Ajeet vs Kfir
Ajeet vs Kfir at a glance — top speed 1,152 vs 2,440 km/h, range 172 vs 1,000 km, max takeoff weight 4,173 vs 16,200 kg, built 89 vs 220 units.
Specifications
|
Ajeet |
Kfir |
| Origin country |
🇮🇳 India |
🇮🇱 Israel |
| Category |
Combat Aircraft |
Combat Aircraft |
| Manufacturer |
HAL |
IAI |
| First flight |
6 March 1975 |
4 June 1973 |
| Year introduced |
1977 |
1974 |
| Number produced |
89 units |
220 units |
| Average unit price |
-- |
$20 million |
| Wing area |
12.7 m² |
34.8 m² |
| Wingspan |
6.7 m |
8.2 m |
| Height |
2.5 m |
4.6 m |
| Length |
9.0 m |
15.7 m |
| Maximum speed |
1152 km/h |
2440 km/h |
| Operational range |
172 km |
1,000 km |
| Service ceiling |
13,720 m |
17,678 m |
| Max. takeoff weight |
4,173 kg |
16,200 kg |
| Empty weight |
2,307 kg |
7,285 kg |
| Total thrust |
1 x 20 kN
|
1 x 8,119 kgf
|
Detailed Comparison
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Which is faster, the Ajeet or Kfir?
The Kfir is faster with a maximum speed of 2,440 km/h compared to the Ajeet's 1,152 km/h, a difference of 1,288 km/h.
Which has longer range, the Ajeet or Kfir?
The Kfir has a longer range at 1,000 km compared to the Ajeet's 172 km.
Which can fly higher, the Ajeet or Kfir?
The Kfir has a higher service ceiling at 17,678 meters (57,998 ft) compared to the Ajeet's 13,720 meters (45,013 ft).
Which is heavier, the Ajeet or Kfir?
The Kfir has a higher maximum takeoff weight at 16,200 kg compared to the Ajeet's 4,173 kg.
Which is larger, the Ajeet or Kfir?
The Kfir is longer at 15.7 meters compared to the Ajeet's 9.0 meters.
Which entered service first, the Ajeet or Kfir?
The Kfir entered service first in 1974, 3 years before the Ajeet which entered service in 1977.
Which has been built in greater numbers, the Ajeet or Kfir?
The Kfir has been produced in greater numbers with 220 units compared to 89 units of the Ajeet.