時(shí)間：2011-10-01 17:38來(lái)源：藍(lán)天飛行翻譯 作者：航空 點(diǎn)擊：次
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Remarkable Takeoff With its powerful engines and efficient aerodynamics, the G150 has remarkable takeoff performance from demanding airports. In 2007, the G150 departed Aspen's 7,815 feet (2,382 m) elevation airport and flew non stop to White Plains, New York, at Mach 0.80 in a record-setting three hours and eight minutes. The G150 continues to make remarkable flights that demonstrate its outstanding combination of speed, range and takeoff performance. *Flights noted were accomplished with the G150. Actual performance will be affected by ATC routing, operating speed, weather, outfitting options and other factors. *NBAA IFR theoretical range. Actual range will be affected by ATC routing, operating speed, weather, outfitting options and other factors. **Stated weights are based on theoretical standard outfitting configurations. Actual weights will be affected by outfitting options and other factors. Specifications PERFORMANCE Maximum Range* 3,000 nm / 5,556 km (Mach 0.75, 4 passengers, 2 crew and NBAA IFR reserves) Long-Range Cruise Speed Mach 0.75 / 430 ktas / 796 km/h Normal Cruise Speed Mach 0.80 / 459 ktas / 850 km/h Mmo (Maximum Operating Mach Number) M ach 0.85 Takeoff Distance (SL, ISA, MTOW) 5,000 ft / 1,524 m Landing Distance (SL, ISA, MLW) 2,880 ft / 878 m Initial Cruise Altitude 41,000 ft / 12,497 m Maximum Cruise Altitude 45,000 ft / 13,716 m WEIGHTS Maximum Takeoff Weight 26,100 lb / 11,839 kg Maximum Landing Weight 21,700 lb / 9,843 kg Maximum Zero Fuel Weight 17,500 lb / 7,938 kg Basic Operating Weight** (including 2 crew) 15,100 lb / 6,849 kg Maximum Payload** 2,400 lb / 1,089 kg Payload with Maximum Fuel ** 850 lb / 386 kg Maximum Fuel Weight 10,300 lb / 4,672 kg DESIGN STANDARDS Avionics Rockwell Collins Pro Line 21 Engines Two Honeywell TFE 731-40AR Rated Takeoff Thrust (each) 4,420 lb / 19.66 kN Passengers: Typical Outfitting 6–8 |
