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Gulfstream G200
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The Gulfstream
G200 is the new designation for the IAI 1126
Galaxy, after Gulfstream Aerospace took over
marketing of the type in May 2001. The aircraft
falls into the super mid-size class of business
jets and offers transatlantic range with a roomy
cabin. |
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Developing nation: |
United States of America / Israel |
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Manufacturer/designer: |
Gulfstream Aerospace / Israel Aircraft
Industries. |
| Production line: |
Ben Gurion International Airport, Israel. |
| Type aircraft: |
Super mid-size business-jet. |
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First flight: |
December 25, 1997 as IAI 1126
Galaxy. |
| First delivery: |
to TTI Industries in January
2000. |
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Gulfstream G200 |
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Cockpit crew: |
2. |
| Passengers: |
10 - 18. |
| Cabin length: |
7,44 m. |
| Cabin diameter: |
2,18 m. |
| Cabin height: |
1,91 m. |
| Cabin volume: |
24,6 m³ |
| Baggage
compartment: |
4,2 m³. |
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Wing span: |
17,70 m. |
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Wing area: |
34,3 m². |
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Fuselage length: |
18,97m. |
| Height: |
6,53 m. |
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Engines: |
- two
Pratt & Whitney 306A each rated 26.9 kN. |
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Weight: |
- basic
operating weight with 2 crew: 9.049 Kg.
- max. zero-fuel weight: 10.866
Kg.
- fuel: 6.804 kg.
- max. payload: 1.837 Kg. |
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Max. take off weight: |
16.080 Kg. |
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Max. landing weight: |
13.608 Kg. |
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Cruise speed: |
796 km/h. |
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Max. speed: |
850 km/h. |
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Service ceiling: |
11.887 m. |
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Max. ceiling: |
13.716 m. |
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Max. range: |
6.301 km. |
| Performance: |
- take-off run 1.854 m at max.
take-off weight.
- landing run 1.000 m at max.
landing weight. |
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