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This short wingspan produced little lift at low speed, resulting in long take-off ... Although computer ... 37 years after its first test flight, Concorde was ...
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 ...
In a pre-computer age, flight engineers were crucial to aviation. Former Concorde flight engineer Warren Hazelby explains how he helped fly the supersonic jet.
(203) was the Concorde lost in the crash of Air France Flight 4590 on 25 July 2000 in the small town of Gonesse, France near Le Bourget, located just outside Paris, killing 113 people. The remains of this aircraft are stored at a hangar at Le Bourget Airport. It is the only Concorde in the history of the design to be destroyed in a crash.
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Its inaugural flight — 60 years ago in September 1964 — kicked off a golden era for supersonic aircraft. The plane would later achieve a speed of just over 2,000 miles per hour, nearly 50% ...
Afterburning was added to Concorde for take-off to cope with weight increases that came after the initial design. It was also used to accelerate through the high-drag transonic speed range, not because the extra thrust was required, but because it was available and improved the operating economics. The redesigned Tu-144D used engines with no ...
The Fairey Delta 2 high-speed experimental aircraft, which had a droop nose that included its cockpit. The droop nose is a feature fitted to a small number of aircraft types so the nose of the aircraft can be lowered during takeoff and landing to improve the pilot's view of the ground below.