GB2126320A - Recoilless ammunition - Google Patents

Abstract

A round of ammunition for a recoilless projectile launcher of the type employing a launch tube (1) which is open at both ends comprises a projectile (2) and a countermass or breach-plug (3) which are connected together to hold between them a propulsive charge or cartridge (4). The projectile and the countermass are connected by a number of small rigid linking rods (7) of low mass and a high ballistic coefficient, one end (71) of each rod being fixed to the casing (32) of the countermass, and its other end (70) being attached to a retaining element (8) provided on the rear portion of the projectile (2). The retaining elements (8) are designed to shear when, during launching of the projectile, the tensile load exerted on them by the linking rods (7) reaches a predetermined value. <IMAGE>

Description

SPECIFICATION Ammunition for a recoilless projectile launcher The present invention relates to a round of ammuni tionfora recoilless projectile launcher of the type having a launch tube which is open at both ends, the round comprising a projectile, a propulsive charge behind the projectile, and a countermass which is located behind the propulsive charge and which is connected to the projectile, at least when the round is loaded into the launch tube.

Recoilless projectile launchers ofthetype employing launch tubes which are open at both ends function in accordance with a well-known principle.

When the propulsive charge, which is located in the launch tube between the projectile and the countermass, is ignited, the pressure of the gases which are generated by its combustion propels the projectile and the countermass, which forms a mobile breachplug, in opposite directions.

In ordertofacilitatethe operation of loading into the launch tube the round of ammunition formed by the projectile,the propulsive charge, and the countermass, it is known to interconnect the projectile and the countermass with the aid of suitable linking means. In addition to holding the round togetherwhile loading, this linking means must be capable of preventing the two mobile components (the projectile and countermass) from moving until the pressure in the tube generated by the combustion of the charge reaches a certain value, which is termed the forcing pressure.

Also the linking means should be capable of permitting the two mobile components to separate easily when the forcing pressure has been reached,and it must not constitute a hazard to the users ofthe weapon when ejected with the countermass from the rearendofthe launch tube.

Various linking means are known, such as a linking collar which encircles the propulsive charge and rigidly interconnects the projectile and the countermass, but none allows all of the above conditions to be met atthe same time.

The present invention aims to provide an improved linking means whereby a round of ammunition of the kind described can be produced which is extremely easy to load, guarantees that the projectile and the countermass are immobiiised in the launch tube until the forcing pressure is reached, and ensures that the weapon crew can use the weapon in safety.

According to the invention therefore, in a round of ammunition ofthe kind described, the countermass is connected to the projectile by linking means comprising a number of small rigid rods of low mass and a high ballistic coefficient, the linking rods being fixed at one end to the countermass in its peripheral region and attached at the other end to retaining elements on the rear portion ofthe projectile,the retaining elements being designed to shear when, during launching ofthe projectile, the tensile load exerted on them bythe linking rods exceeds a predetermined value.

The linking rods are preferably composed of fibres which possess a high Young's modulus, such as glass fibres, fibres of a material which is known under the tradename Kevlar, or carbon fibres, and which are rendered rigid with the aid of a resin.

The linking rods are preferably fixed to the countermass by means of an adhesive, or by being incorporated directly into the body of the casing ofthe countermass.

In a preferred embodiment of the invention the retaining elements are pins which are integral with the body of the projectile, and the ends of the linking rods which are attached thereto are formed as loops which fit over the pins.

The retaining elements,which arepreferablyintegral with the rear portion of the projectile, may be mounted on fairingswhich are integral with the body ofthe projectile at its rear end and which pivotally supportfinsforming a tail assembly ofthe projectile.

According to another special feature, the round of ammunition in accordance with the invention includes a stop ring adjacent the rear end ofthe projectile for locating the round in the launch tube, the retaining elements forthe linking bars being located in the vicinity of the stop ring.

The linking rods used in the present invention ensure that the ammunition is easy to load, while exhibiting a ragiditywhich enables them to support a compressive load. Furthermore, they enable a forcing pressure to be generated in the launch tube when the propulsive charge is ignited, and when the tensile load applied by them to the retaining elements exceeds a predetermined value, the elements shearto allowthe projectile to be propelled from the front of the launch tube and the countermass and linking rods to be expelled from the rear. However, the rods do not present any hazard when they are ejected from the rear ofthetube, duetothefactthattheir mass is low and their ballistic coefficient is high. They are thus decelerated over a short distance, immediately on leaving the tube.

