SS.12/AS.12

"AS.12" redirects here. For other uses, see AS.12 (disambiguation).
NORD SS.12/AS.12

An AS.12
Type surface-to-surface or air-to-surface missile
Place of origin France
Service history
In service 1960-
Production history
Produced 1957-1982
Number built 10000+
Specifications
Weight 76 kg
Length 1.87 m
Diameter 180 mm (body) 210 mm (warhead)
Warhead 28 kg
Engine solid fuel rocket
Wingspan 650 mm
Operational
range
 7000/8000 m
Speed 370 km/h
Guidance
system
 wire MCLOS
Steering
system
 thrust deflection
Launch
platform
 Helicopter, aircraft, ground unit
External images
Aérospatiale SS.12/AS.12
AS.12(M)fitted Alouette III
AS.12(M) fired from French Navy LYNX
SS.12(M) fired from small patrol boat
AS.12(M) French Navy Alouette III
Manufacture's Fact Sheet

The SS.12 and AS.12 are two variants of the same missile: SS for surface-to-surface and AS for air-to-surface. It was designed in 1955-1957 by Nord Aviation, later Aérospatiale. It was a derivative of the NORD SS-10 and SS-11 missiles which were surface-to-surface wire-guided missiles for use by infantry, vehicle or a helicopter primarily in the anti-tank role, but also anti-material, anti-personnel and against light field fortifications. The SS.12/AS.12 was basically an scaled-up version of the SS.11/AS.11 with a massive increase in range and warhead weight. The SS.12/AS.12 original mission was primarily to be anti-shipping from naval helicopters and combat aircraft or ground launchers, and secondary for use against heavy field fortification. Its range and the destructive power of the warhead are roughly equivalent to a 5 inch artillery shell.[1]

Development

The SS.12 was originally intended to be a surface-to-surface weapon. A naval surface-to-surface version, the SS.12M was developed at the same time. Trials of the weapon began in 1956. An air-launched version, the AS.12, was trialed in 1957.[1]

Description

The missile has a distinctive bulging nose and four clipped triangular wings. The missile has two solid fuel rocket motors. One is a powerful booster rocket that burns for 2.2 seconds and the second, is a sustainer motor that burns for 28 seconds. The booster motor exhausts through two nozzles on the sides near the trailing edge of the wings [2] and the sustainer motor exhaust is located in the missile rear at the center. The wings are positioned at an angle of 1 degree to the direction of flight so that the missile spins, giving it stability. Two rearward-facing flares which ignite on launch make the missile more visible to the operator during flight. Two flares are mounted on the opposite side of the booster nozzles between the wings so as not to interfere with the two guidance wires spooling out the rear section of the missile.[3]

The missile steers using four metal vanes around the exhaust nozzle in a thrust vectoring system that directs the thrust of the sustainer motor exhaust nozzle. Steering signals are sent to the missile by means of two wires which pay out from two spools on the rear of the missile. A gas operated arming mechanism is fed from the sustainer motor, arming the warhead 7.7 seconds after launch.

The average maximum flight time of the missile is approximately 30 seconds, giving it a range of 7,000 meters[4] according to whether it is ground-launched or air-launched. Operators train using the T10K simulator, which is a simple device, that projects a beam of light on a predetermined path on a wall-mounted chart. The operator guides the light beam around the path by means of a small hand joystick, training to gain proficiency to position the beam just above the target five seconds before the end of flight then gently flying the beam, which represents the missile's flight, down on to the target for final impact.

The simulator closely resembles the missile's reaction to signal reception, which has an increasing time delay the further the missile travels.

The missile can be fitted with a three different warheads:

The semi-armour piercing warhead has a delayed action allowing it to penetrate 20 mm of armour then travel 2 meters beyond before exploding.

Service

The AS.12 originally entered service with the French Navy in 1960 in the air to surface role against ships and submarines on the surface. In 1966 the French Navy did an evaluation of the SS.11(M) and SS.12(M) from the fast patrol boat La Combattante.[1] In 1966, the Libyan Navy ordered three fast patrol boats from Vosper (Sebha, Sirte and Susa). Delivered in 1968, these were the first operational naval vessels to be armed with AS.12(M) with four launch rails on each side of the vessel's bridge.[5] The Libyan fast patrol boats proved to be a very low cost way to give long range heavy firepower to small naval vessels. Other navies soon followed Libya and bought the SS.12(M) and SS.11(M) for their light naval vessels; among them Brunei, Ethiopia, France, Greece, Ivory Coast, Senegal, and Tunisia. Sweden bought the SS.12(M) (designated the Robot 54) as a heavier support for the SS.11(M) (designated Robot 52). NORD also developed a ten missile trainable launcher for either the AS.11(M) or AS.12(M) which was sold in numbers due to its cost effective firepower.[1]

The AS.12 saw action on both sides of the 1982 Falklands War. It was fired from Westland Wasp helicopters against the Argentine submarine ARA Santa Fe. A total of nine missiles were fired at the submarine which was trapped on the surface and unable to dive after its dive tanks suffered damage from a depth charge attack by a British Royal Navy Wessex HAS.3 antisubmarine helicopter.[6] Of the missiles fired four hit, four missed and one failed to launch. Two of the missiles that hit the target failed to detonate on impact, instead punching a hole through the slender conning tower and exploding on the far side.

In an unusual mission, it was fired from a British Royal Navy Wessex Hu.5 commando helicopter at Port Stanley town hall on 11 June 1982 in an attempt to disrupt a meeting of senior Argentine personnel that took place there every morning. Both missiles that were fired missed, one striking the roof of a police station and the other hitting some telegraph poles.

Production of the SS.11/SS.12 series ceased some time in the 1980s; but in 1978 168,450 missiles had been produced.[7]

The AS.12 has been operational from the following aircraft:

Operators

See also

Notes

  1. 1 2 3 4 Bill Gunston, ROCKETS & MISSILES, page 239-240, Salamander Books Ltd 1978
  2. ↑ note - See first photo External Images
  3. ↑ not - third photo; External Images
  4. ↑ John Norris, in Anti-tank weapons, p. 45, states the SS.12 has a maximum range of 6,000 meters
  5. ↑ Jane's Fighting Ships 1976-77 page 214
  6. ↑ Falklands Air War, Chris Hobson, ISBN 1-85780-126-1, p.37
  7. ↑ FLIGHT International 15th, November 1980, page 1888

References

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