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Concorde 002 First Flight, April 1969
nella discussione ha aggiunto Autodelta85 in Altri Mezzi di Trasporto
General characteristics * Crew: 9 * Capacity: 100 passengers * Length: 202 ft 4 in[15] (61.66 m) * Wingspan: 84 ft 0 in (25.6 m) * Height: 40 ft 0 in (12.2 m ) * Fuselage internal length: 129 ft 0 in (39.32 m) * Fuselage max external width: 9 ft 5 in (2.88 m) * Fuselage max internal width: 8 ft 7 in (2.63 m) * Fuselage max external height: 10 ft 10 in (3.32 m) * Fuselage max internal height: 6 ft 5 in (1.96 m) * Wing area: 3,856 ft² (358.25 m² ) * Lift/drag ratio: Low speed- 3.94, Approach- 4.35, 250 knots, 10,000 ft- 9.27, Mach 0.94- 11.47, Mach 2.04- 7.14) * Elevon area (each): 172.22 ft² (16.0 m²) * Tail fin area: 365.0 ft² (33.91 m²) * Rudder area: 112.05 ft² (10.41 m²)) * Empty weight: 173,500 lb (78,700 kg) * Useful load: 245,000 lb (111,130 kg) * Max takeoff weight: 408,000 lb (185,070 kg) * Maximum fuel load: 210,940 lb (95,680 kg ) * Maximum taxiing weight: 412,000 lb (186,880 kg) * Powerplant: 4× Rolls-Royce/SNECMA Olympus 593 Mk 610 afterburning turbojets o Dry thrust: 32,000 lbf dry (140 kN) each o Thrust with afterburner: 38,050 lbf (169 kN) each Performance * Maximum speed: Mach 2.04 (1,350 mph, 2,170 km/h) * Range: 3,900 nm (4,500 mi, 7,250 km) * Service ceiling: 60,000 ft (18,300 m) * Rate of climb: 1,525 m (5,000 ft)/min (25,41 m/s) * Wing loading: lb/ft² (kg/m²) * Thrust/weight: .373 * Fuel consumption: 46.85 lb/mi (13.2 kg/km) * Maximum nose tip temperature: 260 °F (127 °C) Un aereo allucinante,totalmente antieconomico..ma era l'aereo del futuro...come negli anni '70 sognavano il 2000...che tristezza...- 200 risposte
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