Military Wiki
9K31 Strela-1
(NATO reporting name: SA-9 Gaskin)
Soviet SA-9 Gaskin.jpg
9K31 transporter erector launcher
Type Vehicle-mounted SAM system
Place of origin Soviet Union
Service history
In service 1968-present
Used by See list of operators
Wars Arab-Israeli Wars, Western Sahara War, Yugoslav wars, Lebanon wars, Iran-Iraq war, 2003 invasion of Iraq[1]
Production history
Designer OKB-16 design bureau (now the Moscow-based KB Tochmash Design Bureau of Precision Engineering)
Manufacturer Soviet state factories
Produced 1966
Variants 9K31, CA-95[2]
Specifications (9K31 Strela-1[3])
Weight 7,000 kg
Length 5.8 m
Width 2.4 m
Height 2.3 m (travelling)
Crew 3 (commander, gunner and driver)

Armour 5-14 mm
4 x 9M31 (or 9M31M)
Engine GAZ 41 V-8 water-cooled petrol
140 hp at 3,400 rpm
Power/weight 20 hp/t
Ground clearance 0.43 m
Fuel capacity 290 litres
750 km
Speed 100 km/h (road)
10 km/h (water)

The 9K31 Strela-1 (Russian: 9К31 «Стрела-1»; English: arrow) is a highly mobile, short-range, low altitude infra-red guided surface-to-air missile system. Originally developed by the Soviet Union under the GRAU designation 9K31, it is commonly known by its NATO reporting name, SA-9 "Gaskin". The system consists of a BRDM-2 amphibious vehicle, mounting two pairs of ready-to-fire 9M31 missiles.

Development History

The missiles used in this system were developed alongside the ubiquitous Russian MANPADS 9K32M "Strela-2" (NATO designation SA-7 "Grail") in the 1960s. At first both missiles were intended to be man-portable systems, but as it became obvious that Strela-2 would be far more compact of the two system, the development goals of Strela-1 were changed. Instead of a battalion-level man-portable system the new criteria called for a regimental vehicle-mounted SAM to support the ZSU-23-4. As a result of the change in role and more relaxed weight limits of a vehicle-mounted SAM, the design team made the 9M31 a much heavier missile, which permitted fewer design compromises than in the case of Strela-2 to achieve acceptable kinematic performance. The most notable difference is the much larger diameter of the missile and a blunt seeker head that occupies the full width of the missile body. With all else being equal, the ability of an optical seeker to detect a target is directly proportional to its diameter, but on the other hand aerodynamic drag increases proportionally to the square of the diameter. The Strela-1 also had a warhead over twice as heavy, a proximity fuze and more effective control surface configuration to provide better maneuverability at the cost of increased drag. The net result was a missile four times the weight of Strela-2, with only slightly longer reach but otherwise of much better performance.


Each TEL carries four ready-to fire missiles, but typically no missiles for reloading. Reloading is performed manually and usually takes approximately 5 minutes. The missile boxes are lowered for transport to lower the total height of the vehicle. The driver and commander have periscopes for viewing outside the vehicle when the hatches are closed.


9K31 TEL w/"Flat Box" passive radar detection array. Photo by GulfLINK.

Apart from the new turret, the other major change to the BRDM-2 chassis is the removal of the belly wheels (which are presumably to improve off-road performance). The driver and commander both have infra-red vision systems. The vehicle has standard NBC (Nuclear, Biological and Chemical) protection including overpressure. The missiles fold down to the sides of the turret which greatly reduces the height of the vehicle whilst travelling. Each vehicle weighs around 7 tonnes (7.7 short tons) and has a 104 kW (140 hp) engine and a central tire pressure control system.

Missiles and guidance


According to a number of Russian sources the original 9M31 (US DoD designation SA-9A "Gaskin-Mod0") had a zone of reliable target destruction from 900 to 4200 metres. Several western and also some Russian sources give much higher range estimates of 800 to 6500 m (0.5 to 4 miles); these may refer to maximum firing range against an approaching target and minimum against receding, which are obviously larger envelopes as the target only has to reach the intercept zone by the time the missile would reach it.

The missile is effective against targets receding at a maximum speed of 220 m/s, or approaching at 310 m/s.

Type Surface-to-air missile
Place of origin Soviet Union
Production history
Variants 9M31, 9M31M
Specifications (9M31 [5])
Weight 32 kg
Length 1803 mm
Diameter 120 mm

Warhead Frag-HE
Warhead weight 2.6 kg
RF Proximity

Wingspan 0.36 m[3]
Propellant single-stage solid propellant rocket motor
4,200 metres (2.6 mi)[4] (sometimes reported also as 6.5 kilometres (4.0 mi) for 9M31, 8 kilometres (5.0 mi) for the 9M31M.)
Flight altitude 3,500 metres (11,500 ft) (some sources give also higher figures)
Speed Mach 1.8
photocontrast PbS seeker.[4] (sometimes reported also as IR seeker of 1-3 μm and/or 1-5 μm wavelength);

The warhead was primarily intended to impact the target directly, and had contact and magnetic fuzes, but also contained a back-up optical proximity fuze to detonate the warhead in case of a near miss. The missile also had an unusual safety mechanism in case of a miss; rather than a self-destruct fuze, if the optical fuze didn't detect a target within 13...16 seconds, the warhead safety mechanism would be engaged to prevent its detonation upon impact. Propulsion is by a single-stage solid fuel rocket motor, which is ignited at a distance of few meters from the launch tube: as the throw-out charge ejects the missile from its canister, it is trailing a wire from its rear. The main rocket ignites when missile reaches the wire's end at a few metres distance, and is cut off from it.

