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Aérospatiale-BAC Concorde supersonic transport (SST), along with the Tupolev Tu-144, was one of only two models of supersonic passenger airliners to have seen commercial service.

Concorde had a cruise speed of Mach 2.02 (around 2170 km/h or 1,350 mph) and a maximum cruise altitude of 60,000 feet (18 300 metres) with a delta wing configuration and a reheat-equipped evolution of the engines originally developed for the Avro Vulcan strategic bomber. The engines were built by Rolls-Royce. Concorde was the first civil airliner to be equipped with an analogue fly-by-wire flight control system. Commercial flights, operated by British Airways and Air France, began on January 21, 1976 and ended on October 24, 2003, with the last "retirement" flight on November 26 that year.

Construction of the first two prototypes began in February 1965. Concorde 001 was built by Aerospatiale at Toulouse and Concorde 002 by BAC at Filton, Bristol. Concorde 001 took off for the first test flight from Toulouse on March 2, 1969 and the first supersonic flight followed on October 1. As the flight programme of the first development aircraft progressed, 001 started off on a sales and demonstration tour beginning on September 4, 1971. Concorde 002 followed suit on June 2, 1972 with a sales tour of the Middle and Far East. Concorde 002 made the first visit to the United States in 1973, landing at the new Dallas/Fort Worth International Airport to commemorate its opening.

Span: 84 ft 0 in (25.6 m).
Length: 202 ft 4 in[2] (61.66 m)
Height: 40 ft 0 in (12.2 m )
Engines: 4× Rolls-Royce/SNECMA Olympus 593 Mk 610 afterburning turbojets 170 kN each.
Cruising Speed: Mach 2.04 (1,350 mph, 2,170 km/h)
First Flight: March 2, 1969
Number built: 20 (including prototypes)