IL21766A - Projectile firing device - Google Patents

Projectile firing device

Info

Publication number
IL21766A
IL21766A IL21766A IL2176664A IL21766A IL 21766 A IL21766 A IL 21766A IL 21766 A IL21766 A IL 21766A IL 2176664 A IL2176664 A IL 2176664A IL 21766 A IL21766 A IL 21766A
Authority
IL
Israel
Prior art keywords
projectile
firing
guide rod
piston head
case
Prior art date
Application number
IL21766A
Original Assignee
Bertschmann H
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bertschmann H filed Critical Bertschmann H
Publication of IL21766A publication Critical patent/IL21766A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41CSMALLARMS, e.g. PISTOLS, RIFLES; ACCESSORIES THEREFOR
    • F41C27/00Accessories; Details or attachments not otherwise provided for
    • F41C27/06Adaptations of smallarms for firing grenades, e.g. rifle grenades, or for firing riot-control ammunition; Barrel attachments therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F1/00Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
    • F41F1/06Mortars
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F7/00Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B30/00Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
    • F42B30/04Rifle grenades

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)

Description

The present invention relates to projectile firing devices of the type comprising a guide rod, a striker subjected to the action of an instantaneous release propulsion device, a hollouj body fitting slidably on the guide rod, and a piston head fitting in the bore of the hollouj body s© as to form in said bore an extensible explosion chamber in which a firing charge is disposed.
The device according to the invention is characterised in that the firing charge is disposed in the case of an auxiliary projectile housed in said explosion chamber, and in that the hallow body is provided with at least one radial aperture permitting the escape of the explosion gases of the auxiliary projectile charge, the whole device being so shaped and disposed that the hollow body or the guide rod is projected by the auxiliary projectile when the charge contained in its case explodes, and that the gases of this explosion escape through said radial aperture only when one of the two parts, the guide rod or the hollow body has travelled a distance in relation to the other such that the radial aperture of the hollow body is situated between the case and the . all of the auxiliary carrier projectile.
The accompanying drawing illustrates diagrammati-cally by way of example various forms of construction of the projectile firing device forming the subject of the invention.
Figures 1 to relate to a first embodiment, 4 Figure 1 is a view in axial section thereof; Figures 2 are partial view in axial section and 3 two successive phases of the firing and, is a view in elevation of an alternative embodiment. relates to a second form of construction of the projectile firing device according to the invention is a general vieui thereof in axial section with the projectile to be fired in the position occupied on the firing of the shot; is a partial view thereof in axial section with the projectile to be fired in the position which it occupies at the moment when it leaves the device; is a general vieui thereof in elevation on a reduced scale; are axial sections on a larger scale of the percussion device and of the piston head respectively; relate to a third form of construction of the device according to the invention; is a general vieui thereof in axial section similar to Figure 5; is a partial vieui in axial section similar to Figure 6; is a general vieui thereof similar to Figure 7; Figure 13 is a partial axial section on a larger scale of the percussion device, and Figure 14 is an axial section on a larger scale of the piston head.
The projectile firing dev/ice illustrated in Figures 1 to 4 comprises a hollow guide rod 1 closed at its rear end, ujhich is firmly held in a sleeve 2 supported by a fixed support. This closed rear portion of tfhe guide rod 1 contains a slidafrle striker 3 acted on by a pre-armed spring 4 and retained by a catch constituted by a radial pin 5, The mouth of the guide rod 1 is capped by a solid metal cap 6 placed over the end of the tube 1 and having an axial hole 7 of the same diameter as the pin 3a of the striker. The projectile to be fired is engaged on the front and middle portion of the hollow rod 1 carrying the cap 6, This projectile comprises a hollow cylindrical body 8, the cy lindro-conical head 8a_ of which is closed, and the open rear end of which is integral with a metal ring 9 fitting slidably on the hollow rod 1, The middle portion of the hollow body 8 is fitted to slide fluid-tightly on the cap 6, which thus forms a piston head. The bore in the hollow body 8 has at its front end, in front of the cap 6, a portion 10 of slightly reduced diameter forming an explosion chamber containing a small auxiliary projectile comprising an unarmoured ball l^held by crimping in a case 12 containing an explosive charge.
In its middle portion the hollow cylindrical body 8 has a ring of radial apertures 13 bringing the bore into communication with an external decompression chamber outside sleeve 15 fixed between tujo collars 8jb and B on the body 8, The sleeve 15 is likeu/ise provided with a ring of radial apertures 16 bringing the chamber into communication with the free atmosphere.
