US3882780A - Rifle grenade, particularly for firing tear gas or flare projectiles - Google Patents

Rifle grenade, particularly for firing tear gas or flare projectiles Download PDF

Info

Publication number
US3882780A
US3882780A US422724A US42272473A US3882780A US 3882780 A US3882780 A US 3882780A US 422724 A US422724 A US 422724A US 42272473 A US42272473 A US 42272473A US 3882780 A US3882780 A US 3882780A
Authority
US
United States
Prior art keywords
grenade
igniter
rifle
launching tube
bore
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
US422724A
Other languages
English (en)
Inventor
Heinz Gawlick
Rudolf Stahlmann
Ernst Jensen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dynamit Nobel AG
Original Assignee
Dynamit Nobel AG
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 Dynamit Nobel AG filed Critical Dynamit Nobel AG
Application granted granted Critical
Publication of US3882780A publication Critical patent/US3882780A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
    • F42B30/04—Rifle grenades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C14/00—Mechanical fuzes characterised by the ammunition class or type
    • F42C14/02—Mechanical fuzes characterised by the ammunition class or type for hand grenades

Definitions

  • ABSTRACT Rifle grenade for launching from the barrel of a firearm having a grenade body, a launching tube and a detonator.
  • the detonator is in the form of impactinitiatable igniter disposed at one end of the grenade body facing the launching tube and having a striker element spaced from the igniter in a safety position.
  • the striker element is arranged to move forwardly toward the igniter to impact thereon upon launching of the grenade.
  • a delay train may be interposed between the igniter and material carried by the grenade bodyfor igniting the material after a predetermined delay.
  • the present invention relates to a rifle grenade, especially for the firing of tear gas or flare projectiles, with a grenade body, a launching tube, and a detonator.
  • Rifle grenades have been known which serve for the firing of explosive elements.
  • the explosive elements have a percussion detonator, initiating the ignition thereof upon impact on the target.
  • rifle grenades defines the type of grenades which are placed onto the front end of a firearm barrel, optionally with the use of an adapter, and are fired over more or less great distances, depending on their weight, their shape, the firing propellant charge, etc.
  • projectiles are known from DAS [German Published Application1No. 1,933,029, which have a solid element producing irritating gases while smoldering. These projectiles are hurled by hand or optionally are also conveyed to the location of deployment by means of suitable firing devices. These projectiles are ignited either manually directly prior to throwing by means of a friction igniter or also only upon impact on the target by means of a percussion fuze.
  • the projectiles to be hurled by hand have the disadvantage that, on the one hand, the throwing ranges attainable are often too short and, on the other hand, the
  • a conventional rifle grenade with a grenade body, a launching tube, and a detonator, with the detonator constructed as an igniter disposed at the end of the grenade body facing the launching tube and ignitable by impact, with a striker element held at a spacing therefrom in a safety position and movable toward the igniter upon firing, and with a pyrotechnic delay train arranged after the igniter.
  • the ignition is advantageously already initiated during the launching of the rifle grenade, by driving the striker element, under the pressure effect of the propellant gases of the propellant cartridge inserted in the cartridge chamber of the fire arm, toward the igniter.
  • the flawless ignition of the rifle grenade is reliably ensured, entirely independently of the impact surface and the impact angle.
  • This delay can be determined, by the composition of the pyrotechnic mixture and thus its deflagration speed, as well as by the length of the delay train, in correspondence with the requirements of each individual case. For example, the provision can be made that the charge arranged after the delay train is ignited only after the rifle grenade has reached a certain distance from the launching site.
  • the rifle grenade of the present invention is intended particularly for the firing of tear gas or flare projectiles.
  • the conventional tear-gasproducing smoldering charges or flare compositions with ejection and ignition charges are disposed after the pyrotechnical delay train.
  • an additional parachute for the flare can also be provided, in order to provide for a maximally gradual descent of the burning flare.
  • the riflegrenade of this invention can, however, also be advantageously employed for the firing of other irritant-gas elements, smoke-producing marker charges, smoke ammunition, or the like.
