时间：2011-10-04 11:09来源：蓝天飞行翻译 作者：航空 点击：次
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Rome Dubai Singapore Johannesburg Hong Kong Beijing Moscow Sydney – – PERFORMANCE Maximum Range* 4,350 nm / 8,061 km (mach 0.80, 8 passengers, 3 crew and NBAA IFR reserves) Normal Cruise Speed Mach 0.80 / 459 ktas / 850 km/h High Speed Cruise Mach 0.85 / 488 ktas / 904 km/h Mmo (maximum Operating mach Number) Mach 0.88 Takeoff Distance (SL, ISA, MTOW) 5,600 ft / 1,707 m Landing Distance (SL, ISA, MLW) 3,260 ft / 994 m Initial Cruise Altitude 41,000 ft / 12,497 m Maximum Cruise Altitude 45,000 ft / 13,716 m WEIGHTS Maximum Takeoff Weight 74,600 lb / 33,838 kg Maximum Landing Weight 66,000 lb / 29,937 kg Maximum Zero Fuel Weight 49,000 lb / 22,226 kg Basic Operating Weight** (including 3 crew) 43,000 lb / 19,505 kg Maximum Payload ** 6,000 lb / 2,722 kg Payload with Maximum Fuel ** 2,500 lb / 1,134 kg Maximum Fuel Weight 29,500 lb / 13,381 kg DESIGN STANDARDS Avionics Gulfstream PlaneView® Engines Two Rolls-Royce Tay Mk 611-8C Rated Takeoff Thrust (each) 13,850 lb / 61.6 kN Passengers: Maximum 19 Typical Outfitting 12 – 16 INTERIOR Total Interior Length 45 ft 1 in / 13.74 m Cabin Length (excluding baggage) 40 ft 4 in / 12.29 m Cabin Height 6 ft 2 in / 1.88 m Cabin Width 7 ft 4 in / 2.24 m Cabin Volume 1,525 cu ft / 43.2 cu m Baggage Compartment Volume 169 cu ft / 4.8 cu m COMFORT 12 Gulfstream Signature Oval Windows Forward or Aft Galley Forward and Aft Lavatories 6 Select Floor Plans or Tailored Floor Plan Mach Maximum Mach M ach Specifications *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. 7 7 ft 10 in/23.72 m 89 ft 4 in/27.23 m 25 ft 2 in/7.67 m 77 m89 m25 m* |