The operation of the device just described is as folloujs: under the effect of the explosion of the charge contained in the case 12 of the auxiliary projectile (hereinafter referred to as "carrier pro ectile"), this explosion being produced by the percussion pin 3a driven forwards by the spring 4 when the catch 5 is drawn outwards, the ball 11 of the small carrier projectile, which when the device is the position illustrated in Figure 1 touches the solid end of the head 8a of the hollouj body 8, drives the latter forwards, the case 12 adhering through the action of the recoil to the cap 6 covering the mouth of the hollow guide rod 1. During the extremely short time (following the explosion) required by the hollouj body 8 to travel the necessary distance to pass from the position illustrated in Figure 1 to that illustrated in Figure 2, in which the radial apertures 13 are still masked by the cap 6 or the case 12, the explosion gases cannot escape through these apertures and consequently give up all their energy to the carrier projectile, the thrust applied by which to the body 8 attains a maximum. Continuing its travel, guided on the inside by the hollom rod 1, the hollow body 8 leaves said rod as indicated in Figure 3, carrying with it, by means of its integral rear ring 9, the cap 6 and the empty case 12; as soon as the radial apertures 13 pass beyond the case 12, the explosion gases contained in the chamber 10 are admitted through said apertures into the decompression chamber 14, where they can expand before escaping to tre open atmosphere through the apertures 16. This escape of the gases expanded in the chamber 14 enables the noise produced by the explosion of a small cartridge, which is already relatively small to be reduced. The recoil may be absorbed by a damping support in which the sleeve may be fixed.
Figure 4 illustrates an alternative embodiment in which the hollow body is provided with an ogive 18 possessing guide vanes 19 and adapted to contain an explosive, smoke-producing, or tear gas-producing charge, an optical or acoustic signalling device, or any other device operating after a time lag or on impact.
It is obvious that the propulsion device operating the striker may be different from that illustrated by way of example, and that it could for example be electrical, electro-magnetic, pneumatic, or of another type.
In a modified embodiment (not illustrated), the cap-piston head may be integral with the guide rod and said rod may be driven with the hollow body when the ring integral with the latter strikes against the cap 6. In this case the rear end of the hollow guide rod would of course not be fixud in the sleeve 2, but simply laid against a fixed support.
In this case also, the rear end of the hallow guide rod could be open and the propulsion device be independent of said rod and not move with the latter.
The device illustrated in Figures 5 to 9 comprises a solid launching and guide rod 21, the rear end of which is held firmly in a support, which may for example be the muzzle of any firearm, or a support fixed to the ground.
On the rod 21 there is slidably fitted the rear portion 22_a of the hollow body 22 of a projectile to be fired, the cylindro-conical head 23 of which may contain an explosive, anti-tank, smoke-producing, tear gas-producing, or lighting charge, a device operating with a time lag or on impact, or else an optical or acoustic signalling device.
By means of a screw fitting 24 the head 23 of the projectile is made fast to the front hollow portion 25a of a percussion rod 25, the rear end of which terminates in a percussion pin 25b. The percussion rod 25 with its pin 25b is mounted slidably in the bore of the front portion 22t> of the hollow body 22 through the medium of a threaded metal ring 26 (Figure 8). The percussion rod is subjected to the action of a coil spring 28 which' s surrounds its hollow front portion 25a and bears on the one hand against an inside shoulder 22c: provided on the front end 22_b of the hollow body 22, and on the other hand against the front face of the ring 26. The solid portion of reduced diameter of the rod 25 and the percussion pin 25b are guided in a sleeve 27 screwed in the middle portion and in the front portion 22_b of the hollow body 22. A catch pin 29 (Figure 8) penetrating radially into the front portion 22t> of the hollow body 22 enables the percussion spring 28 to be held armed when the ring 26 is situated in the front of the catch 29, the head 23 of the projectile to be fired having been drawn forwards with the percussion rod 25. The front portion 22b_ of the hollow body is fixed to the middle portion of the latter through the medium of the sleeve 27 screwed into these two parts.
A piston head 3D fits in the bore of the middle and rear portions of the hollow body 22 forming a cylinder, so as to slide in a fluid-tight manner therein, and has an axial hole 31 bringing a rear space 32 into communication with a front chamber 33 containing a wad of stiff grease 34. The piston head bears at the rear against the front end of the guide rod 21, of which an extension 21a having a reduced diameter penetrates with play into the rear space 32. The portion of the bore in the hollow body 22 which is situated between the front face of the piston head 30 and the rear face of the sleeve 27 forms an explosion chamber containing an auxiliary projectile 35 which, like usual standard ammunition, is composed of a case 35¾g containing an ex-plosive charge and a cy lindro-conical ball 3 E¾ of more or less soft metal (not armoured), secured by crimping in the case 35j . When this auxiliary projectile 35 is contained in the explosion chamber having the dimensions possessed by it on the firing of the shot (Figure 5 ) , said projectile practically completely fills said chamber and the conical point of the ball 35Jk» engages lightly in the front grease chamber 33 of the piston head 30.