  • the striker element In order to prevent the rifle grenade of this invention from being ignited inadvertently, for example when dropped to the ground accidentally, the striker element is held in a safety position at a distance from the igniter.
  • the striker element can be connected, for example, by way of predetermined breaking points with the launching tube with the strength thereof being dimensioned so that the striker element separates from the tube only after reaching a predetermined propellant gas pressure and is driven against the igniter.
  • a detonator holder or carrier is provided with a central continuous bore with the igniter being inserted therein from one end, preferably by a friction fit and, from the other end, a pyrotechnical delay train, housed in a sleeve, is inserted in this bore, preferably by means of a threaded connection.
  • the detonator holder is made of a metal, preferably aluminum.
  • the striker element can additionally be disposed in a tubular extension of the detonator holder extending toward the rear beyond the igniter, so that the striker element is axially displaceable therein.
  • the detonator holder serves for the coupling of the grenade body and the launching tube.
  • the individual parts are threadedly joined, optionally with the use of special supporting disks, locknuts, or the like.
  • the detonator holder has at least one gas discharge duct starting from the central bore in the zone between the igniter and the delay train.
  • gas discharge ducts Preferably, two or more symmetrically distributed gas discharge ducts are provided. These ducts connect the space between the igniter and the delay train with a further space, so that the combustion gases of the pyrotechnical mixture can flow off into this space and thus the mixture can burn up at a practically constant pressure.
  • This additional space can be, for example, the interior of the launching tube or also an empty space or chamber provided around the casing of the pyrotechnic delay train.
  • the striker element can furthermore be combined with an intercept member disposed in a force fit within the launching tube and movable in the forward disrection under the effect of an impringing armed projectile.
  • an intercept member disposed in a force fit within the launching tube and movable in the forward disrection under the effect of an impringing armed projectile.
  • the proportion of kinetic energy of the projectile driven through the barrel which is converted into heat and thus dissipated can be chosen in dependence on the particular requirements.
  • another feature of this invention provides the intercept member with a blind bore starting at the rear end thereof.
  • the blind bore generally extends over about three quarters of the length of the intercept member and is chosen to be somewhat smaller in its inside diameter than the caliber of the projectile, so that the latter is securely caught in the member after entering the blind bore.
  • the invention provides to equip the launching tube at its rear end with a lid connected to the tube by a shape-mating and/or frictional connection.
  • the lid is pulled off prior to firing of the rifle grenade.
  • This lid can advantageously also serve simultaneously for holding the propellant cartridge included with each rifle grenade.
  • this propellant cartridge can, however, also be inserted in the launching tube together with an accessory sight enclosed with each rifle grenade, so that the marksman always has all parts required for the satisfactory firing of the rifle grenade readily available.
  • FIG. 1 shows the entire rifle grenade, partially in a longitudinal sectional view
  • FIG. 2 shows a fragmentary view of the rifle grenade according to FIG. 1 on an enlarged scale
  • FIG. 3 shows another embodiment of a portion of a rifle grenade in accordance with the present invention
  • FIG. 4 shows another embodiment of a portion of a rifle grenade in accordance with the present invention
  • FIG. 5 shows a rifle grenade with a lid inserted in the launching tube
  • FIG. 6 shows another embodiment in accordance with the present invention.
  • FIG. 1 a rifle grenade having a grenade body 1 and having the launching tube 2 with the tail unit 3 inserted in the rear end of the grenade body 1.
  • the grenade body 1 produced preferably of a synthetic resin, especially a thermoplastic synthetic resin, carries in its interior, in a conventional manner, the smoldering compositions, flare charges, or the like, which are not shown.
  • the grenade body 1 is tightly sealed at the front end by means of the nose 4 attached thereto and preferably welded thereto along the periphery.
  • FIG. 2 is an elevational view of the igniter or primer element 6 and the pyrotechnical delay train 7, accommodated in a sleeve.
  • the igniter 6 is inserted with frictional seat from behind in the continuous bore 8 of the detonator carrier 5, while the pyrotechnic delay train 7 is threadedly inserted in the bore 8 from the front.
