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The French-built prototype Concorde 001 flew on March 2, 1969 and the British-made Concorde 002 flew on April 9, 1969.
Both prototypes entered service in 1971. Commercial service began in 1976 but only 9 aircraft were ordered.
| CREW | 3-4 |
| PASSENGERS | 144 |
| ENGINE | 4 x Rolls-Royce/SNECMA Olympus 593 Mk 610, 169.1kN |
| WEIGHTS |
| Take-off weight | 185066 kg | 408003 lb |
| Empty weight | 78698 kg | 173500 lb |
| DIMENSIONS |
| Wingspan | 25.55 m | 83 ft 10 in |
| Length | 62.10 m | 203 ft 9 in |
| Height | 11.40 m | 37 ft 5 in |
| Wing area | 358.22 m2 | 3855.84 sq ft |
| PERFORMANCE |
| Cruise speed | 2179 km/h | 1354 mph |
| Ceiling | 18290 m | 60000 ft |
| Range | 6582 km | 4090 miles |
 | A three-view drawing (1190 x 668) |
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