
Loading the evidence…
Preparing your view.
Preparing your view.


At a glance
Measured figures
J-21 Jastreb · Length
Single source10.88 m (35 ft 8 in)[source]
Configuration
| Specification | Soko J-21 Jastreb | Su-25 Frogfoot |
|---|---|---|
| Type | Light attack aircraft[source] | Attack aircraft / close air support[source] |
| Manufacturer | SOKO[source] | Sukhoi, Tbilisi Aircraft Manufacturing, Ulan-Ude Aviation Plant[source] |
| Designer | Aeronautical Technical Institute (ATI)[source] | Sukhoi[source] |
| Status | Retired from Republika Srpska Air Force (2006)[source] | In service |
Su-25/Su-25K, late production · including nose probe
15.53 m (50 ft 11 in) (including nose probe)[source]
Empty; Empty weight
Single sourceMaximum take-off; J-21 Jastreb · Max takeoff weight
Single source5,100 kg (11,244 lb)[source]
2820 кг[source]
Empty; Su-25/Su-25K, late production · Empty weight
Single sourceGross; Su-25/Su-25K, late production · Gross weight
Single sourceCruise; J-21 Jastreb · at 5,000 m (16,000 ft)
Single sourceMaximum; J-21 Jastreb · Maximum speed
Single source820 km/h (510 mph, 440 kn)[source]
740 km/h (460 mph, 400 kn) at 5,000 m (16,000 ft)[source]
Maximum; Su-25/Su-25K, late production · at sea level
Single source975 km/h (606 mph, 526 kn) at sea level[source]
Su-25/Su-25K, late production · at sea level with 4,400 kg (9,700 lb) of ordnance and two external fuel tanks
Single source750 km (470 mi, 400 nmi) at sea level with 4,400 kg (9,700 lb) of ordnance and two external fuel tanks[source]
J-21 Jastreb · 1 × BMB (Rolls-Royce/Bristol Siddeley) Viper Mk 531 turbojet engine thrust
Single source1 × BMB (Rolls-Royce/Bristol Siddeley) Viper Mk 531 turbojet engine, 13.32 kN (2,990 lbf) thrust[source]
Su-25/Su-25K, late production · 2 × Soyuz/Tumansky R-195 turbojet engine thrust each
Single source2 × Soyuz/Tumansky R-195 turbojet engine, 44.18 kN (9,930 lbf) thrust each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | Yugoslav Air Force[source] | — |
|---|
| Number built | 224[source] | Over 1,000[source] |
|---|
| Manufactured | 1968–1977[source] | 1978–2017[source] |
|---|
| First flight | 19 July 1965[source] | 22 February 1975 ( 1975-02-22 )[source] |
|---|
| Developed from | Soko G-2 Galeb[source] | — |
|---|
| Fuel capacity | 440 kg (970 lb) internal fuel + 435 kg (959 lb) in 2x 275 L (60 imp gal; 73 US gal) jettisonable wing-tip fuel tanks.[source] | 3,200 L (850 US gal; 700 imp gal)[source] |
|---|
| g limits | +8 -4[source] | + 6.5[source] |
|---|
| Guns | 3 × 12.7 mm (0.5 in) Browning AN/M3 machine guns[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-2 autocannon with 250 rounds SPPU-22 gun pods for 2 × 23 mm Gryazev-Shipunov GSh-23 autocannons with 260 rounds[source] |
|---|
| Hardpoints | 8 with a capacity of inboard pylons (2 of) 250 kg (550 lb), outboard pylons (6 of) 50 kg (110 lb), with provisions to carry combinations of:[source] | 11 hardpoints with a capacity of up to 4,000 kg (8,800 lb) of stores, with provisions to carry combinations of: Rockets: UB-16 rocket pods for S-5 rockets UB-32 A rocket pods for S-5 rockets B-8M 1 rocket pods for S-8 rockets S-24 S-25 Missiles: Air-to-air missiles : K-13 A R-60 R-73 E Air-to-surface missiles : Kh-23 Kh-25 ML Kh-29 L 9K121 Vikhr Kh-38 (Su-25SM3) Anti-radiation missiles : Kh-28 Bombs: BETAB-500 concrete-penetrating bomb FAB-250 general-purpose bomb FAB-500 GP bomb FAN-500 bomb KAB-500KR TV-guided bomb ZAB-500 incendiary bomb Other: ASO-2V decoy dispensers (chaff and flare): Su-25s in Syria have been pictured with four rows of ASO-2V decoy dispensers (chaff and flare) along the tailcone's upper surface aft of the vertical stabiliser. Geran-5 drone[source] |