  • the striker element 10, made, for example, of aluminum, is axially displaceably inserted in the tubular extension 9 of the detonator carrier 5, pointing toward the rear with the striker element being held in the extension by means of the spring ring 11 and is biased away from the igniter by means of the spring element 12 formed as a helical spring so as to be in a safety position.
  • the bore 8 is connected with the interior of the launching tube 2 via the two gas discharge ducts 13.
  • the detonator holder 5 has an annular collar 14 at its end facing the grenade body and a supporting disk 15, together with the bottom portion 16 of the grenade body 1 is supported on this collar 14 and securely held in this position by means of the launching tube 2 being threaded onto the detonator carrier 5 with the aid of the screw connection 17 such that the detonator carrier couples the grenade body 1 and the launching tube 2.
  • Black powder stoppers 18 are inserted, in this embodiment, in the front end of the delay train 7 and these stoppers serve conventionally for the further transmission of the ignition impulse to the frontmost charge, not shown herein.
  • the various charges are composed and housed in the customary manner.
  • the ignition is initiated during the launching of the rifle grenade by driving the striker element 10 under the pressure effect of the propellant gases of the propellant cartridge inserted in the cartridge chamber of the firearm toward the igniter 6.
  • the detonator carrier 5 likewise made of a metal, is formed with an outer diameter corresponding to that of the grenade body 1. From the rear, the launching tube 2 is threadedly inserted by means ofa screw connection 20, while the grenade body 1 is attached from the front and fastened by means of a locknut 21.
  • this embodiment is preferably employed for heavier rifle grenades, or for those which are to be fired over longer distances, since these require a higher firing pressure.
  • detonator holder 5 Another advantage of the detonator holder 5 shown herein is the radial arrangement of the gas discharge ducts 13, since these can be more readily manufactured than the gas discharge ducts 13 which extend obiquely toward the rear, as shown in FIG. 2.
  • These radial gas discharge ducts 13 are connected, via the annular recess 22 and the bores 23 provided in the locknut 21, with the additional space or chamber 24, into which the gases produces during the burning of the pyrotechnical delay train 7 can escape.
  • the further space 24 is formed as an annular chamber in the member 25, which latter is preferably injection-molded from a synthetic resin.
  • the additional charges, cover disks, etc., of which only a portion 26 are indicated of the conventional flare, irritant gas, smoke, marker projectiles or the like are disposed after this member 25.
  • the striker element 10 made of a metal, rests against a shoulder 27 and this striker element is supported at the detonator carrier 5 away from the igniter 6 by a spring element 12, fashioned as a cup spring.
  • the embodiment shown in FIG. 4 differs from the construction shown in FIG. 3 in the structure of the striker element which, in this case, is combined with an intercept meinber 28, i.e., is constructed integrally therewith.
  • a blind bore 30 emanates from the rear end of the intercept member 28 and is shown in dashed lines. The blind bore is arranged to receive the live ammunition projectile fired by the firearm with the intercept member 28 and striker element 10 being driven forwardly against the igniter 6.
  • the launching tube 2 is provided, at its rear end, with a frictionally attached lid 31, exhibiting a pull strip 32 for ready removal prior to firing.
  • the propellant cartridge 33 is inserted in the lid 31 so that the required tight seal of launching tube 2 is ensured.
  • the tail unit 3 pushed onto the launching tube 2 is held by means of a retaining ring 34.
  • the propellant cartridge 33 is inserted in an accessory sight 35 which, in turn, is inserted in the launching tube 2.
  • the lid 31 is provided which is inserted in the launching tube 2 with a frictional fit. Prior to firing, the marksman removes the lid 31, withdraws the accessory sight 35 with the propellant cartridge 33, and then inserts or attaches the individual parts in or to the firearm in a conventional manner.
  • the construction of the rifle grenade in accordance with the present invention makes it possible advantageously to fire the grenade, when irritant-gas projectiles are used, readily over distances of 75lOO in. ac-
  • the grenade body constructed with a corresponding strength, penetrates the window pane, door panel, or the like and either is caught therein or drops into the space, so that the irritant gas can escape into the space via the discharge openings disposed at the front end of the grenade body and can render any terrorists or similar persons present therein temporarily incapacitated.
  • the discharge openings are formed in the nose of the grenade body as regions of lesser wall thickness which, when a certain gas pressure has been reached within the grenade body, rupture in a defined manner.
