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Aerospatiale / BAC Concorde

Aerospatiale / BAC Concorde G-BOAA © Mike Vallentin
Photo ©: Mike Vallentin

Concorde

Super-Sonic Airliner

The Aerospatiale / BAC Concorde is a four-engine supersonic airliner with a capacity of maximum 128 passengers. The Concorde was jointly developed by Aerospatiale (France) and British Aircraft Corporation (United Kingdom).

Crew3
Passengers92-120 / 128
 
Propulsion4 Turbojat Engines
Engine ModelRolls-Royce/SNECMA Olympus 593
Engine Power (each)
dry/with Afterburner
140 / 169 kN31473 / 37992 lbf
 
max. Cruise Speed2006 km/h1083 kts
  1246 mph
max. Speed (vne)2330 km/h1258 kts
  1448 mph
Mmo (max. Mach)Mach 2.2
Service Ceiling18.288 m60.000 ft
Rate of climb1524 m/min5000 ft/min
Range7.251 km3.915 NM
4.505 mi.
 
Empty Weight78.690 kg173.482 lbs
max. Takeoff Weight185.066 kg408.000 lbs
 
Wing Span25,55 m83,8 ft
Wing Area358,2 m²3856 ft²
Length62,10 m203,7 ft
Height11,40 m37,4 ft
 
First Flight02.03.1969 (F-WTSS)
Production Statusout of production
Total Production20
 
IATA CodeSSC
FAA TCDSA45EU
Data for (Version)Aérospatiale-BAC Concorde

Remarks
The Concorde was the world's second supersonic airliner after the Tupolev Tu-144. The first flight was two month after the Tu-144. The Concore was only operated by Air France and British Airways only.


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