One example, of a round of ammunition in accordance with the invention will now be described with reference to the accompanying drawings, in which:~ Figure 1 is a diagrammatic view illustrating the relative positions ofthe main components ofthe ammunition when loaded in the launch tube of a recoiless projectile launcher; Figure 2 is a section through a portion of a launch tube showing the round of ammunition in the tube, part of the round being broken away and shown in section to show internal details; and, Figure 3 is a cross-section along the line Ill-Ill in Figure 2.

Figure 1 represents, in a diagrammatic manner, a weapon ofthetypewhich launches a projectile, such as a rocket, without recoil from an open ended launch tube by igniting a propulsive charge between the projectile and a dispersible mobile breach-plug forming a countermass. The drawing shows a launch tube 1 ,open at both ends, containing a projectile 2 and a countermass or mobile breach-plug 3 separated by a propulsive charge 4, known as a cartridge. On burning, this cartridge generates gases, and hence a pressure in the tube 1 which propels the projectile and the mobile breach-plug in opposite directions. The nature of the cartridge 4 and the masses ofthe various components are designed such that the projectile 2 attains a desired velocity V1 atthe front end of the tube 1.The mobile breach-plug 3, which is ejected from the rear ofthe tube 1 at a velocity V2, should be rapidly decelerated on leaving the tube and must not give rise to any element capable of being dangerous outside a safety zone which is defined in accordance with the standards in forceforweapons and ammunition of this type. In orderto satisfy these requirements, the mobile breach-plug 3 is composed essentiallyofa material which can fragment.

Figure 2 shows, in a more detailed manner, a mobile breach-plug 3 comprising a casing 32 containing a ballast 31 composed, for example, of a finely-broken material. The rear end ofthe mobile breach-plug 3 is closed by means of a plate 33 which is joined to the casing 32 so that, after firing and the breach-plug 3 has emerged from the rearofthetube 1,the plate 33 separates from the casing 32 and enables the ballast 31 to disperse.

Aflexible electrical lead 53, located inside a protective tube 34, passes through the breach-plug 3 to an igniter assembly 5 located atthe centre of the cartridge4 between the breach plug 3 and the rearend ofthe projectile 2. In the embodiment illustrated, the igniter assembly 5 comprises a primer 52 and a relay charge 51.

The projectile 2 comprises a body 20 having at its rear a rocket-motor body 21 containing a propulsive charge and having a nozzle 22 for restricting the escape of the gases when the charge is ignited. The rocket-motor body 21 carries on its outside a tail assembly comprising fins 23 which are pivotally mounted on hinge-bolts 25 carried byfairings 24 which are integral with the body of the rocket-motor 21. In Figure 2, thefins 23 are shown in a folded position inside the launch tube 1, this being the position adopted while the round of ammunition is being stored. The fins pivot outwards into their operative portion when the projectile 2 is fired and leaves the tube.

The round of ammunition defined bythe projectile 2, the mobile breach-plug 3, and the cartridge 4, is immobilised inside the launch tube 1 with the aid of a ring 6, which is known as a stop-ring. This ring 6 is integral with the round, and is fixed in the tube 1 by, for example, an external collar-system 60 carrying positioning pins 61 which can be inserted radially through the tube 1 to engage the stop ring 6 (see Figure 3). The relative positions of the ring Sand ofthe projectile 2 can be defined by radial elements 62 which are integral with the ring Sand are intercalated between the fins 23 of the tail assembly of the projectile 2. By means of the positioning pins 61, the complete round of ammunition can be positioned in the launch tube 1 in a precise manner, both longitudinally and radially.

For convenience, and to ensure safe loading of the round ofammunition into the tube 1, itis desirablefor the round comprising the projectile 2, the mobile breach-plug 3, the cartridge 4, and the stop-ringS, to be assembled as a unit for insertion into the tube 1.

However, the cartridge 4 is an element without mechanical strength, and it is therefore necessary that the projectile 2 and the breach plug 3 should be connected together in a sufficiently rigid manner to transmit a compressive load and maintain the proper relative positions of the projectile 2 and the breach plug 3 during loading. The connection should also guarantee that, on firing, the projectile 2 and the breach-plug 3 will remain in place inside the launch tube 1 until the pressure between them in the tube reaches a certain value which defines a forcing pressure. The linking connection thus plays the part not only of rendering the round of ammunition rigid when it is being loaded, but also serves to create a round of ammunition oftheforcing-pressuretype.

