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G-2 Galeb vs Soko G-4 Super Galeb

G-2 Galeb vs Soko G-4 Super Galeb at a glance — top speed 812 vs 910 km/h, range 669 vs 1,900 km, max takeoff weight 4,300 vs 6,330 kg, built 248 vs 85 units.

Soko G-2 Galeb military training aircraft side profile drawing
🇷🇸 G-2 Galeb
Specifications
G-2 Galeb Soko G-4 Super Galeb
Origin country 🇷🇸 Ex-Yugoslavia 🇷🇸 Ex-Yugoslavia
Category Military Training Aircraft Military Training Aircraft
Manufacturer Soko Soko
First flight 31 July 1961 17 July 1978
Year introduced 1965 1983
Number produced 248 units 85 units
Average unit price $180K --
Wing area 19.4 m² 19.5 m²
Wingspan 11.6 m 9.9 m
Height 3.3 m 4.3 m
Length 10.3 m 12.3 m
Maximum speed 812 km/h 910 km/h
Operational range 669 km 1,900 km
Service ceiling 12,000 m 12,850 m
Max. takeoff weight 4,300 kg 6,330 kg
Empty weight 2,620 kg 3,250 kg
Total thrust 1 x 1,134 kgf 1 x 1,815 kgf
Performance Radar Chart

Detailed Comparison

The Soko G-2 Galeb established Yugoslavia’s domestic aerospace capability in the 1960s, functioning as a reliable basic trainer analogous to the Jet Provost. Its successor, the G-4 Super Galeb, abandoned this utilitarian lineage for a high-performance design mirroring the British Aerospace Hawk. While the G-2 was a volume product for the Non-Aligned Movement, the G-4 represented a genuine attempt to compete with Western advanced jet trainers, though its potential was strangled by geopolitical dissolution.

Development and Design

The G-2 Galeb, initiated in 1957, relied heavily on British technology—specifically the Armstrong Siddeley Viper engine—to replace the Lockheed T-33. Its straight-wing architecture and unpressurized cockpit prioritized stability for ab initio cadets. Conversely, the G-4 Super Galeb (N-62) adopted the swept-wing configuration essential for advanced combat lead-in. Visually and structurally echoing the BAe Hawk, the G-4 integrated Martin-Baker seats and a stepped cockpit, addressing the G-2’s poor instructor visibility. The G-4 was not merely an upgrade but a clean-sheet redesign meant to bridge the gap to high-performance interceptors like the MiG-29, incorporating avionics for adverse weather operations that the G-2 lacked.

Specifications and Performances

Performance metrics illustrate the doctrinal shift from basic handling to tactical energy management. The G-4 utilizes the uprated Rolls-Royce Viper 632-46, generating 1,815 kgf of thrust compared to the G-2’s 1,134 kgf. This yields a 36% increase in climb rate (31.0 m/s vs 22.8 m/s). While the G-2 maxes out at 812 km/h, the G-4 reaches 910 km/h, edging closer to transonic regimes required for modern fighter training. The G-4 provides a significant leap in combat radius, nearly tripling the range (1,900 km vs 669 km) and upgrading armament from fixed .50 caliber nose guns to a centerline 23mm GSh-23L cannon pod and heavier ordnance capacity, including cluster munitions.

Deployment and Usage

The G-2 saw extensive service as the primary trainer for the Yugoslav Air Force and achieved export success in Libya and Zambia. Its combat record is defined by low-intensity conflicts and attrition; Libyan G-2s were heavily targeted by NATO during the 2011 civil war. The G-4’s operational history is inextricably linked to the violent breakup of Yugoslavia. Unlike the G-2, the G-4 was employed aggressively in close air support (CAS) roles during the Balkan conflicts. This exposure proved costly: NATO F-16s downed three G-4s during Operation Deny Flight in 1994, and 23 were destroyed on the ground in 1999. The G-4 secured only one export client, Myanmar, before sanctions halted production.

Conclusion

The G-2 Galeb succeeded as an industrial milestone, proving SOKO could manufacture reliable jet aircraft in volume. However, the G-4 Super Galeb is objectively the superior platform, offering avionics, kinematics, and payload options comparable to the Alpha Jet or MB-339. The G-2 belongs to the obsolescent first generation of straight-wing jet trainers. The G-4 remains a viable, if orphan, platform for light attack and advanced training, limited only by the geopolitical collapse that severed its supply chain and export potential.

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Frequently Asked Questions

Which is faster, the G-2 Galeb or Soko G-4 Super Galeb?
The Soko G-4 Super Galeb is faster with a maximum speed of 910 km/h compared to the G-2 Galeb's 812 km/h, a difference of 98 km/h.
Which has longer range, the G-2 Galeb or Soko G-4 Super Galeb?
The Soko G-4 Super Galeb has a longer range at 1,900 km compared to the G-2 Galeb's 669 km.
Which can fly higher, the G-2 Galeb or Soko G-4 Super Galeb?
The Soko G-4 Super Galeb has a higher service ceiling at 12,850 meters (42,158 ft) compared to the G-2 Galeb's 12,000 meters (39,370 ft).
Which is heavier, the G-2 Galeb or Soko G-4 Super Galeb?
The Soko G-4 Super Galeb has a higher maximum takeoff weight at 6,330 kg compared to the G-2 Galeb's 4,300 kg.
Which is larger, the G-2 Galeb or Soko G-4 Super Galeb?
The Soko G-4 Super Galeb is longer at 12.2 meters compared to the G-2 Galeb's 10.3 meters.
Which entered service first, the G-2 Galeb or Soko G-4 Super Galeb?
The G-2 Galeb entered service first in 1965, 18 years before the Soko G-4 Super Galeb which entered service in 1983.
Which has been built in greater numbers, the G-2 Galeb or Soko G-4 Super Galeb?
The G-2 Galeb has been produced in greater numbers with 248 units compared to 85 units of the Soko G-4 Super Galeb.