LRAC F1
| LRAC F1 | |
|---|---|
A LRAC launch tube pictured during an open day in 2009
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| Type | Shoulder-launched missile weapon |
| Place of origin | France |
| Service history | |
| Used by | France |
| Production history | |
| Designer | Société technique de recherches en industries mécaniques |
| Manufacturer | Manufacture Nationale d'Armes de Saint-Etienne the launcher and Luchaire SA the rocket projectile |
| Specifications | |
| Weight | 5 kg, with sights |
| Length | 1.17 metre |
| Crew | 2 |
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| Caliber | 89 mm |
| Rate of fire | 3 to 4 rounds per minute |
| Muzzle velocity | 295 m/s |
| Effective firing range | 300 to 500 metres |
| Maximum firing range | 2300 m (at 45° angle) |
| Sights | APX M 290 and passive night telescope |
The LRAC F1, officially called Lance-Roquettes AntiChar de 89 mm modèle F1 (89 mm anti-tank rocket launcher model F1) is a French reusable rocket launcher developed by Luchaire Défense SA, and manufactured in cooperation with Manufacture Nationale d'Armes de Saint-Étienne and was in the 1970s marketed by Hotchkiss-Brandt. It replaced the 89 mm M20A1 Super Bazooka in French Army service. Through the use of fiberglass and plastic in the launcher it is over 2 kg lighter when loaded than the M20A1 while having a greater effective range. The LRAC FI is sometimes referred to as the STRIM 89mm antitank rocket launcher from the abbreviations for the private firm Société technique de recherches en industries mécaniques that was contracted in 1964 by the French Ministry of Defence, to research a replacement for the M20A1 Super Bazooka. In the early 1970s, two antitank weapons were placed in production for evaluation by the French Army to replace the M20A1: the 80mm ACL-APX, a recoilless cannon with a rocket assist projectile, and the 89mm LRAC F1 STRIM 89mm rocket launcher. The STRIM design was chosen as the replacement for the M20A1 based on its higher penetration ability of its antitank ammunition and the much lower over all manufacturing costs compared to the 80mm ACL-APX system.
The launcher is normally operated by a crew of two, a loader and a gunner. The launcher is loaded by attaching a rocket container to the rear of the launcher. When the container is attached, the electrical firing circuit is connected. The rocket container is 626 millimetres long and weighs approximately 3.2 kilograms. On the left side of the launcher is the 3× APX M 309 optical sight, which is graduated between 100 and 1,000 metres. The launcher has a shoulder rest and forward pistol grip, both of which may be adjusted to suit the firer. The forward pistol grip contains a mechanical safety switch and the firing mechanism. When the safety is off, pulling the trigger generates a charge which fires the rocket.
The watertight rear plug of the rocket container is removed just before firing, which closes the firing circuit and allows the rocket to be fired. The rocket is propelled by a large number of long sticks of tubular propellant that produce a constant pressure while burning, providing constant acceleration. The engine burns out before the rocket leaves the launcher at a velocity of approximately 300 metres per second. As soon as the rocket leaves the launcher, nine fins fold backwards from the rear. These fins provide stability for the rocket while it is in flight. There are two safeties. The first is a bore-riding pin located mid-body of the projectile that blocks the warhead firing circuit. After the projectile leaves the tube, the bore-riding pin falls out releasing the second safety which prevents detonation until the rocket has traveled at least 10 metres from the launcher. The rocket reaches a range of 330 metres in about 1.25 seconds, and 360 metres in 1.36 seconds.
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Wikipedia