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Historical

Concorde

The supersonic airliner that crossed the Atlantic in 3.5 hours — and retired to silence.

Mach 2.04 Cruise Speed 2,179 km/h at 18,000 m
Concorde
01 — Overview

History & background.

Concorde was the only supersonic commercial airliner to enter regular passenger service and sustain it for decades. Jointly developed by British Aerospace and Aérospatiale, it flew its first commercial flights simultaneously from London and Paris on January 21, 1976, and operated without interruption for 27 years. In its prime, Concorde crossed the North Atlantic in under 3.5 hours — a journey that took subsonic jets nearly twice as long.

At its official cruise speed of Mach 2.04 (2,179 km/h) and cruising altitude of 18,000 metres (59,000 feet), Concorde flew in the stratosphere where the thin atmosphere reduced drag sufficiently to sustain supersonic flight on its four Rolls-Royce/SNECMA Olympus 593 afterburning turbojets. Aerodynamic friction heated the nose to +127°C, expanding the aluminium airframe by approximately 30 cm in flight. The iconic drooped nose — which lowered 12.5° for takeoff and landing to give the pilots a forward view over the long ogival delta wing — became the aircraft’s defining visual feature.

Concorde Variants and Production

Twenty Concorde airframes were built in total. Two prototype aircraft (001 and 002), two pre-production airframes (01 and 02), and sixteen production aircraft were constructed between 1965 and 1979. Of the production aircraft, fourteen entered passenger service: seven with British Airways (Series 100, designated 102) and seven with Air France (Series 100, designated 101). All service aircraft shared an identical performance specification: Mach 2.04 cruise, 18,300 m service ceiling, 7,250 km range, and seating for exactly 100 passengers in a single business class. The two unsold production aircraft were ultimately donated to museums.

The Crash and Retirement

On July 25, 2000, Air France Flight 4590 crashed on takeoff from Paris Charles de Gaulle, killing all 109 people on board and 4 on the ground. The cause was a titanium strip on the runway that punctured a tyre, sending debris into a fuel tank and igniting a catastrophic fire. The Concorde fleet was grounded, returned to service in November 2001 with enhanced tyre and fuel tank protection, but the combined effect of reduced post-9/11 business travel and Airbus withdrawing technical support made continued operation uneconomical. Both British Airways and Air France retired their fleets simultaneously in October 2003.

Concorde’s cultural legacy far exceeded its commercial footprint. For a generation it represented the pinnacle of technological ambition in civil aviation. No supersonic passenger aircraft entered scheduled service in the two decades that followed its retirement.

02 — Technical Data

Specifications & performance.

cruise speedMach 2.04 (2,179 km/h) at altitude
engine4× Rolls-Royce/SNECMA Olympus 593 (169.3 kN each with reheat)
first flightMarch 2, 1969
length61.66 m (expands 30 cm in flight)
max speedMach 2.23 (never-exceed)
mtow187,700 kg
range7,250 km (transatlantic)
seating100 passengers (standard)
service ceiling18,300 m (60,040 ft)
statusRetired (2003); 20 airframes preserved worldwide
wingspan25.61 m (ogival delta)
03 — Gallery

In the Aviation Guide app.

Concorde three-view schematic
Droop nose mechanism
Engine detail
04 — Questions

Frequently asked about Concorde.

How fast did Concorde fly?+
Concorde cruised at Mach 2.04 (2,179 km/h / 1,354 mph) at an altitude of 18,000 m (59,000 ft), allowing it to cross the North Atlantic in approximately 3 hours 30 minutes. Its never-exceed speed was Mach 2.23.
Why did Concorde retire?+
Concorde retired in 2003 following several factors: the July 2000 crash of Air France Flight 4590 near Paris (killing 113 people), the post-9/11 decline in luxury travel, increasing maintenance costs, and Airbus's decision to withdraw technical support. British Airways and Air France both retired their fleets simultaneously in October 2003.
Why did the Concorde nose droop?+
Concorde's distinctive drooping nose was necessary because the aircraft's long, slender delta-wing design created a very high pitch attitude during approach and landing, blocking the pilots' forward view. The nose lowered to 12.5° for takeoff and landing, and raised to a streamlined position for supersonic cruise.

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