|---|
| Rockets | 6 × VRZ-157 127 mm (5.00 in) rockets[source] | UB-16 rocket pods for S-5 rockets UB-32 A rocket pods for S-5 rockets B-8M 1 rocket pods for S-8 rockets S-24 S-25[source] |
|---|
| Source measurement | Compared to the Galeb, the Jastreb has a strengthened structure, allowing more weapons to be carried, including three 12.7 mm (0.5 in) Browning AN/M3 machine guns, mounted in the nose of the aircraft. Also, the Jastreb is able to carry up to 800 kg (1,800 lb) on under-wing pylons, two inner pylons having a capacity of 250 kg (550 lb) for bombs, rocket launchers, and additional tanks, while the six outer pylons can carry VRZ-157 127 mm (5.00 in) rockets.[source]Soko J-21 Jastreb · Design and development; only the objects and conditions stated in this passage The first Yugoslav Air Force attack on Croatian troops took place on July 9, 1991 near Ilok, when two J-21 Jastreb attacked the base of the 1st Brigade of the Croatian National Guard . On August 24, 1991, during the Battle of Vukovar a member of the Croatian National Guard shot down one Yugoslav Air Force J-21 and damaged another aircraft with M55 anti-aircraft gun. On 15 November 1991, during the Battle of the Dalmatian Channels , three Yugoslav Air Force J-21 Jastrebs flew low over Brač and Šolta; minutes later, two were reportedly shot down by Croatian M55 anti-aircraft gun and Strela 2M. On 7 August 1995, during Operation Storm near Dvor na Una, members of the Air Defence Battalion of the 2nd Guards Brigade shot down a J-21 Jastreb over Bosanski Novi.[source]Soko J-21 Jastreb · Operational history / Croatia; only the objects and conditions stated in this passage Length: 10.88 m (35 ft 8 in)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Wingspan: 10.56 m (34 ft 8 in)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Height: 3.64 m (11 ft 11 in)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Wing area: 19.43 m 2 (209.1 sq ft)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Max takeoff weight: 5,100 kg (11,244 lb)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Fuel capacity: 440 kg (970 lb) internal fuel + 435 kg (959 lb) in 2x 275 L (60 imp gal; 73 US gal) jettisonable wing-tip fuel tanks.[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Powerplant: 1 × BMB (Rolls-Royce/Bristol Siddeley) Viper Mk 531 turbojet engine, 13.32 kN (2,990 lbf) thrust[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Powerplant: 2 × JATO units solid-fuelled rockets, 4.45 kN (1,000 lbf) thrust each[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Maximum speed: 820 km/h (510 mph, 440 kn)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Cruise speed: 740 km/h (460 mph, 400 kn) at 5,000 m (16,000 ft)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Range: 1.520 km (0.944 mi, 0.821 nmi) with tip tanks[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Service ceiling: 12,000 m (39,000 ft)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Rate of climb: 21 m/s (4,100 ft/min)[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Guns: 3 × 12.7 mm (0.5 in) Browning AN/M3 machine guns[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Hardpoints: 8 with a capacity of inboard