GB2136934A

GB2136934A - Rocket launchers

Info

Publication number: GB2136934A
Application number: GB08307679A
Authority: GB
Inventors: Peter Robert Thomas Cutler
Original assignee: Pains Wessex Ltd
Current assignee: Pains Wessex Ltd
Priority date: 1983-03-19
Filing date: 1983-03-19
Publication date: 1984-09-26
Also published as: EP0119569A2; EP0119569A3

Abstract

A rocket launcher comprises a launch tube 11 mounted on a handle 14, the handle being rotatable relative to, and about the axis of, the launch tube to operate a striker for firing a rocket 15 located within the launch tube. The launch tube 11 is of hollow wall construction and permits propulsion gases discharged from the rocket 15 upon ignition to enter the space between the walls 11a, 11b and flow forwardly, out of contact with the rocket, discharging from outlets in the outer end face of the tube, after the end cap 16 has been blown off. <IMAGE>

Description

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GB 2 136 934 A 1

SPECIFICATION

Improvements in rocket launchers

This invention relates to rocket launchers, and in particular to hand-held rocket launchers for 5 launching, for example, parachute flares.

Hand held rocket launchers usually comprise a launch tube in which a rocket is secured by an end cap, the cap being removed either manually before firing, or as a result of firing, the rocket. Such a 10 rocket is often launched under distress or other difficult conditions. It is therefore important that the firing of the rocket should take place simply but accurately and when required, without interference from the end cap if this is removed by 15 firing of the rocket.

In prior art rocket launchers propulsion gases have been vented either rearwardly through the base of the launch tube, which in the case of hand-held rocket launchers represents a 20 hazardous situation, or forwardly along the side of the rocket. In the latter case, if the rocket has been a close fit within the launch tube, firing of the rocket has created a gas pressure within the launcher at the rearward end of the rocket. This 25 has tended to expel the rocket before the rocket motor has achieved full ignition. It however the rocket has been a loose fit within the launch tube, so that the propulsion gases have been able to escape between the rocket and the wall of the 30 launch tube, the movement of the rocket down the launch tube has been erratic and the trajectory of the rocket has been unpredictable.

According to the present invention there is provided a rocket launcher, adapted to be hand-35 held, and comprising a launch tube having a cylindrical wall which has a rocket discharge opening at its forward end and is secured to a striker assembly at its rearward end. The wall of the launch tube is hollow to provide one or more 40 gas flow passages extending therealong from one or more inlets, open to the interior of the launch tube adjacent its rearward end, to one or more outlets at its forward end, to permit propulsion gases emitted from discharge nozzles at the 45 rearward end of the rocket to be conducted to said forward end of the launch tube out of contact with the rocket.

Preferably the launch tube is provided with an end cap which is fitted to the forward end of the 50 launch tube to cover the outlet of said one or more gas flow passages. Upon firing of the rocket, the closure cap, if not directly removed manually, will be blown off the end of the launch tube by gas discharge from such passages before the rocket 55 leaves the launch tube and accordingly does not impede the progress of the rocket. It will thus be seen that manual removal of the closure cap is not necessary.

A packing member is located in contact with 60 the forward end of the rocket and the inside of the launch tube. The packing member is retained in the launch tube by friction and is ejected as the rocket leaves the launch tube.

The invention is illustrated by way of example in the accompanying drawing in which:—

Fig. 1 is a side elevation, part sectioned, or a hand-held rocket launcher, and

Fig. 2 is a section on the line II—II of Fig. 1.

As shown in the drawing, the launcher 10 comprises a launch tube 11 mounted on a striker assembly 12, the striker assembly including a generally cylindrical housing 13 and a tubular handle 14 mounted for rotation on the housing 13. The striker assembly will be described further below, but it is sufficient to say, at this stage, that the launcher is operated by the user holding the launch tube 11 in one hand, the handle 14 in the other hand and, after release of a safety device, rotating the handle relative to the launch tube to operate the striker.

The present invention is primarily directed to the launch tube 11 which is a cylinder of hollow wall construction, in particular having outer and inner walls 11 a, 11 b, interconnected by webs to leave a passage, or particularly a multiplicity of passages, 11c between the inner and outer walls for the passage of gases resulting from the firing of a rocket 15 contained within the launch tube. The launch tube is conveniently a one-piece plastics extrusion moulding.

The launch tube is mounted in the open forward end of the housing 13 by forming a step 13a around the inside of the lip of the housing 13 and fitting the launch tube 11 into the forward end of the housing so that the outer wall 11 a of the tube 11 rests on the step, leaving the passages 11 c open to the interior of the launch tube 11 and of the housing 13 to provide gas inlets to the passages. At the forward end of the launch tube, the passages 11 c open on to the end surface of the launch tube to provide a plurality of gas outlets.