The rear portion 22a of the hollow body has in its thin wall a ring of radial apertures 6 bringing the bore of said rear portion into communication with an external decompression chamber 37 which together with said thin wall forms an external sleeve 38 fixed between a rear collar 39 and an outer rib 40 (Figure 6) on the hollow body 22ja . This external sleeve 38 may also be provided with radial apertures 41 bringing the decompression chamber 37 into communication with the outside, or in the construction illustrated with an empty space 42 provided between the sleeve 38 and a tubular support 43 carrying vanes 44 and provided with perforations or longitudinal slots. This support 43 is fixed between the rear collar 39 and a nut 45, The operation of the projectile firing device which has just been described (Figures 5 to 9) is as follows ; In order to load this device, the front portion 22JD of the hollow body 22 and also the connecting sleeve 27 are unscreu/ed in order to free the explosion chamber situated between the piston hsad 30 and the front end of the middle portion of the hollow body 22, the piston head 30 being supported against the free end of the guide rod 21, A ball cartridge 35 is then introduced into said chamber with its ball 3¾ directed towards the rear and bearing by its conical tip against the cylindrical wall of the grease chamber 33 of the piston head 30. The sleeve 27 and the front portion 22b of the hollow body are then screwed back in position, after the head 23 of the projectile to be launched has been pulled forward in order to arm the percussion spring 28, which is held armed by means of the catch pin 29 which bears on the rear face of the ring 26. The front face of the case 35^ of the carrier projectile 35 rests on the rear face of the threaded sleeve 27, In order to fire the shot and project the head projectile 23 forwards, it is sufficient to pull the catch pin 29 in the outward direction in order to free the armed spring 28 and propel towards the rear the percussion rod 25, the pin 25_b of which strikes against the case 35b and causes it to explode. The case 35^ then acts on the rear face of the sleeve 27 which is integral with the hollow body 22 and propelJs the latter forwards, while the ball ^SQ is wedged in the grease chamber 33 of the piston head 30. As it does so, the-, ball ^,.which is of relatively soft metal brakes the recoil as soon as the shot is fired; this braking is accentuated by the wad of grease 34 into which the tip of the ball penetrates. As a result, the grease is pressed through the axial passage 31 in the piston head 30 towards the rear space 32 in the latter, into which the extension 21 of reduced diameter of the guide rod 21 penetrates with play. The grease is spread around this extension and over the rear face of the pistonhead which surrounds the space 32 and on this annular surface forms a thin damping film intended to damp the impact of the piston head against the end of the cylinder when the projectile leaves the guide rod 21.
The grease thus not only forms a recoil and impact damper, but also contributes towards sealing the explosion chamber immediately after the firing of the shot. As soon as the hollow body has travelled a sufficient distance on the guide rod 21 for its radial apertures 36 to be situated between the ball and the case of the carrier projectile, the gases contained in the explosion chamber, and already partially expanded because of the elongation of that chamber 26 can escape through said apertures and pass into the decompression chamber 37 and thence into the outside space 42 and finally into the atmosphere.
Because of this progressive decompression of the explosion gases, and on the other hand because of the propulsion of the hollow body by the case 3^ possessing on the firing of the shot its maximum speed imparted to it by all the energy developed by the explosion of the charge enclosed by the ball secured by crimping in the case, it is possible to obtain with a cartridge of relatively small calibre a substantially greater propulsion effect than that which would- be obtained with a much heavier charge exploding directly in an explosion chamber (for example a blank cartridge). In addition, the damping by the ball acting progressively, starting from the firing of the shot, on the piston head 30 and the wad of grease 34 contributes towards considerably reducing the recoil effect and the mechanical stresses on materials used, as well as reducing the noise of the explosion, which is already vary small because of the use of a cartridge which is very small in relation to the weigh.t of the projectile to be launched.
