Bombardier Challenger 300 3D 모델

The Bombardier BD-100 Challenger 300 is a super-mid-sized jet capable of traversing transcontinental distances. It is not developmentally related to the similarly named Challenger 600-series, or the 600-derived Challenger 800-series. The project was launched at the Paris Air Show on July 13, 1999, at which time it was called the Bombardier Continental. It was a "clean sheet" design, assembled in Bombardier's Learjet plant at Wichita Mid-Continent airport, Kansas. The jet was renamed in September 2002 after much debate about which category {Learjet, Challenger, or Global} the new aircraft fit into. It entered commercial service in January 2004. Crew: Two (pilot & co-pilot) Capacity: Up to 16 passengers (normally 8) Length: 20.93 m (68 ft 8 in) Wingspan: 19.46 m (63 ft 10 in) Height: 6.2 m (20 ft 4 in) Wing area: 48.5 m2 (522 sq ft) Empty weight: 10,591 kg (23,349 lb) Max takeoff weight: 17,622 kg (38,850 lb) Powerplant: 2 × Honeywell HTF7000 turbofan engines, 30.36 kN (6,825 lbf) thrust each Maximum speed: 891 km/h (554 mph; 481 kn) Maximum speed: Mach 0.83 Cruising speed: 850 km/h (528 mph; 459 kn) Range: 5,741 km (3,567 mi; 3,100 nmi) at 0.78 Mach Service ceiling: 13,716 m (45,000 ft) Rate of climb: 25.4 m/s (5,000 ft/min) at 17,622 kg (38,850 lb) max gross weight Wing loading: 359.5 kg/m2 (73.6 lb/sq ft) Avionics: Rockwell Collins Proline 21 Info & Specs: Wikipedia