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NATO Codename SA - 16
| Type | "Surface - to - Air" |
| Crew | 1 - 2 |
| Entered service in | 1983 |
| Missiles characteristics | |
| Number of missiles | 1 |
| Missiles weight | 10.6 kg |
| Missiles length | 1.6 m |
| Warheads weight | 1.15 kg |
| Maximum target's speed | 700 km/h |
| Maximum firing range | 5.2 km |
| Minimum firing range | 0.5 km |
| Maximum target's altitude | 3.5 km |
| Minimum target's altitude | 10 m |
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9M39 "Igla" portable air defense complex entered
service in USSR Armed Forces in 1983. It is intended to fight against low
flying air targets in good visibility conditions. "Igla" is battalions
and lower subdivisions or tactical groups frontline air defense complex.
In NATO countries it is known as SA - 16.
Complex contains
anti-aircraft g Complex control elements are mounted in the handle. There is also placed identification antenna. Whole indentification system consists from request receiver, antenna and electrical supply source. Anti-aircraft guided missile "Igla" has "duck" aerodynamic scheme fitted with solid fuel engine. Missile has infrared guidance warhead. Warhead is fitted with logical selection device which ignores active countermeasures and infrared traps. Missile is launched using initial start engine which separates after leaving loading device. Launching device consists from launching tube and electrical supply source. Launching tube serves as missile carrying and transporting container. "Igla" is fitted with dioptrical sight which is used to notice and to track target. It is used to find range target's and to insert overtaking angle. Sights body has indicator signalizing when target is intercepted by guided warhead. "Igla" portable air defense missile complex is used on helicopters as an air - to - air missile as well. Usually missiles in launching devices are hanged by two or four on helicopter's hardpoints. A number of missiles depends from combat mission.
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