  • Rifle grenade comprising a grenade body, launching tube means disposed at one end of said grenade body, and detonator means for said grenade, said detonator means including an impact-initiatable igniter disposed proximate to the one end of the grenade body facing the launching tube means, a striker means for impacting on said igniter being spaced from said igniter in a safety position and being responsive to the launching of the grenade for moving forwardly toward said igniter to impact thereupon, delay means responsive to the initiation of said igniter for igniting material carried by said grenade body after a predetermined time delay, said delay means including a pyrotechnic delay train operationally disposed between said igniter and the material carried by said grenade body, said detonator means further including means for carrying said igniter, said carrying means including a member having a central continuous bore extending therethrough, said igniter being positioned in the bore from one end thereof and
  • Rifle grenade according to claim 1 wherein said grenade body is arranged for carrying at least one of tear gas, flare projectiles, smoke producing material, irritant agent material and explosive material.
  • said detonator means further includes means for spacing said striker means from said igniter.
  • said spacing means includes at least one spring member.
  • Rifle grenade according to claim 1, wherein said carrying means interconnects said grenade body and said launching tube means.
  • Rifle grenade comprising a grenade body, launching tube means disposed at one end of said grenade body, and detonator means for said grenade, said detonator means including carrying means having a member with a central continuous bore extending therethrough, and impact-initiatable igniter disposed proximate to the one end of the grenade body facing the launching tube means and positioned in the bore from one end thereof, delay means responsive to the initiation of said igniter for igniting material carried by said grenade body after a predetermined time delay, said delay means being operationally disposed between said igniter and the material carried by said grenade body and being positioned at least partially within the bore from the other end thereof, said igniter and said delay means being spaced from one another within the central bore of said carrying means, said carrying means being provided with at least one continuously open gas discharge duct extending outwardly from the central bore in the region between said igniter and said delay means, and a striker means for impacting
  • said delay means includes a pyrotechnic delay train disposed within a sleeve member, said sleeve member being positioned at least partially within the bore from the other end thereof.
  • Rifle grenade according to claim 7, wherein said carrying means interconnects said grenade body and said launching tube means, and said at least one continuously open gas discharge duct serves for venting the central bore in the region between said igniter and said delay means.
  • said detonator means further includes intercept means positioned in said launching tube means and having said striker means mounted thereon, said intercept means being arranged to be impinged upon by alive projectile for being driven forwardly to impact said striker means on said igniter.
  • Rifle grenade according to claim 11, wherein said launching tube means is provided with a guide sleeve therein, said intercept means being positioned within said guide sleeve.
  • said detonator means further includes means for carrying the igniter, said guide sleeve having a portion thereof clamped within said launching tube means between a shoulder of said launching tube means and a portion of said carrying means.
  • Rifle grenade according to claim 7, wherein said launching tube means is provided at the end thereof disposed away from the one end of said grenade body with a lid member detachably connected thereto.
  • lid member is detachably connected to said launching tube means by at least one of a shape-mating and frictional connection.
  • lid member is detachably connected to said launching tube means by at least one of a shape-mating and frictional connection.
  • Rifle grenade according to claim 22 further comprising a propellant cartridge for the firing of the rifle grenade being carried by said lid member.
  • Rifle grenade according to claim 22 further comprising an accessory sight and a propellant cartridge for the firing of the n'fle grenande being positioned within said launching tube means.
  • said detonator means further includes means for spacing said striker means from said igniter.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Telescopes (AREA)
US422724A 1972-12-07 1973-12-07 Rifle grenade, particularly for firing tear gas or flare projectiles Expired - Lifetime US3882780A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2259861A DE2259861A1 (de) 1972-12-07 1972-12-07 Gewehrgranate, insbesondere zum verschuss von traenengas- oder leuchtkoerpern