As can be seen in Figure 2, in the round in accordance with the invention the mobile breach-plug 3 and the projectile 2 are connected by a number of linking rods 7 which are fixed to the breach-plug 3 and are hooked onto the rear end ofthe projectile 2 by means of end-loops 70 which fit around retaining pins 8 mounted on the projectile 2. The retaining pins 8 may, as shown, be provided on extensions of the fairings 24 which support the hinge-bolts 25 for the fins 23 ofthetail assembly of the projectile.

The fixing ofthe ends 71 of the linking rods 7 to the breach-plug 3 should be of the highest quality, and may be effected either by bonding the ends 71 to the casing 32 ofthe breach plug, or by integral incorporation of the rods into the body ofthe casing 32.

The essential function of the rods 7 is to hold the round together during loading and to transmit the tensile load which is necessary in orderto shearthe retaining pins 8 to break the connection between the projectile and the breach plug at the desired moment afterfiring. However,the massofthe rods7 must be very low, and their ballistic coefficient, which is defined as the ratio of the aerodynamic drag to the mass, must be high in orderto ensurethatthe rods are decelerated over a short distance after exit from the rear end ofthe launch tube 1 when the round is fired, and thus do not form dangerous projectiles. By way of example, the mass of a rod 7 may be of the order of one thousandth ofthetotal mass ofthe round of ammunition.

It is particularly advantageous to manufacture the rods 7 from a fibre-based material, comprising fibres which possess a high Young's modulus, such as carbon fibres, glass fibres, or fibres ofthe material known by the tradename Kevlar, and which have been rendered rigid with the aid of a resin.

The rods 7 are positioned around the cartridge 4 near the launch tube wall, and can easily be adapted to suit different types of projectile or different types of mobile breach-plug, since it suffices to produce, on the one hand, a connection between one end 71 ofthe rods and the breach-plug casing 32, and, on the other hand, a connection between the other end 70 ofthe rods and retaining pins 8 atthe rear of the projectile 2.

The pins 8 can be formed without difficulty and may easily be adjusted to break under a predetermined tensile load exerted by the rods 7, this load corresponding to predetermined forcing pressure depending on interior-ballistics calculations relating to the ejection of the projectile 2 and of the breach-plug 3 when the weapon is fired.

In operation, the firing command is transmitted by the electrical cable 53 to the igniter assembly 5, which initiates the combustion of the charge of powder 4.

The combustion gases generate a pressure in the combustion chamber, which is defined by the volume between the projectile 2 and the mobile breach-plug 3, and this pressure gives rise to a force which tends to separate the two components 2 and 3, which are connected bythe rods 7. Underthetensile load resulting from this force, the linking rods 7 transmit a shearing load to the retaining pins 8, and these pins break when the forcing pressure reaches the predetermined value defined bythe interior-ballistics calculations. The projectile 2 and the breach-plug 3 are then released, and are propelled from opposite ends of the tube 1 as indicated in Figure 1.

Claims (9)

1. A round of ammunition for a reciolless projectile launcher of the type having a launch tube which is open at both ends, the round comprising a projectile, a propulsive charge behind the projectile, and a coun termasswhich is behind the propulsive charge and which is connected to the projectile, at least when the round is loaded into the launch tube, by linking means comprising a number of small rigid rods of low mass and a high ballistic coefficient, the linking rods being fixed at one end to the countermass in its peripheral region and attached attheotherendto retaining elements on the rear portion of the projectile, the retaining elements being designed to shear when, during launching ofthe projectile, the tensile load exerted on them bythe linking rods exceeds a predetermined value.

2. A round of ammunition according to claim 1, in which each linking rod is composed of fibres which possess a high Young's modulus and which are resin bonded together to form the rigid rod.

3. A round of ammunition according to claim 2, in which the fibres are glass fibres or carbon fibres.

4. A round of ammunition according to any one of claims 1 to 3, in which the linking rods are fixed to the countermass by means of an adhesive.

5. A round of ammunition according to any one of claims 1 to 3, in which the linking rods are fixed to the countermass by incorporation directly into the body of the countermass casing.

6. A round of ammunition according to any one of claims 1 to 5, in which the retaining elements are pins which are integral with the body ofthe projectile, and the ends of the linking rods which are attached thereto are formed as loops which fit over pins.

7. A round of ammunition according to any one of claims 1 to 6, in which the retaining elements are mounted on fairings which are integral with the body of the projectile at its rear end and which pivotally supportfinsforming a tail assembly of the projectile.

8. Around ofammunition according to any one of claims 1 to 7, which includes a stop ring adjacentthe rear end ofthe projectile for locating the round in the launch tube.

9. A round of ammunition according to claim 1, substantially as described with reference to the accompanying drawings.