An open architecture avionics suite installed on the Yak-130 allows a wide range of western weapon systems and guided missiles to be integrated including the AIM-9L Sidewinder, Magic 2 and the AGM-65 Maverick. Weapons fits include the Vikhr laser-guided missile, R-73 infrared-guided air-to-air missiles (NATO designation AA-11 Archer) and the Kh-25 ML (NATO designation AS-10 Karen) air-to-surface laser-guided missile. A Platan electro-optical guidance pod is installed under the fuselage for deployment of the KAB-500Kr guided bomb.
AIM-9L Sidewinder
af.mil
The Sidewinder is the most widespread Air-to-Air missile in the world; its first version, the AIM-9B, entered service in 1953 and since then it has been continuously updated up to the latest versions AIM-9L and AIM-9M and it boasts many imitation attempts, like the Russian AA-2 “Atoll” or the Israeli Rafael “Shafrir 2”.
It features four detachable double-delta control surfaces behind the nose and a roll stabilizing rear wing/rolleron assembly. The main components of the missiles are an infrared homing guidance system with “all aspect” capability, an explosive/fragmentation warhead weighting about 10 Kg and an active optical target detector. According to the avionic system of the carrier aircraft, the missile can be fired in two modes:
- “Boresight Mode”: IR seeker slaved to the aircraft weapon aiming system
- “Scan Mode”: IR seeker performs autonomous scanning
Technical specification
LENGTH: | 2.87 m |
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DIAMETER: | 127 mm |
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WING SPAN: | 0.64 m |
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WEIGHT: | 87 Kg |
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WARHEAD: | 9.5 Kg HE/fragmentation |
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FUZE: | Active Laser |
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GUIDANCE: | IR |
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PROPULSION SYS.: | Rocket motor, solid propellant |
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RANGE: | 8 Km |
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Source nibbio14.altervista.org
Magic 2 (R-550)
Magic 2 missile
Magic R550 -“All aspect” medium-range missile, developed in 1967 by Matra and entered service in 1974. Advanced aerodynamic characteristics, thanks to moving control fins near the nozzle, in combination with four aerodynamic vanes which serve to stabilize the flow for better control.
LAUNCH-PLATFORM | Mirage 2000, Rafale, F-16, Sea Harrier, Mirage 5, Super Etendard, Mirage F1, Mirage III |
DESIGNER | Marta, MBDA |
COUNTRY | France |
IN SERVICE | 1975 (Magic)
1986 (Magic II) |
TYPE | Short-range air-to-air missile |
POWER PLANT | Rocket motor |
Thrust, kN | – |
DIMENSIONS | |
Length, mm | 2750 |
Diameter, mm | 160 |
Wing span, mm | 470 |
WEIGHT | |
Weight, kg | 89 |
Warhead weight, kg | 30 |
Warhead type | Fragmentation |
GUIDANCE SYSTEM | IR |
PERFORMANCE | |
Speed, (Mach) | 4 |
Range, km | 15 |
AGM-65 Maverick
AGM-65 Maverick
Vikhr laser-guided missile
turbosquid.com
The 9A4172 Vikhr is a Russian long-range anti-tank guided missile. It is known in the West as the AT-16 Scallion. It was developed in the Soviet Union during the 1980s. At the time Soviets needed a new missiles, to replace the 9K114 Shturm (AT-6 Spiral) system, that could penetrate contemporary Western main battle tanks with composite and explosive reactive armor, such as the American
M1 Abrams, German
Leopard 2, and British
Challenger. Prototypes were tested by the Soviet armed forces in 1989. First production missiles were delivered in 1992. During the same year the Vikhr was first publicly revealed. Since its introduction sales of the Vikhr missile have been slow, partly because Russia also uses
Ataka missile, developed by another manufacturer, which is similar in function, but uses different guidance. In 2013 Russian MoD ordered over 6 000 Vikhr-1 missiles in order to prevent the manufacturer from going bankrupt. Delivery was completed in 2016. The Vikhr has been exported to Egypt, and possibly some countries.
Launchers with the Vikhr missiles can be mounted on helicopters, vehicles and watercraft. This missile is typically used on Russian helicopters, such as the
Ka-52, and
Su-25T ground attack aircraft. However much more numerous Russian Mil attack helicopters, such as the
Mi-24 and
Mi-28 are typically equipped with broadly similar
Ataka anti-tank missiles.
The Vikhr missiles are used in conjunction with APU-6 and APU-8 aviation launchers. The APU-6 launcher carries 6 missiles and is used on the Ka-50 helicopters. The APU-8 launcher carries 8 missiles and is used on the Su-25T ground attack aircraft.
