The Gulfstream G200, formerly known as the IAI-1126 Galaxy, is a twin-engine business jet. It was designed originally by Israel Aerospace Industries (IAI) and was produced by IAI for Gulfstream Aerospace from 1999 through 2011.

The G200 was originally named "Astra Galaxy". When Gulfstream Aerospace purchased Galaxy Aerospace in 2001 the model was rebranded as the Gulfstream G200. Israel Aircraft Industries' subsidiary Galaxy Aerospace Inc. began designing the Galaxy in the late 1980s in a risk-sharing partnership with the Soviet aircraft design bureau Yakovlev OKB. The program officially launched in September 1993. Yakovlev handled design and manufacturing of the forward fuselage and empennage. However, the Russian company had trouble meeting agreed production schedules, and the partnership was ended in 1995. This led to another risk-sharing agreement, with EADS Sogerma manufacturing the fuselage and empennage, and IAI being responsible for final assembly and other prime contractor duties.

The Galaxy first flew on December 25, 1997. By December 1998 it had received certification from the US and Israeli aviation agencies. Deliveries began the following year. The Galaxy was renamed "G200" after Gulfstream Aerospace acquired Galaxy Aerospace in June 2001.

In 2005, Gulfstream began designing a follow-on aircraft. The new model, known as the "G250", was launched in 2008. It was later renamed the Gulfstream G280. The final production G200 rolled off the production line on December 19, 2011; 250 units had been built.

General characteristics

• Crew: 2
• Capacity: Typical Seating of 8-10, 18 Max / 4,050 lb (1,840 kg)
• Length: 62 ft 3 in (18.97 m)
• Wingspan: 58 ft 1 in (17.70 m)
• Height: 21 ft 5 in (6.53 m)
• Wing area: 369 sq ft (34.3 m²)
• Empty weight: 19,200 lb (8,709 kg)
• Max takeoff weight: 35,450 lb (16,080 kg)
• Powerplant: 2 × Pratt & Whitney Canada PW306A turbofans, 6,040 lbf (26.9 kN) thrust each

Performance

• Maximum speed: 487 kn (560 mph, 900 km/h) at altitude
• Cruise speed: 459 kn (528 mph, 850 km/h) normal cruise at altitude
• Range: 3,400 nmi (3,910 mi, 6,300 km) at Mach 0.75 with 4 passengers
• Service ceiling: 45,000 ft (13,700 m)

Source: Wikipedia