The seeker head is an unusual construction, using uncooled lead sulphide (PbS) detector elements, but with an unusual tracking mechanism. Uncooled PbS elements are commonly used to detect radiation at only short wavelengths of less than 2 micrometers. Only very hot objects emit strongly at such short wavelengths, limiting heat-seeking systems using uncooled PbS detector elements to rear-hemisphere engagements against jet targets, although propeller-driven aircraft and helicopters can of course be engaged from any direction from which the exhaust or other very hot parts of the engine are visible.

The seeker head of 9M31, however, utilizes the PbS elements differently from usual. Taking advantage of the fact that the clear sky gives strong and constant background emission at below 2 micrometer range, peaking at visual light (0.4 to 0.7 micrometer) wavelengths at which PbS in 295 kelvins temperature still provides a response, the seeker head is used to track a change of radiation from the target compared to the background. The method is called optical photocontrast homing (Rus.: фотоконтрастное наведение). The advantage of photocontrast homing method over traditional heat-seeking homing heads using PbS elements is that it negates the most serious drawback of early-generation IR-homing missiles: complete lack of front-aspect engagement capability against approaching jets. Even early cooled seeker heads had usually only limited forward hemisphere engagement abilities, often reducing to zero in case of jets approaching exactly towards the shooter.

The new photo-contrast seeker had its own serious limits also, however, which came in the form of rather strict meteorological conditions that had to be met in order to enable the seeker to detect and track the target: it could only engage targets against background conditions of either clear sky or solid overcast, minimum of 20 degrees away from the sun, and at least 2 degrees above horizon. Nonetheless, following a study of battlefield conditions and aircraft tactics in past conflicts where short-range air defences had been used, it was concluded that conditions allowing the use of such homing system were common enough to make it a cost-effective design choice and a better trade-off than the only practical alternative available at the time, which was infrared homing restricted to rear-hemisphere engagements.

No doubt the fact that Strela-1 would be supplemented by IR-homing Strela-2 and radar-controlled ZSU-23-4 self-propelled AA gun system may have influenced the decision in favour of such an unusual homing system. The main advantage the choice was that it made Strela-1 the only ADA system in the Soviet tank or motor rifle regiment that could engage approaching targets out to a range of several kilometers - the ZSU being hampered by very short range, and Strela-2 by its limitation to tail-chase engagements of ground attack jets, after the jet had already delivered its attack.


While the 9M31 was accepted to service after state trials in 1968, the trials committee also suggested improvements that should be incorporated into the weapon as soon as possible. As a result of these improvements the 9M31M "Strela-1M" (US DoD designation SA-9B "Gaskin-Mod0") entered service in 1970.

The new version introduced many slight improvements in performance characteristics of the missile: it had a slightly heavier warhead, more accurate guidance system to increase the probability of direct impacts, and extended range. Range is again reported to be as high as 8000 m (0.35 to 5 miles) in a number of western and also a few Russian sources, whereas for example Petukhov & Shestov, Lappi, and a number Russian web sources give much more modest performance figures; considering the performance of similar systems, at least an intercept range of 8000 m seems unlikely for such a small, high-drag missile design.


The Strela-1 was deployed in short-range air defence batteries of Soviet motor rifle and tank regiments. The battery consisted of a gun platoon of four ZSU-23-4 Shilkas, and a SAM platoon with four Strela-1 vehicles. The Strela-1 platoon contains, in addition to a command vehicle, one TEL fitted with a passive radar detection system similar to a Radar Warning Receiver, and several more (usually three) without any radar system. The radar detection system is the 9S16 "Flat Box" and consists of four sensors mounted around the BRDM vehicle giving it 360 degree coverage. This system emits no radar energy but can detect radio waves emitted from aircraft, giving the vehicle warning about incoming aircraft and aiding in the acquisition of the target aircraft with the optical system. Typical tactics call for the launch of two missiles against each target to improve the chance of destroying it.

In Russia, the 9K31 Strela-1 system was superseded by the 9K35 Strela-10.


Croatian 9K31.

Missile launch of a Romanian CA-95 (licensed built 9K31 Strela-1 using a TABC-79 vehicle instead of a BRDM-2).

  •  Algeria - 46[6]
  •  Angola
  •  Armenia
  •  Benin - 4[3]
  •  Bulgaria - 50,[3] to be phased out
  •  Cuba - 60[3]
  •  Croatia
  •  Bosnia and Herzegovina 34 + (5)
  •  Egypt - 20
  •  Ethiopia
  •  Hungary - 28
  •  India - 400[3]
  •  Libya - 60[3]
  •  Mauritania - 4[3]
  •  Mongolia - unknown number[7]
  •  Mozambique
  •  Nicaragua
  •  Poland
  •  Romania - 48 produced under license as CA-95.
  •  Sahrawi Arab Democratic Republic
  •  Serbia - 30 + 220 (in reserve)
  •  Syria
  •  Uganda
  •  Ukraine
  •  Uzbekistan
  •  Vietnam
  •  Yemen

Former Operators

  •  Czechoslovakia
  •  FR Yugoslavia
  •  Iraq
  •  Slovenia
  •  Russia
  •  Soviet Union

See also


This page uses Creative Commons Licensed content from Wikipedia (view authors).