Gulfstream G100 vs Gulfstream IV
Overview
The Gulfstream G100 and the Gulfstream IV are both Military Transport Aircraft, manufactured by Gulfstream and Gulfstream respectively.
Top speed is 874 km/h for the Gulfstream G100 vs 935 km/h for the Gulfstream IV. The Gulfstream G100 has an operational range of 5,462 km vs 7,815 km for the Gulfstream IV. The Gulfstream G100 operates at altitudes up to 13,716 m compared to 13,716 m for the Gulfstream IV. At 33,520 kg MTOW, the Gulfstream IV is 2.9x the Gulfstream G100's 11,500 kg.
The Gulfstream G100 has been produced in 265 units vs 900 for the Gulfstream IV. Unit cost is $4.3M for the Gulfstream G100 vs $26M for the Gulfstream IV. The Gulfstream G100 first flew 1 years before the Gulfstream IV (1984 vs 1985).
| Israeli-American mid-size business jet, recognized for transcontinental range, introduced in the late 20th century. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Gulfstream |
| First flight | 1 January 1984 |
| Year introduced | 1985 |
| Number produced | 265 units |
| Average unit price | $4.3 million |
| American business jet from the late 20th century, recognized for its widespread use in corporate and private aviation. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Gulfstream |
| First flight | 19 September 1985 |
| Year introduced | 1987 |
| Number produced | 900 units |
| Average unit price | $26 million |
| Wing area | 29.4 mΒ² β |
| Wingspan | 16.6 m β |
| Height | 5.5 m β |
| Length | 17.0 m β |
| Maximum speed | 874 km/h β |
| Operational range | 5,462 km β |
| Service ceiling | 13,716 m β |
| Max. takeoff weight | 11,500 kg β |
| Empty weight | 6,531 kg β |
| Total thrust | 2 x 964 kgf β |
| Wing area | 88.3 mΒ² β |
| Wingspan | 23.5 m β |
| Height | 7.7 m β |
| Length | 27.2 m β |
| Maximum speed | 935 km/h β |
| Operational range | 7,815 km β |
| Service ceiling | 13,716 m β |
| Max. takeoff weight | 33,520 kg β |
| Empty weight | 19,504 kg β |
| Total thrust | 2 x 3,141 kgf β |
Performance Radar Chart
Detailed Comparison
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