Concorde
General characteristics
* Crew: 3 (pilot, co -pilot and flight engineer)[77]
* Capacity: 92-120 passengers (128 in high-density layout[78]). BA and AF Concordes had 100 seats. with AF removing a small number of seats after the safety modifications of CY2000-2001 due to weight considerations.
* Length: 202 ft 4 in[79] (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 ft� (358.25 m�)
* Empty weight: 173,500 lb (78,700 kg)
* Useful load: 245,000 lb (111,130 kg)
* Powerplant: 4� Rolls-Royce/SNECMA Olympus 593 Mk 610 afterburning turbojets
o Dry thrust: 32,000 lbf (140 kN) each
o Thrust with afterburner: 38,050 lbf (169 kN) each
* Maximum fuel load: 210,940 lb (95,680 kg)
* Maximum taxiing weight: 412,000 lb (186,880 kg)
Performance
* Maximum speed: Mach 2.2[80] (~1,450 mph, 2,330 km/h[80])
* Cruise speed: Mach 2.02 (~1,320 mph)
* Range: 3,900 nmi (4,500 mi, 7,250 km)
* Service ceiling 60,000 ft (18,300 m)
* Rate of climb: 5,000 ft/min. (25.41 m/s)
* Thrust/weight: 0.373
* Lift/drag ratio: Low speed- 3.94, Approach- 4.35, 250 kn, 10,000 ft- 9.27, Mach 0.94- 11.47, Mach 2.04- 7.14
* Fuel consumption for max. range (max. fuel/max. range): 46.85 lb/mi (13.2 kg/km)
* Maximum nose tip temperature: 260 �F (127 �C)
Gallery:
cockpit and cabin
Speed display
Source:
CODE
http://en.wikipedia.org/wiki/Concorde
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