The projectile firing device illustrated in Figures 10 to 15 is distinguished from that just described in that the hollow body is fixed while the guide rod itself is projected by the carrier projectile. The central body of the projectile 80 to be launched, for example of an anti-tank grenade provided with vanes 81 and carrying in its head 82 an explosive or other charge, is screwed on the front threaded end 51a of the guide rod 51. A hollow body 52, the rear portion 52_a of which is held firmly in a support, is fitted slidably by means of a sleeve 53 on the guide rod 51. The middle portion of the hollow body 52 is fixed to a rear extension 52ja by means of a sleeve 57 screwed into these two parts. In I the fixed rear extension 52a of the hollow body therejis slidably mounted, through the medium of a threaded ring 54, a percussion rod 55 which ends at the front in a pin 55b and on the hollow rear portion 55_a of which there is wound the percussion spring 58 which bears on the one hand against the -ep-ring 54 and on the other hand against an inside shoulder 52b on the rear extension 52a. of the hollow body.
The rear end of the extension 52a of the hallow body is provided with a longitudinal slot 56 engaging a catch pin 59 inserted in the hollow rear end 55a of the percussion rod 55 and intended to keep the percussion spring 58 armed when it is pulled to the rear as far as the rear end of the slot 56 and locked in that position by introducing it by a slight turn into a lateral notch 56a in the wall of the slot In the bore in the hollow body 52 ahead of the sleeve 57 there is fitted with fluid-tight slidability a piston head 60 having an axial hole 61 bringing a front space 62 into communication with a rear chamber 63 in which a wad of stiff grease 64 is disposed (Figure 14), The piston head 6© bears at the front against the rear end of the guide rod 51, of which an extension of reduced diameter engages with play in the front space 62 in the piston head 60. The portion of the bore in the hollow body 52 which is situated between the rear face of the piston head 60 and the front face of the sleeve 57 forms an explosion chamber in which there is received an auxiliary projectile 65 composed, like customary standard ammunition, of a case 65a containing an explosive charge and of a cy lindro -conical Jpall 65_b of more or less soft metal (not armoured), secured by crimping in the case 65a. UJhen this carrier projectile is accommodated, with its ball 65b towards the front, in the explosion chamber as the latter is constituted before the firing of the shot (Figure 10), it fills said chamber almost completely and the conical tip of its ball 65b engage^lightly in the grease chamber 63 in the piston head 60.
The outside portion of the holloui body 52 has in its mall of reduced thickness a ring of radial apertures 66 bringing the bore of said portion into communication with an external decompression chamber formed by said wall together with an external sleeve 63 fixed between a collar 69 on the sleeve 53 and an external rib 70 on the hollow body 52. This external sleeve 68 may also be provided with radial apertures, not shown, bringing the decompression chamber 67 into communication with the outside, or when the projectile 80 integral with the guide rod 51 is in the position shown in Figure 10 on the firing of the shot, with the inside empty space 71 in the tubular support 72 which is open at the rear and carries the vanes 81 of the projectile.
The operation of this projectile firing device (Figures 10 to 14) is as follows: In order to load the projectile firing device, the front portion of the hollow body 52 and also the connecting sleeve 57 are unscrewed in order to free the explosion chamber situated between the piston head 60 and the rear end of the middle portion of the hollow body 52, the piston head 60 being supported against the rear end 51b of the guide rod 51. A ball cartridge 65 is introduced into said chamber with its ball 65b directed forwards and bearing by its conical tip against the cylindrical wall of the grease chamber 63 in the piston head 60. The sleeve 57 and the middle portion of the hollow body 52 are then screwed in place again and the percussion spring 58 is armed by pulling towards the rear the percussion rod 55 by means of the radial catch pin 59, which is locked, by a slight rotation, in the notch 56a. In order to fire the shot and project the projectile 80, with its head 82 forwards (Figure 12), it is sufficient to free the catch pin 59 from the notch 65a in order to free the percussion spring 58 which propels forwards the percussion rod 55, the pin 55_b of which strikes the case 65a of the carrier projectile 65 and explodes the charge which it contains, thus propelling the ball 65_b which drives forwards the piston head 60 and, through the latter, the guide rod 51 which is integral through its threaded end 51a with the projectile body 80. The ball 65t) is wedged in the grease chamber 63 and in the latter compresses the grease of the wad 64, part of which passes through the axial passage 61 into the front space 62 and spreads around the extension 51b of the rod 51 and over the front surface of the piston head, where it forms a film which damps the impact of the piston head 60 against the and of the cylinder formed by the sleeve 53,i at the moment when the rod 51 with the projectile 80 carried by it leaves the fixed hollow body 52. As soon as the guide rod 51 propelled by the piston head 60 under the thrust of the ball 65_b has travelled, in the bore in the hollow body 52, through a sufficient space for the radial apertures 66 on said body to be situated between the ball 65b and the case 65a. on the carrier projectile, the gases contained in said space can escape through said apertures and pass into the decompression chamber 67 and thence to the outside through the open rear of the support 72 of the vanes 81.

