这是两飞机的数据： ___________________________________________________________________________ AG600:
General characteristics Capacity: 50 passengers Length: 36.9 m (121 ft 1 in) Wingspan: 38.8 m (127 ft 4 in) Height: 12.1 m (39 ft 8 in) Max takeoff weight: 53,500 kg (117,947 lb) Powerplant: 4 × WJ-6 turboprops, 3,805 kW (5,103 hp) each Propellers: 6-bladed constant speed propellers
Performance Maximum speed: 570 km/h (354 mph; 308 kn) Range: 5,500 km (3,418 mi; 2,970 nmi) Service ceiling: 10,500 m (34,400 ft)
_________________________________________________________________________ US-2:
General characteristics Crew: 11 Capacity: 20 passengers or 12 stretchers Length: 33.46 m (109 ft 9 in) Wingspan: 33.15 m (108 ft 9 in) Height: 9.8 m (32 ft 2 in) Wing area: 135.8 m2 (1,462 sq ft) Empty weight: 25,630 kg (56,504 lb) Gross weight: 43,000 kg (94,799 lb) water take-off Max takeoff weight: 47,700 kg (105,160 lb) land take-off Powerplant: 4 × Rolls-Royce AE 2100J turboprop, 3,424 kW (4,592 hp) each Powerplant: 1 × LHTEC T800 turboshaft Boundary layer control compressor, 1,017 kW (1,364 hp) Propellers: 6-bladed Dowty R414
Performance Maximum speed: 560 km/h (348 mph; 302 kn) Cruise speed: 480 km/h (298 mph; 259 kn) at 6,000 m (20,000 ft) Range: 4,700 km (2,920 mi; 2,538 nmi) Service ceiling: 7,195 m (23,606 ft) Takeoff distance on ground at MTOW: 490 m (1,610 ft) Landing distance on ground at MTOW: 1,500 m (4,900 ft) Takeoff distance on water at Loaded weight: 280 m (920 ft) Landing distance on water at Loaded weight: 330 m (1,080 ft)
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