Gulfstream Gulfstream G100
Summary
| Category | Transport aircraft |
| Origin country | 🇺🇸 United States |
| First flight | 1 January 1984 |
| Year of introduction | 1985 |
| Number produced | 265 units |
Description
The Gulfstream G100 is a business jet developed by the American aerospace company Gulfstream Aerospace Corporation. This aircraft was initially designed by Israel Aerospace Industries as the Astra SPX before being acquired by Gulfstream. The G100 is a mid-sized aircraft primarily used for business and executive travel. It features a spacious cabin with comfortable seating and amenities, offering a range of in-flight services to passengers. With its capable performance and range, the G100 is able to operate on both short and medium-haul flights. It has been deployed worldwide for various business and corporate missions, providing reliable and efficient transportation for its clientele.
Technical specifications
| Version: Gulfstream G100 | |
|---|---|
| Maximum speed | 874 km/h (543 mph) |
| Wing area | 29.4 m² (316.5 sqft) |
| Wingspan | 16.6 m (54.6 ft) |
| Height | 5.5 m (18.2 ft) |
| Length | 17.0 m (55.6 ft) |
| Service ceiling | 13716 m (45000 ft) |
| Empty weight | 6531 kg (14398 lbs) |
| Max. takeoff weight | 11500 kg (25353 lbs) |
| Climb rate | 19.0 m/s (62.3 ft/s) |
| Powerplant | 2 × turbojets Honeywell TFE731-40R-200G delivering 1928 kgp |
Current operating countries
| Country | Units | ||
|---|---|---|---|
|
India | 2 | |
|
United States | 2 | |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.