Claims (3)

HAVING NOW particularly descrbed and ascertained _the nature of our said inventon and in what manner the same is ~to be · performed, : we declare that what we claim is.
1. A projectile firing device comprising a guide rod, a striker subjected to the action of an instantaneous release propulsion device, a hollouj body fitting slid- . 5 ably on the guide rod, and a piston head fitting so as to slide in a fluid-tight manner. in the bore in the hollouj body in such a manner as to form in said bore an extensible explosion chamber in which a firing charge is disposed, characterised in that the firing 10 charge is disposed in the case of an auxiliary projectile housed in said explosion chamber, and in that the holloui body is provided with at least one radial aperture permitting the escape of the explosion gases of the charge contained in the case of the auxiliary pro- 15 jectilo, the whole arrangement being so shaped and disposed that the hallow body or the guide rod is projected by the auxiliary projectile on the explosion of the charge contained in its case, and that the gases of said explosion escape through said radial 20 aperture only when one of the tu/o parts, the guide rod or the holloui body, has travelled a distance in relation to the other such that the radial aperture in the hollouj body is situated between the case and the all of the auxiliary carrier projectile, 25
2. A device according to Claim 1, characterised in that a projectile to be fired is integral with the hollow body on which the carrier projectile acts.
3. A device according to Claim 1, characterised in that the projectile to be fired is integral with the guide 30 rod on which the carrier projectile acts. A device according to Claim 1, characterised in that the guide rod is at least partly hollow and that the striker with its catch type percussion device is mounted in said hollow rod. A device according to Claim 4, characterised in that the piston head is constituted by a perforated cap fitting over the mouth of the hollow guide rod, the striker being so disposed as to strike the case of the carrier projectile through the axial hole in said cap. A device according to Claims 1 and 2, characterised in that the striker is disposed in the front portion of the hollow body and strikes the case of the carrier projectile, the ball of which is directed towards the rear and bears against the piston head olosing the explosion chamber, bearing on the firing of the shot against the end of the guide rod held in a fixed support, A device according to Claims 1 and 3, characterised in that the striker is disposed in the rear portion of the hollouj body and strikes the case of the carrier projectile, the forwardly directed ball of which bears against the piston head which closes the explosion chamber, bearing on the firing of the shot against the rear end of the guide rod. A device according to Claims 1, 3 and characterised in that the case of the carrier projectile •eixikee—by its rear face against a sleeve screwed in the hollow body and provided uiith an axial hole for the passage of the striker. i A device according to Claims 1, 3 ij and §, characterised in that the striker is mounted in a fixed tubular support which is at least detachably secured to the hollouj body. A device according to any of the foregoing Claims characterised in that the piston head is provided with an axial hole bringing into communication with one v 1<* another two end cavities^ one of which is intended to receive the end of the guide rod and the other to wedge the ball on the carrier projectile, A device according to Claim Jd, characterised in that the end cavity in the piston head which is intended to wedge the ball of the carrier projectile contains a wad of grease contributing towards damping the impact of the ball on the firing of the shot and the impact ofthe piston head against the end of the bore in the hollow body when the projectile to be launched leaves the firing device. A device according to any of the foregoing Claims, characterised in that the hollow body is provided with an outside sleeve forming a gas decompression -chamber, with which the radial aperture is in communication,' characterised inj^the explosion chamber is so dimensioned that on the firing of the shot it is practically completely filled by the carrier projectile, so as to provide said projectile with maximum thrust on -the- firing of the shot and so that the recoil will be immediately damped through the driving of the soft metal ball into the grease chamber in the piston head. A projectile firing device substantially as herein before described and illustrated with reference to the accompanying drawings. Dated this 24th day;-of July, 1964
IL21766A 1964-05-12 1964-07-26 Projectile firing device IL21766A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH617864A CH410687A (en) 1964-05-12 1964-05-12 Projectile intended to be fired by means of a fixed launching and guiding rod
CH693664A CH410684A (en) 1964-05-12 1964-05-27 Device for launching a projectile fitted with a guide rod