Country of origin | Russia |
Entered service | 1992 |
Missile | |
Armor penetration | 1 000 mm behind ERA |
Missile length | 2.75 m |
Missile diameter | 0.13 m |
Fin span | 0.38 m |
Missile launch weight | 45 kg |
Warhead weight | 10 – 12 kg |
Warhead type | Tandem HEAT |
Range of fire | up to 10 km |
Guidance | Laser-guided |
R-73 infrared-guided air-to-air missiles (NATO designation AA-11 Archer)
military.wikia.org
The R-73 short-range air-to-air missile was developed by “Molniya” (recently the special design bureau Nr.4) design bureau. It’s team at the beginning of the 1970s developed the R-60 missile and the R-73 was intended to replace it. It is known as the AA-11 “Archer” with NATO countries.
Missile features a wide angle infrared seeker and extreme maneuverability.
The R-73 is completed with a vectored trust system to makevery tight turns. It’s minimum range of fire is 0.3 km and missile is intended as a dogfight weapon in close air combats. Furthermore the R-73 is considered to be the most dangerous weapon system in close visual combat.
There were developed later variants of the R-73 missile:
– The R-73E missile features extended range;
– The R-73M1 (sometimes designated as R-73 RDM-1) features improved overall performance;
– The R-73M2 (R-73 RDM-2) has even better performance characteristics than it’s predecessor – the R-73M1;
– The K-74ME.
All these missiles have the same AA-11 “Archer” NATO designation.
Model | R-73E | R-73M1 | R-73M2 |
Entered service in | ? | 1982 | ? |
Range against closing target | < 30 km | 30 km | 40 km |
Range against receding target | < 15 km | 15 km | ? |
Weight | 115 kg | 105 kg | 110 kg |
Weight of warhead | 7.4 kg | 8 kg | ? |
Type of warhead | expanding rod | | |
Speed | Mach 2.5 | | |
Guidance | infrared | | |
Kill probability | ? | 0.6 | ? |
Length | 2.9 m | | |
Diameter | 0.17 m | | |
Fin span | 0.51 m | | |
Carried by | Ka-50, Ka-52, MiG-29, MiG-31, Su-25, Su-27, Su-30, Su-33, Su-34, Su-35, Su-37, Su-39, Yak-141 | | |
Kh-25 ML (NATO designation AS-10 Karen) air-to-surface laser-guided missile
The Kh-25/Kh-25M (Russian: Х-25; NATO:AS-10 ‘Karen‘) is a family of Soviet lightweight air-to-ground missiles with a modular range of guidance systems and a range of 10 km. The anti-radar variant (Kh-25MP) is known to NATO as the AS-12 ‘Kegler‘ and has a range up to 40 km.Designed by Zvezda-Strela, the Kh-25 is derived from the laser-guided version of their Kh-23 Grom (AS-7 ‘Kerry’). It has now been succeeded by the Kh-38 family, but the Kh-25 remains in widespread use.
The Kh-25 is very similar to the later version of the Kh-23, with cruciform canards and fins.
The Kh-25MP has two versions of its homing head, 1VP and 2VP, sensitive to different frequencies.
The original Kh-25 entered service with the Soviet Air Force between 1973-5, equipping the Mikoyan-Gurevich MiG-23, MiG-27 and Sukhoi Su-17M. Since then it has been cleared for use on the MiG-21, MiG-29, Sukhoi Su-17/20/22 family, Sukhoi Su-24, Su-25 and Su-27. It can also be carried by attack helicopters such as the Kamov Ka-50.
Kh-25ML – semi-active laser guidance with tandem warhead that can penetrate 1 metre (39 in) of concrete.
Specifications | |
Weight | Kh-25ML :299 kg (659 lb)
Kh-25MP :315 kg (694 lb) |
Length | Kh-25ML :370.5 cm (12 ft 2 in)
Kh-25MP 1VP :425.5 cm (167.5 in)
Kh-25MP 2VP :435.5 cm (171.5 in) |
Diameter | 27.5 cm (10.8 in) |
Warhead | High explosive, shell-forming |
Warhead weight | Kh-25MP :89.6 kg (198 lb), Kh-25MR :140 kg (309 lb) |
| |
Wingspan | 75.5 cm (29.7 in) |
Operational
range | Kh-25ML :11 km (5.9 nmi)
Kh-25MP :up to 60 km (32 nmi)
Kh-25MTP : 20 km (11 nmi) |
Speed | Kh-25ML :1,370–2,410 km/h (850–1,500 mph)
Kh-25MP :1,080–1,620 km/h (670–1,000 mph) |
Guidance
system | Laser guidance, passive radar, TV guidance, IIR, Satellite guidance,active radar homing depending on variant |
Launch
platform | MiG-21, MiG-23/27, MiG-29, Ka-52 , Su-17/20/22, Su-24,Su-25, Su-27, Yakovlev Yak-130
Kh-25MP : MiG-23/27, Su-17/22, Su-24, Su-25 |
KAB-500Kr guided bomb
The KAB-500Kr corrected air bomb is designed to engage stationary ground/surface small-sized hardened targets, such as reinforced concrete shelters, runways, railway and highway bridges, military industrial installations, warships, and transport vessels.
