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August 2002
- Concorde: We Fly Aboard at Mach 2!
- SST! Evolution of the Supersonic Transport
- Silverplate B-29s: World’s First Atomic Bombers
Manuals & Photos
- Concorde Flying Manual, Volume I, 1976
- Concorde Flying Manual, Volume IIa, 1979
- Concorde Flying Manual, Volume IIb, 1979
- Concorde Memento Air France
- Concorde Performance Manual, Part 1, 1996
- British Airways Concorde Brochure, 1996
- British Airways Concorde Safety Card
- Over 330 Concorde Photos
Aérospatiale/BAC Concorde
Specifications
On Display
Cutaway
Videos
General Characteristics

- Crew: 3 (2 pilots and 1 flight engineer)
- Capacity: 92–120 passengers
(128 in high-density layout) - 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: 3,856.2 sq ft (358.25 m2)
- Empty weight: 173,504 lb (78,700 kg)
- Gross weight: 245,000 lb (111,130 kg)
- Max takeoff weight: 408,010 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) internal
- Fuselage height: maximum of 10 ft 10 in (3.30 m) external, 6 ft 5 in (1.96 m) internal
- Maximum taxiing weight: 412,000 lb (187,000 kg)
- Powerplant: 4 × Rolls-Royce/Snecma Olympus 593 Mk 610 turbojets with reheat, 31,000 lbf (140 kN) thrust each dry, 38,050 lbf (169.3 kN) with afterburner
Performance
- Maximum speed: 1,354 mph (2,179 km/h, 1,177 kn)
- Maximum speed: Mach 2.04 (temperature limited)
- Cruise speed: 1,341 mph (2,158 km/h, 1,165 kn)
- Range: 4,488.0 mi (7,222.8 km, 3,900.0 nmi)
- Service ceiling: 60,000 ft (18,300 m)
- Rate of climb: 3,300–4,900 ft/min (17–25 m/s) at sea level
- 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– 7.14
- Fuel consumption: 47 lb/mi (13.2 kg/km)
- Thrust/weight: 0.373
- Maximum nose tip temperature: 127 °C (260 °F; 400 K)
- Runway requirement (with maximum load): 3,600 m (11,800 ft)
Avionics
- Digital Air Intake Control Units
- Fly by wire flight controls
- Analogue electronic engine controls
- Triple inertial navigation units, one per flight crew
- Dual VHF omnidirectional range instruments
- Dual automatic direction finder instruments
- Dual distance measuring equipment instruments
- Dual instrument landing systems
- Automatic flight control system with dual autopilots, autothrottles, and flight directors: full autoland capability with visibility limits 250 m (820 ft) horizontally, 15 ft (4.6 m) decision height
- Ekco E390/564 weather radar
- Radio altimeters
| Registration | Livery | Location |
|---|---|---|
| G-AXDN | British Airways | Cambridge, England |
| G-BBDG | British Airways | Surrey, England |
| G-BOAA | British Airways | North Berwick, Scotland |
| G-BOAB | British Airways | Heathrow, England |
| G-BOAC | British Airways | Manchester, England |
| G-BOAD | British Airways | New York, USA |
| G-BOAE | British Airways | Charnocks, Barbados |
| G-BOAF | British Airways | Filton, England |
| G-BOAG | British Airways | Seattle, USA |
| G-BSST | British Aircraft Corporation | Yeovilton, England |
| F-BTSD | Air France | Le Bourget, France |
| F-BVFA | Air France | Dulles, Virginia, USA |
| F-BVFB | Air France | Sinsheim, Germany |
| F-BVFC | Air France | Blagnac, France |
| F-BVFF | Air France | Roissy-en-France, France |
| F-WTSA | Air France | Athis-Mons, France |
| F-WTSB | Air France | Blagnac, France |