The forward end of the launch tube is closed by an end cap 16 which fits resiliently over this end and which engages the outer side of the launch tube to form a seal, conveniently using an 0 ring seal 17.

This end cap 16 is designed to be blown off the end of the launch tube, upon firing the rocket, by propulsion gases which initially are discharged rearwardly from the rearward end of the rocket, then reverse direction, as shown by the arrows, enter and flow forwardly along the passages 11 c and discharge from the forward end of the passages 11 c against the inside of the end cap, creating sufficient pressure to blow the end cap off the launch tube.

The rocket 15, which conveniently is of the solid propellant type, has an igniter located centrally at its rearward end to be struck by a striker and a number of angled discharge nozzles 15a at its rearward end designed not only to propel the rocket but also to impart spin to the rocket for stabilisation.

The result of the flow of propulsion gas through the passages 11 c of the launch tube, by-passing the rocket, is not only to remove the end cap 16 and so prevent it from impeding the flight of the rocket, but also to prevent an undesirable pressure

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rise within the launch tube 11 behind the rocket which would tend to drive the rocket out of the launch tube before the emission of propulsion gas had imparted the necessary thrust to the rocket.

5 A disc-shaped packing member 18 is fitted into the forward end of the launch tube to engage the inside of the launch tube and to contact the forward end of the rocket 15. This packing member engages the launch tube with sufficient 10 friction to prevent discharge of the rocket prior to full ignition.

The striker assembly 12 can be formed as described in detail in British Patent Specification No. 869341.

15 In the present embodiment, the assembly 12 comprises, in addition to housing 13, a striker 20 slidable longitudinally, on the axis of the launch tube, within a sleeve 21 and biased by a spring 22. The sleeve 21 is secured to the housing 13 by 20 an annular cam 23 which bridges between the sleeve 21 and housing 13. The annular cam is formed, over each semi-circle of its surface length, with a slow rise fast drop cam profile. At its rearward end the striker carries a transverse pin 25 24 whose ends engage the cam profiles and are held in contact therewith by the spring 22. The pin 20 also engages in slots (not shown) in the handle which extend parallel to the launch tube axis. Thus upon rotation of the handle 14 relative to the 30 launch tube 11, the pin 20 is caused to ride up the slow rise cam profiles, simultaneously compressing the spring, until the pin drops over the fast drop profiles and allows the striker to be driven forward by the spring against the igniter of 35 the rocket.

The striker is preferably provided with a safety device in the form of a projection 14a on the inside of the handle 14 which engages in a slot 13b in the housing 13 (or vice versa). The slot has 40 a first short circumferential portion leading into an axial portion and thence into second full circumferential portion. Each portion contains a neck or other construction past which the projection must be pushed, each obstruction

45 providing sufficient resistance to movement of the projection to prevent inadvertent use.

In order therefore to fire the rocket, the handle must be (1) rotated past the first obstruction into a READY position, (2) moved axially past the second

50 obstruction into a ARMED position, and (3) rotated past the third obstruction to the FIRE position, in which the striker spring is loaded and then released to strike the igniter.

Claims

55 1 • A rocket launcher, adapted to be hand-held, and comprising a launch tube having a cylindrical wall which has a rocket discharge opening at its forward end and is secured to a striker assembly at its rearward end, said cylindrical wall being

60 hollow to provide on or more gas flow passages extending therealong from one or more inlets,

open to the interior of the launch tube adjacent its rearward end, to one or more outlets at its forward end, to permit propulsion gases emitted from

65 discharge nozzles at the rearward end of the rocket to be conducted to said forward end of the launch tube out of contact with the rocket.
2. A rocket launcher according to claim 1 wherein the tube comprises coaxial inner and

70 outer cylindrical wall members interconnected by spacers.
3. A rocket launcher according to claim 1 or claim 2 having a cap which fits over the end of the cylindrical wall and is removable by discharge of

75 the rocket, or of rocket gases from said outlets.
4. A rocket launcher according to any preceding claim having a packing member fitted within, and in frictional engagement with, the forward end of the launch tube to prevent the discharge of the

80 rocket prior to full ignition.
5. A rocket launcher according to any preceding claim having a striker mechanism including a handle rotatable about the axis of the launch tube to operate the striker.

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6. A rocket launcher substantially as herein described with reference to the accompanying drawings.

Printed in the United Kingdom for Her Majesty's Stationery Office, Demand No. 8818935, 9/1984. Contractor's Code No. 6378. Published by the Patent Office, 25 Southampton Buildings, London, WC2A 1AY, from which copies may be obtained.