J-20 Kraguj
Yugoslavian light attack aircraft, largely used in the Croatian War of Independence during the early 1990s.
| Crew | 1 |
| Length | 7.9 m (26.0 ft) |
| Wingspan | 10.6 m (34.9 ft) |
| Height | 3 m (9.8 ft) |
| Wing area | 17 m² (183.0 sqft) |
| Empty weight | 1,130 kg (2,491 lbs) |
| Max. takeoff weight | 1,624 kg (3,580 lbs) |
| Powerplant | 1 × pistons engine Lycoming GSO-480-B1A6 254 kW each |
| Maximum speed | 295 km/h (183 mph) |
| Operational range | 800 km (497 mi) |
| Service ceiling | 8,000 m (26,247 ft) |
| Climb rate | 8.0 m/s (26.2 ft/s) |
Description
The Soko J-20 Kraguj was designed by VTI and manufactured by SOKO in Yugoslavia. It first flew in 1962. This light military, single-engine, low-wing single-seat aircraft with a metal airframe, was designed to perform close air support, counterinsurgency (COIN), and reconnaissance missions.
Design
The Soko J-20 Kraguj features a classic semi-monocoque, metal structure with a slightly tapered wing. The pilot is accommodated in an enclosed, heated, and ventilated cockpit, equipped with adjustable seats, with the cockpit canopy sliding backwards to open. The landing gear is non-retractable and includes a tail wheel. Shock absorption is achieved through rubber dampers, and hydraulic brakes provide wheel braking. The powerplant consists of one 340 hp Textron Lycoming GSO-480-B1J6 piston engine coupled with a Hartzell HC-B3Z20-1/10151C-5 three-blade metal variable-pitch propeller. Engine cooling airflow is enhanced by two specially designed ejectors. The aircraft carries 36 US Gal of fuel in two rubber tanks, enabling a flight range of 350 NM with a full armament configuration. A 1.5 kW generator and a storage battery supply 28 V DC electric power. The windshield is defogged and de-iced by blowing hot air.
Armament
The J-20 Kraguj features a permanent armament of two wing-mounted 7.7 mm Colt–Browning Mk II machine guns, each with a capacity of 650 rounds, complemented by a collimator sight in the cockpit. For combat missions, it is equipped with underwing pylons capable of carrying external loads including bombs (such as 100 kg bombs, cluster bombs, and cargo bombs), multi-tube launchers for twelve 57 mm air-to-ground rockets, and launchers for 128 mm (HVAR-5) air-to-ground rockets. Adapters on the underwing pylons facilitate the configuration switch between various free-fall bombs and rocket launchers.
Operational History
The Soko J-20 Kraguj was conceived with a unique operational doctrine in mind, drawing from Yugoslavia's experiences in WWII. It was designed to function as a "Partisan aircraft," providing reconnaissance and strike capabilities to guerilla groups should the Yugoslav Air Force be neutralized early in a conflict. To that end, the Kraguj was designed to operate from short, unimproved airstrips, especially in mountainous regions, and was even capable of being fitted with skis. In addition to its primary ground support role, it also served as a trainer for basic flight and advanced ground attack training. The type was used by the SFR Yugoslav Air Force, the Air Force of Republika Srpska, and the Croatian Air Force.
Variants
Main Variants:
- The standard J-20, the primary production model designed for close air support, counterinsurgency, and reconnaissance.
Frequently Asked Questions
What type of aircraft is the J-20 Kraguj?
What is the maximum speed of the J-20 Kraguj?
What is the range of the J-20 Kraguj?
When did the J-20 Kraguj first fly?
How many J-20 Kraguj have been built?
What is the service ceiling of the J-20 Kraguj?
- AUG 12026 Updated Manufacturer updated
- APR 72026 Updated Picture credits updated in a site-wide editorial pass
- JAN 122026 Updated Range updated in a site-wide editorial pass