CL-600 Challenger vs Gulfstream G100
Overview
The CL-600 Challenger and the Gulfstream G100 are both Military Transport Aircraft, manufactured by Bombardier and Gulfstream respectively.
Top speed is 882 km/h for the CL-600 Challenger vs 874 km/h for the Gulfstream G100. The CL-600 Challenger has an operational range of 7,400 km vs 5,462 km for the Gulfstream G100. The Gulfstream G100 operates at altitudes up to 13,716 m compared to 12,497 m for the CL-600 Challenger.
The CL-600 Challenger has been produced in 1,066 units vs 265 for the Gulfstream G100. Unit cost is $14M for the CL-600 Challenger vs $4.3M for the Gulfstream G100. The CL-600 Challenger first flew 6 years before the Gulfstream G100 (1978 vs 1984).
| 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 introduced | 1980 |
| Number produced | 1066 units |
| Average unit price | $14 million |
| Israeli-American mid-size business jet, recognized for transcontinental range, introduced in the late 20th century. | |
|
|
| Origin country | 🇺🇸 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 |
| Wing area | 48.3 m² ◉ |
| Wingspan | 19.6 m ◉ |
| Height | 6.3 m ◉ |
| Length | 20.9 m ◉ |
| Maximum speed | 882 km/h ◉ |
| Operational range | 7,400 km ◉ |
| Service ceiling | 12,497 m ◉ |
| Max. takeoff weight | 19,550 kg ◉ |
| Empty weight | 9,292 kg ◉ |
| Total thrust | 2 x 2,073 kgf ◉ |
| Wing area | 29.4 m² ◉ |
| Wingspan | 16.6 m ◉ |
| Height | 5.5 m ◉ |
| Length | 17.0 m ◉ |
| Maximum speed | 874 km/h ◉ |
| Operational range | 5,462 km ◉ |
| Service ceiling | 13,716 m ◉ |
| Max. takeoff weight | 11,500 kg ◉ |
| Empty weight | 6,531 kg ◉ |
| Total thrust | 2 x 964 kgf ◉ |
Performance Radar Chart
Detailed Comparison
Loading analysis...
Generating comparison analysis...
Unable to generate comparison at this time.
Frequently Asked Questions
Which is faster, the CL-600 Challenger or Gulfstream G100?
The CL-600 Challenger is faster with a maximum speed of 882 km/h compared to the Gulfstream G100's 874 km/h, a difference of 8 km/h.
Which has longer range, the CL-600 Challenger or Gulfstream G100?
The CL-600 Challenger has a longer range at 7,400 km compared to the Gulfstream G100's 5,462 km.
Which can fly higher, the CL-600 Challenger or Gulfstream G100?
The Gulfstream G100 has a higher service ceiling at 13,716 meters (45,000 ft) compared to the CL-600 Challenger's 12,497 meters (41,000 ft).
Which is heavier, the CL-600 Challenger or Gulfstream G100?
The CL-600 Challenger has a higher maximum takeoff weight at 19,550 kg compared to the Gulfstream G100's 11,500 kg.
Which is larger, the CL-600 Challenger or Gulfstream G100?
The CL-600 Challenger is longer at 20.9 meters compared to the Gulfstream G100's 17.0 meters.
Which is more expensive, the CL-600 Challenger or Gulfstream G100?
The CL-600 Challenger is more expensive at approximately $14 million per unit compared to the Gulfstream G100 at $4.3 million.
Which entered service first, the CL-600 Challenger or Gulfstream G100?
The CL-600 Challenger entered service first in 1980, 5 years before the Gulfstream G100 which entered service in 1985.
Which has been built in greater numbers, the CL-600 Challenger or Gulfstream G100?
The CL-600 Challenger has been produced in greater numbers with 1,066 units compared to 265 units of the Gulfstream G100.