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At a glance
Measured figures
Jaguar A / S · Length
Single source16.83 m (55 ft 3 in)[source]
Configuration
| Specification | SEPECAT Jaguar | Soko J-21 Jastreb |
|---|---|---|
| Type | Attack aircraft[source] | Light attack aircraft[source] |
| National origin | France / United Kingdom[source] | — |
| Manufacturer | SEPECAT ( Breguet / BAC )[source] | SOKO[source] |
| Built by | SEPECAT / HAL[source] | — |
| Status | In service[source] |
J-21 Jastreb · Length
10.88 m (35 ft 8 in)[source]
Empty; Jaguar A / S · typical, (dependent on variant and role)
Single sourceGross; Jaguar A / S · full internal fuel and 120 rpg
Single sourceMaximum take-off; Jaguar A / S · with external stores
Single source7,000 kg (15,432 lb) typical, (dependent on variant and role)[source]
10,954 kg (24,149 lb) full internal fuel and 120 rpg[source]
15,700 kg (34,613 lb) with external stores[source]
Empty; Empty weight
Single sourceMaximum take-off; J-21 Jastreb · Max takeoff weight
Single sourceMaximum; Jaguar A / S · Mach 1.1 at sea level
Single source1,350 km/h (840 mph, 730 kn) Mach 1.1 at sea level[source]
Jaguar A / S · hi-lo-hi (internal fuel)
Single source815 km (506 mi, 440 nmi) hi-lo-hi (internal fuel)[source]
Jaguar A / S · 2 × Rolls-Royce Turbomeca Adour Mk.102 afterburning turbofan engines thrust each dry
Single sourceJaguar A / S · with afterburner
Single source2 × Rolls-Royce Turbomeca Adour Mk.102 afterburning turbofan engines, 22.75 kN (5,110 lbf) thrust each dry, 32.5 kN (7,300 lbf) with afterburner[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]
J-21 Jastreb · 4,100 ft/min
Single source21 m/s (4,100 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Retired from Republika Srpska Air Force (2006)[source] |
| Primary users | Indian Air Force Royal Air Force (historical) French Air Force (historical) Royal Air Force of Oman (historical)[source] | — |
|---|
| Number built | 573[source] | 224[source] |
|---|
| Manufactured | 1968–1981[source] | 1968–1977[source] |
|---|
| Introduction date | 1973[source] | — |
|---|
| First flight | 8 September 1968[source] | 19 July 1965[source] |
|---|
| Retired | 2005 (France) / 2007 (UK) / 2014 (Oman)[source] | — |
|---|
| Fuel capacity | 4,200 L (1,100 US gal; 920 imp gal) internal, with provision for three 1,200 L (320 US gal; 260 imp gal) drop tanks on inboard and centreline pylons[source] | 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] |
|---|
| Guns | 2× 30 mm (1.181 in) calibre DEFA cannon with up to 150 rounds/gun[source] | 3 × 12.7 mm (0.5 in) Browning AN/M3 machine guns[source] |
|---|
| Hardpoints | 7 (4× under-wing, 2× over-wing and 1× centreline) with a capacity of 10,000 lb (4,500 kg), with provisions to carry combinations of: Rockets: 8× Matra rocket pods with 18× SNEB 68 mm rockets each Missiles: Air-to-air missiles : 2× AIM-9 Sidewinder on outboard pylons ( French Air and Space Force ) or 2× AIM-9 Sidewinder on overwing pylons 2× R.550 Magic on outboard pylons ( French Air and Space Force ) ASRAAM ( Indian Air Force ) Astra ( Indian Air Force ) Air-to-surface missiles : AS-30L ( French Air and Space Force ) Rampage ( Indian Air Force ) Anti-ship missiles : Harpoon ( Indian Air Force ) Sea Eagle ( Indian Air Force ) Anti-radiation missiles : AS.37 Martel Rudram-1 ( Indian Air Force ) Precision-guided munition : Smart Anti-Airfield Weapon ( Indian Air Force ) Bombs: various unguided or laser-guided bombs Nuclear bombs : 2× WE177 A nuclear bombs 1× AN-52 nuclear bomb ( French Air and Space Force ) Other: external drop tanks for extended range/loitering time.[source] | 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] |
|---|
| Aspect ratio | 3.12[source] | — |
|---|
| g limits | +8.6 (ultimate load +12)[source] | +8 -4[source] |
|---|
| Time to altitude | 9,145 m (30,003 ft) in 1 minute 30 seconds[source] | — |
|---|
| Wing loading | 649.3 kg/m 2 (133.0 lb/sq ft) maximum[source] | — |
|---|
| Thrust/weight | Adour Mk.102: 0.422[source] | — |
|---|
| Take-off run | 580 m (1,900 ft) with typical tactical load[source] | — |
|---|
| Take-off run to 15 m (49 ft) | 940 m (3,080 ft) with typical tactical load[source] | — |
|---|
| Landing run from 15 m (49 ft) | 785 m (2,575 ft) with typical tactical load[source] | — |
|---|
| Landing run | 470 m (1,540 ft) with typical tactical load[source] | — |
|---|
| Landing speed | 213 km/h (132 mph; 115 kn)[source] | — |
|---|
| Rockets | 8× Matra rocket pods with 18× SNEB 68 mm rockets each[source] | 6 × VRZ-157 127 mm (5.00 in) rockets[source] |
|---|
| Missiles | Air-to-air missiles : 2× AIM-9 Sidewinder on outboard pylons ( French Air and Space Force ) or 2× AIM-9 Sidewinder on overwing pylons 2× R.550 Magic on outboard pylons ( French Air and Space Force ) ASRAAM ( Indian Air Force ) Astra ( Indian Air Force ) Air-to-surface missiles : AS-30L ( French Air and Space Force ) Rampage ( Indian Air Force ) Anti-ship missiles : Harpoon ( Indian Air Force ) Sea Eagle ( Indian Air Force ) Anti-radiation missiles : AS.37 Martel Rudram-1 ( Indian Air Force ) Precision-guided munition : Smart Anti-Airfield Weapon ( Indian Air Force )[source] | — |
|---|
| Bombs | various unguided or laser-guided bombs Nuclear bombs : 2× WE177 A nuclear bombs 1× AN-52 nuclear bomb ( French Air and Space Force )[source] | — |
|---|
| Other | external drop tanks for extended range/loitering time.[source] | — |
|---|
| Designer | — | Aeronautical Technical Institute (ATI)[source] |
|---|
| Primary user | — | Yugoslav Air Force[source] |
|---|
| Developed from | — | Soko G-2 Galeb[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 |
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| Role | — | Yugoslav single-seat, single-engined, light attack aircraft ,[source] |
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| Country of origin | — | Yugoslavia[source]Inventory Origin column; table 1, row 6, cell 2; revision 1376096397 |
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