KAB-500Kr
Weights: total/warhead/HE, kg | 520/380/100 |
Dimensions: | |
length, m | 3,05 |
diameter, m | 0,35 |
empennage, m | 0,75 |
| |
Bomb drop altitude, km | 0,5-5 |
Carrier speed, km/h | 550…1100 |
Root mean square deviation, m | 4…7 |
Warhead type | concrete-piercing |
| (high explosive penetrator) |
| |
The aircraft is fitted with a 30mm GSh-301 cannon or a podded GSh-23 cannon installed under the fuselage. It can also deploy unguided B-8M and B-18 rockets, 250kg and 50kg bombs and cluster bombs.
B-8M rocket pod
Wikimedia Commons
rocket pods B-8M1
– length: 2 760 mm
– body diameter: 520 mm
– the weight of the empty rocket pods: 160 kg
– the number of portable missiles: 20
– carrier: aircraft
Source armedconflicts.com
‘S-8’ 80mm unguided rocket
The S-8 system is the main caliber weapon in the class of unguided aircraft rockets and can solve a variety of aircraft missions.
The rocket is provided with a solid propellant motor with a summary thrust pulse of 5,800 N.s and operating time of 0.7 s. Progressive methods for body shaping from ready-made rolled aluminum and unique engineering solutions in terms of separate elements aimed at reducing motor manufacturing labor consumption and costs are used in its construction.
The following types of S-8 rockets are operational today:
- S-8KOM with HEAT fragmentation warhead;
- S-8BM with concrete-piercing (penetrating) warhead;
- S-8-OM with illuminating warhead.
B-13 Rocket pod
KAB-500Kr guided bomb and B-13 Rocket pod
‘S-13’ type 122mm unguided rocket
The
S-13 is a 122 mm calibre unguided rocket weapon developed by the Soviet Air Force for use by military aircraft. It remains in service with the Russian Air Force and some other countries.
S-13T: Tandem HEAT, range 1.1 – 4 km Combined penetration of 6 m of earth and 1 m of reinforced concrete. Velocity 500 m/s.
S-13T
S-13OF: The only 122mm rocket available, this large rocket packs a blast-fragmentation warhead with some serious wallop, dealing significant damage to soft targets and lightly armored vehicles, and can even destroy a main battle tank with a direct hit. With only 5 rockets per pod, accurate delivery is key.
The S-13OF
30mm GSh-301 cannon
30mm GSh-301 cannon
The GSh-301 is a modern Soviet single barrel autocannon with a high rate of fire. It arms the two most common types of Soviet multirole fighters, the MiG-29 and the larger Su-27.
The GSh-301 fires the 30x165mm round at a rate of fire of 1.500 to 1.800 rpm. Short bursts are fired. A 100 round burst destroys the barrel. Effective range is quoted as 200 to 800 m against aerial targets and 1.200 to 1.800 m against ground targets. Combined with targeting computer and laser range finder accuracy is reported to be good.
Type | Autocannon |
Caliber | 30x165mm Soviet |
Mechanism | Short recoil operated |
Barrel | 1.500 m barrel |
Dimensions | 1.978 m long, 156 mm wide, 185 mm tall |
Weight | 46 kg |
Feeding | Single belt feed |
Rate of fire | 1.500 – 1.800 rpm |
Muzzle velocity | 860 m/s |
Recoil | ? |
Remarks | 2.000 round barrel life |
Source weaponsystems.net
GSh-23 cannon gun pod
The GSh-23 functions on the Gast principle. In this twin barrel setup the recoil from one barrel cycles the action of the other, allowing for an instant high rate of fire. The GSh-23 is belt fed from a single belt. The GSh-23L adds a muzzle brake that helps reduce recoil. Both GSh-23 and GSh-23L are solenoid fired.
The GSh-23 fires the 23x115mm round that is also widely used in other Soviet aircraft cannon. The rate of fire is 3.000 to 3.400 rpm and is instantly achieved as opposed to Gatling type weapons. The muzzle velocity of 715 m/s is low compared to other modern aircraft cannon.
Type | Autocannon |
Caliber | 23x115mm AM-23 |
Mechanism | Gas operated, Gast principle |
Barrel | Twin barrel, 1.000 m, rifled, 10 grooves, 575 mm right hand twist |
Dimensions | 1.387 m long, 165 mm wide, 168 mm tall |
Weight | 50 kg |
Feeding | Single belt feed |
Rate of fire | 3.000 – 3.400 rpm |
Muzzle velocity | 700 – 730 m/s |
Recoil | 2.900 kg recoil force |
Remarks | Muzzle brake |
RADAR
The Yak-130 is fitted with the 8GHz to 12.5GHz Osa or Oca (Wasp) radar developed by NIIP Zhukovsky. The radar has the capacity to track eight airborne targets simultaneously, simultaneously engage four targets at all angles and simultaneously track two ground targets. The detection range against 5m² cross section targets is 40km in the rear direction and 85km in the forward direction. The lock-on range for operation in automatic tracking mode is 65km.