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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
Performance Radar Chart
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Former operators · 89 built
Largest operators · in service
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Frequently Asked Questions

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.