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Concorde pilots were routinely trained to handle double-engine failure. [103] Concorde used reheat (afterburners) only at take-off and to pass through the transonic speed range, between Mach 0.95 and 1.7. [104]
Partial reheat providing a 20% thrust increase [3] was installed to give the take-off thrust required for Concorde to operate from existing runways, and for transonic acceleration from Mach 0.95 up to Mach 1.7; the aircraft flew supersonically without reheat above that speed. At cruise the engine's direct contribution (transferred by its mounts ...
The official handover ceremony of British Airways' first Concorde occurred on 15 January 1976 at Heathrow Airport. Air France Concorde (F-BTSC) at Charles de Gaulle Airport on 25 July 1975, exactly 25 years before the accident in 2000 British Airways Concorde in Singapore Airlines livery at Heathrow Airport in 1979 Air France Concorde (F-BTSD) with a short-lived promotional Pepsi livery in ...
Former Concorde flight engineer Warren Hazelby explains how he helped fly the supersonic jet. In a pre-computer age, flight engineers were crucial to aviation. Former Concorde flight engineer ...
Five years before Concorde’s first flight, ... The plane would later achieve a speed of just over 2,000 miles per hour, nearly 50% faster than Concorde.
For example, Concorde had very high drag (a lift to drag ratio of about 4) at slow speed, but it travelled at high speed for most of the flight. Designers of Concorde spent 5000 hours optimizing the vehicle shape in wind tunnel tests to maximize the overall performance over the entire flightplan.
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Concorde was originally designed for cruising speeds up to Mach 2.2, [55] but its regular service speed was limited to Mach 2.02 to extend airframe life. [56] One of Tupolev's web site pages states that "TU-144 and TU-160 aircraft operation has demonstrated expediency of limitation of cruise supersonic speed of M=2.0 to provide structure ...