Publications (1)

Publication Number Publication Date
IL21766A true IL21766A (en) 1968-01-25

Family

ID=25699120

Family Applications (1)

Application Number Title Priority Date Filing Date
IL21766A IL21766A (en) 1964-05-12 1964-07-26 Projectile firing device

Country Status (12)

Country Link
US (1) US3306163A (en)
AT (1) AT252071B (en)
BE (1) BE649125A (en)
CH (2) CH410687A (en)
DE (1) DE1428609A1 (en)
DK (1) DK116263B (en)
ES (1) ES301472A1 (en)
FI (1) FI44536C (en)
FR (1) FR1399374A (en)
GB (1) GB999501A (en)
IL (1) IL21766A (en)
SE (1) SE303441B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH450228A (en) * 1965-10-22 1968-01-15 Transurvey Holding Company Inc Device for launching a projectile
US3505924A (en) * 1967-04-18 1970-04-14 Allied Res Ass Inc Silent mortar
CH464736A (en) * 1967-10-03 1968-10-31 Batou Boris Shooting equipment comprising a mortar and a projectile
CH479044A (en) * 1968-04-11 1969-09-30 Transurvey Holding Company Inc Ballistic assembly formed by a projectile and its launching device
IT1216479B (en) * 1988-02-29 1990-03-08 Socimi LIGHT GRINDER LAUNCHES OF THE PERFECT TYPE.
CA3041106C (en) 2009-09-09 2020-11-10 Aerovironment, Inc. Reinforced unmanned aerial vehicle launch tube
CN111220024B (en) * 2018-11-23 2021-12-07 谢明龙 Grenade auxiliary ejector

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1721704A (en) * 1926-05-26 1929-07-23 Madaschi Giuseppe Apparatus for throwing bombs or torpedoes
FR714636A (en) * 1930-07-25 1931-11-25 Pomegranate enhancements
NL122936C (en) * 1960-05-05
NL124802C (en) * 1961-07-20 Energa

Also Published As

Publication number Publication date
FI44536B (en) 1971-08-02
US3306163A (en) 1967-02-28
FI44536C (en) 1971-11-10
GB999501A (en) 1965-07-28
CH410684A (en) 1966-03-31
AT252071B (en) 1967-02-10
DK116263B (en) 1969-12-22
CH410687A (en) 1966-03-31
BE649125A (en) 1964-10-01
DE1428609A1 (en) 1969-02-27
SE303441B (en) 1968-08-26
ES301472A1 (en) 1965-01-16
FR1399374A (en) 1965-05-14

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