Gulfstream IV vs CL-600 Challenger
| 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
|
| Canadian business jet, introduced in the 1980s, extensively deployed for VIP and corporate travel worldwide. |
|
| Origin country |
🇨🇦 Canada
|
| Category |
Military Transport Aircraft |
| Manufacturer |
Bombardier |
| First flight |
8 November 1978 |
| Year of introduction |
1980 |
| Number produced |
1066 units
|
| Average unit price |
$14 million
|
| 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
◉
|
|
|
| Wing area |
48.3 m²
◉
|
| Wingspan |
19.6 m
◉
|
| Height |
6.3 m
◉
|
| Length |
20.9 m
◉
|
| Maximum speed |
882 km/h
◉
|
| Operational range |
-- km
|
| Service ceiling |
12,497 m
◉
|
| Max. takeoff weight |
19,550 kg
◉
|
| Empty weight |
9,292 kg
◉
|
| Total thrust |
2 x 4,146 kgf
◉
|
|
|
Photo of CL-600 Challenger by Bombardier.