pylons (2 of) 250 kg (550 lb), outboard pylons (6 of) 50 kg (110 lb), with provisions to carry combinations of: Other:[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage 2 × rocket pods each with 12x 55 mm (2.17 in) rockets[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage Rockets: 6 × VRZ-157 127 mm (5.00 in) rockets[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage 2 × 250 kg (550 lb) general-purpose bombs or[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage 2 × 150 kg (330 lb) cluster bombs or[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage 2 × 120 kg (260 lb) cluster fragmentation bombs[source]Soko J-21 Jastreb · Specifications (J-21 Jastreb); only the objects and conditions stated in this passage | — |
|---|
| Role | Yugoslav single-seat, single-engined, light attack aircraft ,[source] | — |
|---|
| Country of origin | Yugoslavia[source]Inventory Origin column; table 1, row 6, cell 2; revision 1376096397 | — |
|---|
| National origin | — | Soviet Union / Russia / Georgia[source] |
|---|
| Built by | — | TAM Management Tbilisi Aircraft Manufacturing Ulan-Ude Aviation Plant[source] |
|---|
| Primary users | — | Russian Aerospace Forces Ukrainian Air Force Korean People's Army Air Force Peruvian Air Force See Operators for others[source] |
|---|
| Introduction date | — | 19 July 1981[source] |
|---|
| Variant | — | Sukhoi Su-28[source] |
|---|
| 1 | — | SPM-17A cannon[source] |
|---|
| 2 | — | Air brakes[source] |
|---|
| 3 | — | Electronic countermeasures[source] |
|---|
| 4 | — | Laser Station Maple-PS[source] |
|---|
| 5 | — | Avionics[source] |
|---|
| 6 | — | Identification friend or foe system[source] |
|---|
| 7 | — | Pitot tube[source] |
|---|
| 8 | — | Drogue parachute[source] |
|---|
| 9 | — | Fuel tanks[source] |
|---|
| 10 | — | Main landing gear[source] |
|---|
| 11 | — | K-36L ejection seat[source] |
|---|
| 12 | — | Bulletproof glass[source] |
|---|
| 13 | — | Periscope[source] |
|---|
| 14 | — | Turbojet[source] |
|---|
| 15 | — | Air intake[source] |
|---|
| 16 | — | RSBN Short Range Navigation System[source] |
|---|
| 17 | — | PA-7 Pitot tube[source] |
|---|
| 18 | — | Front landing gear[source] |
|---|
| 19 | — | Canopy[source] |
|---|
| 20 | — | TSA-17 Sight[source] |
|---|
| 21 | — | Hinged ladder[source] |
|---|
| 22 | — | Longeron[source] |
|---|
| 23 | — | Flaps[source] |
|---|
| 24 | — | Leading edge slats[source] |
|---|
| 25 | — | Empennage, including rudder[source] |
|---|
| 26 | — | Aileron[source] |
|---|
| 27 | — | ASO-2V infrared countermeasures[source] |
|---|
| 28 | — | SPO-15 radar warning receiver[source] |
|---|
| 29 | — | Tail flaps[source] |
|---|
| 30 | — | CDD-25 hardpoints[source] |
|---|
| 31 | — | AAP-60 Starter engines[source] |
|---|
| Missiles | — | Air-to-air missiles : K-13 A R-60 R-73 E Air-to-surface missiles : Kh-23 Kh-25 ML Kh-29 L 9K121 Vikhr Kh-38 (Su-25SM3) Anti-radiation missiles : Kh-28[source] |
|---|
| Bombs | — | BETAB-500 concrete-penetrating bomb FAB-250 general-purpose bomb FAB-500 GP bomb FAN-500 bomb KAB-500KR TV-guided bomb ZAB-500 incendiary bomb[source] |
|---|
| Other | — | ASO-2V decoy dispensers (chaff and flare): Su-25s in Syria have been pictured with four rows of ASO-2V decoy dispensers (chaff and flare) along the tailcone's upper surface aft of the vertical stabiliser. Geran-5 drone[source] |
|---|
Maximum take-off; Su-25/Su-25K, late production · Max takeoff weight
Single source