Publications (1)

Publication Number Publication Date
US3882780A true US3882780A (en) 1975-05-13

Family

ID=5863762

Family Applications (1)

Application Number Title Priority Date Filing Date
US422724A Expired - Lifetime US3882780A (en) 1972-12-07 1973-12-07 Rifle grenade, particularly for firing tear gas or flare projectiles

Country Status (10)

Country Link
US (1) US3882780A (cs)
JP (1) JPS506200A (cs)
AT (1) AT337052B (cs)
BE (1) BE808371A (cs)
DE (1) DE2259861A1 (cs)
FR (1) FR2209921B1 (cs)
GB (1) GB1448993A (cs)
IT (1) IT997941B (cs)
MY (1) MY7700258A (cs)
NL (1) NL7316819A (cs)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4493263A (en) * 1981-11-16 1985-01-15 Carabateas Eustratios N Ballistic propulsion system
US4708061A (en) * 1986-02-22 1987-11-24 Hilti Aktiengesellschaft Explosive powder charge operated driving device
US5583314A (en) * 1994-05-19 1996-12-10 Luchaire Defense Sa Firing indicator device for a projectile, and rifle grenade equipped with a firing indicator device
US20050188886A1 (en) * 1996-11-18 2005-09-01 Pepperball Technologies, Inc. Non-lethal projectile systems
US20060011090A1 (en) * 2004-04-09 2006-01-19 Pepperball Technologies, Inc., A Delaware Corporation Primer launched projectile systems
US20080017179A1 (en) * 2004-05-12 2008-01-24 Pepperball Technologies, Inc. Compressed Gas Cartridge Puncture Apparatus
US20090071459A1 (en) * 2007-09-18 2009-03-19 Pepperball Technologies, Inc. Systems, methods and apparatus for use in distributing irritant powder
US20090266262A1 (en) * 2003-02-10 2009-10-29 Pepperball Technologies, Inc. Stabilized non-lethal projectile systems
US8196513B1 (en) * 2009-12-04 2012-06-12 The United States Of America As Represented By The Secretary Of The Navy Stand-off disrupter apparatus
CN103075919A (zh) * 2013-01-28 2013-05-01 马永忠 一种爆炸式催泪弹
US9671204B2 (en) * 2013-08-23 2017-06-06 Hanwha Techwin Co., Ltd. Rifle grenade using bullet trap

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3048206C2 (de) * 1980-12-20 1985-06-13 Diehl GmbH & Co, 8500 Nürnberg Übungsgeschoß
JPS6058760A (ja) * 1983-09-09 1985-04-04 Mitsubishi Electric Corp 通報装置
GB8622646D0 (en) * 1986-09-19 1987-02-04 Smith J L C Minefield penetration
JPH01249616A (ja) * 1988-03-30 1989-10-04 Hisakatsu Sato 公害防止用もみがら活性炭の製造法とその装置と利用法
JP2022003373A (ja) 2020-06-23 2022-01-11 キヤノン株式会社 位置合わせ装置、マークの位置を求める方法、プログラム、リソグラフィ装置、および物品製造方法

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2415803A (en) * 1944-12-23 1947-02-18 Abell Royal Allen Cartridge
US2968870A (en) * 1958-02-20 1961-01-24 Energa Sighting device for rifle grenades and the like
US3243909A (en) * 1964-11-23 1966-04-05 Inventors League Inc Grenade launcher
US3726036A (en) * 1970-07-09 1973-04-10 Brunswick Corp Launch tube assembly
US3726226A (en) * 1971-08-31 1973-04-10 Us Army Universal smoke marking grenade for dry and inundated areas

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE306500C (cs) *
GB190910494A (en) * 1909-12-03 1910-12-05 Frederick Marten Hale Improvements in and pertaining to Projectiles.
FR503200A (fr) * 1917-02-07 1920-06-04 Eugene Andre Francois Naud Grenade à fusil à grande portée
FR644598A (fr) * 1927-10-26 1928-10-10 Grenade perfectionnée et son dispositif de lancement pour l'extinction à distance des incendies
BE357116A (cs) * 1929-01-05
US2737892A (en) * 1948-12-14 1956-03-13 Patrick J Dalton On-off self destruction base fuze

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2415803A (en) * 1944-12-23 1947-02-18 Abell Royal Allen Cartridge
US2968870A (en) * 1958-02-20 1961-01-24 Energa Sighting device for rifle grenades and the like
US3243909A (en) * 1964-11-23 1966-04-05 Inventors League Inc Grenade launcher
US3726036A (en) * 1970-07-09 1973-04-10 Brunswick Corp Launch tube assembly
US3726226A (en) * 1971-08-31 1973-04-10 Us Army Universal smoke marking grenade for dry and inundated areas

