Gulfstream II vs Gulfstream IV
| American business jet, operational from 1960s to present, widely used for executive transport and various military applications worldwide. | |
| Origin country | 🇺🇸 United States |
| Category | Military Transport Aircraft |
| Manufacturer | Gulfstream |
| First flight | 2 October 1966 |
| Year of introduction | 1967 |
| Number produced | 256 units |
| Average unit price | $-- million |
| American business jet from the late 20th century, recognized for its widespread use in corporate and private aviation. | |
| Origin country | 🇺🇸 United States |
| Category | Military Transport Aircraft |
| Manufacturer | Gulfstream |
| First flight | 19 September 1985 |
| Year of introduction | 1987 |
| Number produced | 900 units |
| Average unit price | $26 million |
| Wing area | 75.2 m² ◉ |
| Wingspan | 20.8 m ◉ |
| Height | 7.5 m ◉ |
| Length | 24.1 m ◉ |
| Maximum speed | 935 km/h ◉ |
| Operational range | -- km |
| Service ceiling | 13,716 m ◉ |
| Max. takeoff weight | 29,710 kg ◉ |
| Empty weight | 16,576 kg ◉ |
| Total thrust | 2 x 5,171 kgf ◉ |
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| Wing area | 88.3 m² ◉ |
| Wingspan | 23.5 m ◉ |
| Height | 7.7 m ◉ |
| Length | 27.2 m ◉ |
| Maximum speed | 935 km/h ◉ |
| Operational range | 7,815 km |
| Service ceiling | 13,716 m ◉ |
| Max. takeoff weight | 33,520 kg ◉ |
| Empty weight | 19,504 kg ◉ |
| Total thrust | 2 x 6,282 kgf ◉ |