 in (3.32 m)
• Fuselage max internal height: 6 ft 5 in (1.96 m)
• Wing area: 3,856 ft² (358.25 m² )
• Lift/drag ratio: Low speed- 3.94, Approach- 4.35, 250 knots, 10,000 ft- 9.27, Mach 0.94- 11.47, Mach 2.04- 7.14)
• Elevon area (each): 172.22 ft² (16.0 m²)
• Tail fin area: 365.0 ft² (33.91 m²)
• Rudder area: 112.05 ft² (10.41 m²))
• Empty weight: 173,500 lb (78,700 kg)
• Useful load: 245,000 lb (111,130 kg)
• Max takeoff weight: 408,000 lb (185,070 kg)
• Maximum fuel load: 210,940 lb (95,680 kg )
• Maximum taxiing weight: 412,000 lb (186,880 kg)
• Powerplant: 4× Rolls-Royce/SNECMA Olympus 593 Mk 610 afterburning turbojets
  • Dry thrust: 32,000 lbf dry (140 kN) each
  • Thrust with afterburner: 38,050 lbf (169 kN) each

Performance

• Maximum speed: Mach 2.04 (1,350 mph, 2,170 km/h)
• Range: 3,900 nm (4,500 mi, 7,250 km)
• Service ceiling: 60,000 ft (18,300 m)
• Rate of climb: 1,525 m (5,000 ft)/min (25,41 m/s)
• Wing loading: lb/ft² (kg/m²)
• Thrust/weight: .373
• Fuel consumption: 46.85 lb/mi (13.2 kg/km)
• Maximum nose tip temperature: 260 °F (127 °C)