Alarus CH2000 vs HJT-16 Kiran
The Alarus CH2000 and the HJT-16 Kiran are both Military Training Aircraft, manufactured by AMD and HAL respectively. The HJT-16 Kiran reaches 695 km/h — 2.6x the Alarus CH2000's 265 km/h. The Alarus CH2000 has an operational range of 900 km vs 615 km for the HJT-16 Kiran. The HJT-16 Kiran operates at altitudes up to 9,144 m compared to 3,810 m for the Alarus CH2000. At 4,235 kg MTOW, the HJT-16 Kiran is 5.5x the Alarus CH2000's 767 kg. The Alarus CH2000 has been produced in 150 units vs 190 for the HJT-16 Kiran. The HJT-16 Kiran first flew 31 years before the Alarus CH2000 (1964 vs 1995).
| Canadian light sports aircraft, produced in the 1990s, primarily employed for flight training and personal use. | |
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| Origin country | 🇨🇦 Canada |
| Category | Military Training Aircraft |
| Manufacturer | AMD |
| First flight | 1 January 1995 |
| Year introduced | 1995 |
| Number produced | 150 units |
| Average unit price | $725K |
| Indian jet trainer, primarily used by the Indian Air Force from the 1960s, notable for intermediate training roles. | |
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| Origin country | 🇮🇳 India |
| Category | Military Training Aircraft |
| Manufacturer | HAL |
| First flight | 4 September 1964 |
| Year introduced | 1968 |
| Number produced | 190 units |
| Average unit price | -- |
| Wing area | 12.7 m² ◉ |
| Wingspan | 8.8 m â—‰ |
| Height | 2.1 m â—‰ |
| Length | 7.0 m â—‰ |
| Maximum speed | 265 km/h â—‰ |
| Operational range | 900 km â—‰ |
| Service ceiling | 3,810 m â—‰ |
| Max. takeoff weight | 767 kg â—‰ |
| Empty weight | 492 kg â—‰ |
| Total thrust | 1 x 87 kW â—‰ |
| Wing area | 19.0 m² ◉ |
| Wingspan | 10.7 m â—‰ |
| Height | 3.6 m â—‰ |
| Length | 10.6 m â—‰ |
| Maximum speed | 695 km/h â—‰ |
| Operational range | 615 km â—‰ |
| Service ceiling | 9,144 m â—‰ |
| Max. takeoff weight | 4,235 kg â—‰ |
| Empty weight | 2,560 kg â—‰ |
| Total thrust | 1 x 1,134 kgf â—‰ |
Performance Radar Chart
Frequently Asked Questions
Which is faster, the Alarus CH2000 or HJT-16 Kiran?
The HJT-16 Kiran is faster with a maximum speed of 695 km/h compared to the Alarus CH2000's 265 km/h, a difference of 430 km/h.
Which has longer range, the Alarus CH2000 or HJT-16 Kiran?
The Alarus CH2000 has a longer range at 900 km compared to the HJT-16 Kiran's 615 km.
Which can fly higher, the Alarus CH2000 or HJT-16 Kiran?
The HJT-16 Kiran has a higher service ceiling at 9,144 meters (30,000 ft) compared to the Alarus CH2000's 3,810 meters (12,500 ft).
Which is heavier, the Alarus CH2000 or HJT-16 Kiran?
The HJT-16 Kiran has a higher maximum takeoff weight at 4,235 kg compared to the Alarus CH2000's 767 kg.
Which is larger, the Alarus CH2000 or HJT-16 Kiran?
The HJT-16 Kiran is longer at 10.6 meters compared to the Alarus CH2000's 7.0 meters.
Which entered service first, the Alarus CH2000 or HJT-16 Kiran?
The HJT-16 Kiran entered service first in 1968, 27 years before the Alarus CH2000 which entered service in 1995.
Which has been built in greater numbers, the Alarus CH2000 or HJT-16 Kiran?
The HJT-16 Kiran has been produced in greater numbers with 190 units compared to 150 units of the Alarus CH2000.