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4493263A (en) * 1981-11-16 1985-01-15 Carabateas Eustratios N Ballistic propulsion system
US4708061A (en) * 1986-02-22 1987-11-24 Hilti Aktiengesellschaft Explosive powder charge operated driving device
US5583314A (en) * 1994-05-19 1996-12-10 Luchaire Defense Sa Firing indicator device for a projectile, and rifle grenade equipped with a firing indicator device
US20050188886A1 (en) * 1996-11-18 2005-09-01 Pepperball Technologies, Inc. Non-lethal projectile systems
US20090266262A1 (en) * 2003-02-10 2009-10-29 Pepperball Technologies, Inc. Stabilized non-lethal projectile systems
US20060011090A1 (en) * 2004-04-09 2006-01-19 Pepperball Technologies, Inc., A Delaware Corporation Primer launched projectile systems
US20080017179A1 (en) * 2004-05-12 2008-01-24 Pepperball Technologies, Inc. Compressed Gas Cartridge Puncture Apparatus
US20090071459A1 (en) * 2007-09-18 2009-03-19 Pepperball Technologies, Inc. Systems, methods and apparatus for use in distributing irritant powder
US7752974B2 (en) 2007-09-18 2010-07-13 Pepperball Technologies, Inc. Systems, methods and apparatus for use in distributing irritant powder
US8196513B1 (en) * 2009-12-04 2012-06-12 The United States Of America As Represented By The Secretary Of The Navy Stand-off disrupter apparatus
CN103075919A (zh) * 2013-01-28 2013-05-01 马永忠 一种爆炸式催泪弹
US9671204B2 (en) * 2013-08-23 2017-06-06 Hanwha Techwin Co., Ltd. Rifle grenade using bullet trap

Also Published As

Publication number Publication date
NL7316819A (cs) 1974-06-11
ATA1017773A (de) 1976-09-15
FR2209921A1 (cs) 1974-07-05
JPS506200A (cs) 1975-01-22
FR2209921B1 (cs) 1977-06-10
AT337052B (de) 1977-06-10
DE2259861A1 (de) 1974-06-12
IT997941B (it) 1975-12-30
MY7700258A (en) 1977-12-31
BE808371A (fr) 1974-03-29
GB1448993A (en) 1976-09-08

Similar Documents

Publication Publication Date Title
US3882780A (en) Rifle grenade, particularly for firing tear gas or flare projectiles
US2764092A (en) Impact fuze for projectiles
US5107766A (en) Follow-thru grenade for military operations in urban terrain (MOUT)
US20060169165A1 (en) Super long range crash-bang round
US4574702A (en) Armour-piercing high-explosive projectile with cartridge
US20020088367A1 (en) Non-lethal ballistic
US4947753A (en) Stun grenade
US9127920B2 (en) Pyrotechnic slug
US2697400A (en) Projectile with shaped charge and point initiating fuze
US5945629A (en) Fuseless ballistic explosive projectile
HU218748B (hu) Kis, közepes vagy nagy űrméretű fegyverhez való lőszer, kilövőköpenyhez hozzárendelt űrméret alatti nyíllövedékkel
UA126700C2 (uk) Снаряд з піротехнічним бойовим зарядом
US3101053A (en) Combination fragmentation structural incendiary damage projectile
RU2439473C1 (ru) Управляемый реактивный снаряд
KR940004649B1 (ko) 폭발탄체를 갖춘 산탄총 카트리지
US3724381A (en) Tear gas element
US4449456A (en) Safety device for a projectile
US2717552A (en) Perforating explosive projectile
EP2083239B1 (en) Warhead with multiple effect units
US3211098A (en) Cartridge for practice firing
US5196646A (en) Dual purpose fuze
US2579323A (en) Rocket projectile
JPH06221800A (ja) 砲身前域用安全信管および該砲身前域用安全信管を装備した砲弾
US3848530A (en) Shot obturation system for fully telescoped caseless ammunition
RU2084812C1 (ru) Бронебойная пуля