Abstract: A practice round [10] for use in firearms including a casing [11] holding a projectile [16]. A standard primer cap [20] is detonated to propel the projectile forward. A vent hole [40] in the casing limits the pressure buildup in the casing cavity [17].

Abstract: A modified propellant increment for the propulsion system of an ammunition round includes a body composed of combustible propellant material and having a hollow interior, and a plurality of holes defined through the body which communicate the exterior of the body with the hollow interior thereof. The hollow interior of the body is empty of any propellant other than the propellant material composing the body. The holes are arranged in first and second arcuate rows on opposite planar end portions of the body and ensure complete combustion of the body upon burning thereof.

Abstract: A sub-caliber trainer round that includes a projectile with weighted means or weighting the projectile to the desired weight and the projectile having a rear piston like portion for sliding in a cylindrical bore and having a front portion as a marking means for marking the impact position of the projectile relative to a target. The projectile is designed to be mounted in a cylindrical bore as a shotgun shell with a primer and powder for launching the projectile in much the same manner as a shotgun shell.

Abstract: An exercise firing projectile containing a plurality of pyrotechnic fragmentation devices are expelled from the projectile casing above the target area by an ejection charge, and delay tubes of the fragmentation devices are ignited at the same time by this charge through a central igniter tube contained within the projectile. The active charge of the devices consist of a grainy composite with quick reaction time.

Abstract: A sabot projectile with a propulsion mechanism for utilization in a liner for a barreled firing apparatus. In the projectile, the propellent cage for a projectile with a propulsion mechanism includes hinge-like segments articulated forwardly in the firing direction, which encompass the projectile about the circumference thereof and are rotatable therewith, inasmuch as the segments are held together through the intermediary of a retainer ring.

Abstract: A ceramic munitions projectile, particularly useful for practice or target munitions is provided. The projectile is preferably made of zirconia which is densified by a pressureless sintering method. The projectile has sufficient toughness to withstand acceleration and torque created during projectile firing and trajectory.

Abstract: An initiating device which employs discardable arming members is disclosed. The design qualifies as a low cost, responsive, impact initiating system for a practice projectile. The method is embodied in a sub-caliber flight projectile as part of a mortar training device.

Abstract: A wing-stabilized hollow charge shell constructed as dummy ammunition and having a tail unit (13) of the same caliber comprises a front explosive chamber (1) and a rear explosive chamber (2) and at the end face of the shell case is provided with a detonator rod (4). The entire shell case, including the detonator rod (4), is formed by parts (3, 5, 7) consisting of the same or similar material which are undetachably connected together.

Abstract: The invention relates in particular to hunting ammunition for a fire-arm of the kind having a subcaliber bullet fitted with a feathering, the subcaliber bullet allowing for destabilization on its trajectory beyond a distance travelled outside of the fire-arm.

Abstract: A subcaliber projectile intended for arrow stabilization has its guide assembly set so that the projectile spins around its longitudinal axis and is constructed so that it is unbalanced with respect to its longitudinal axis such that the spinning reaches a critical number of revolutions at a given time during the trajectory of the projectile and the resulting resonance causes destruction of the projectile.

Abstract: A disintegrating projectile for cartridged maneuver ammunition for an automatic weapon. The projectile includes a thin-walled and closed body of plastic-like material. The body includes a circularly cylindrical section which changes into a tapering hollow tip. A rotationally symmetrical, stiffening, one-piece plastic insert, is adapted to the inner wall of the hollow tip and extends longitudinally of the projectile between a rear circular delimitation and a front circular limitation. The insert has the shape of two cups and includes a circular disc serving as a common bottom of the cups which are arranged one behind the other in the longitudinal direction of the projectile. The rear cup has a side wall thickness that constantly increases from the rear circular delimitation to the adjacent face of the circular disc member and the front cup has a side wall thickness that constantly increases from the front circular delimitation to the adjacent face of the circular disc member.

Abstract: A mortar training device which includes full-size, simulated, propelling charges is disclosed. The device enables a trainee to subtract simulated charges, as required, to achieve a desired zone of reduced firing distance, following procedures similar to those used with standard service ammunition. The method is embodied in a sabot projectile having a sub-caliber flight projectile. The system provides zones of firing distance which are approximately one-tenth that of standard service ammunition.

Abstract: A spin-stabilized training projectile provides a reliable reduction of a firing range by means of the special construction of a recess in the body of the projectile. The flight path of the training projectile is adaptable to the corresponding flight path of a corresponding live reference projectile over a distance in a predetermined region of the first portion of the flight path of the training projectile.

Abstract: The invention is a projectile which will not ricochet upon striking a solid object. The projectile has a hull containing a payload cavity with a liquid payload, rotors within the payload cavity, a threaded shaft extending the length of the hull, and propeller fins at the back end of the shaft which make fewer turns than the hull while the projectile is in flight.

Abstract: A practice ammunition system for a rocket launcher having a guide tube for receiving an original rocket, the original rocket including an ignition device which, prior to launch, performs a data exchange via at least one data line with an external fire control unit for the rocket launcher. The practice ammunition system includes a practice rocket having a rocket engine and an igniter for igniting the rocket engine thereof, the practice rocket being insertable in the guide tube of the rocket launcher, a simulator external to the practice rocket arranged for connection with the practice rocket and the fire control unit with the external simulator, after connection with the training rocket and the fire control unit, simulating functions of the ignition device of the original rocket for performing a data exchange dwith the fire control unit and for enabling launching of the practice rocket from the rocket launcher.

Abstract: Arrangement for interconnecting a projectile and a projectile extension component. The projectile and the extension component each incorporates its own connecting element which are capable of being introduced into each other by causing one of the connecting elements to be so deformed as to be retained in its deformed state in the second connecting element. The connecting elements are capable of being introduced into each other with the help of the firing forces whose effect is immediate when the projectile and the extension component are fired from the barrel of a weapon.

Abstract: An arrangement for mob dispersion includes a cannister which is attachable o the flash suppressor, or grenade launcher adaptor. The cannister contains ammo in the shape of short rubber cylinders stacked on one another to form several cylindrical columns.

Abstract: An arrangement for mob dispersion includes a cannister which is attachable o the flash suppressor, or grenade launcher adaptor. The cannister contains ammo, in the shape of short rubber cylinders, stacked on one another to form several cylindrical columns.

Abstract: A target shooting capsule comprising a substantially spherical, nontoxic, soft elastic gelatin capsule having a dry wall thickness of about 0.004 inches to about 0.013 inches, having a diameter of about 0.16 inches to about 0.265 inches, and containing about 0.03 cc to about 0.12 cc of a water washable, nontoxic fill material.

Abstract: Disclosed is a training projectile having the same ballistic characteristic as the operational projectile. The training projectile comprises on elongated body having a L/D ratio of substantially 10-25. Fins are attached to the projectile and are configured to cause a change in rate of spin of the projectile from its initial rate to a rate which is coincident with a critical rate of spin to cause structural failure of the projectile at a predetermined range in flight.

Abstract: A conversion assembly for converting a practice warhead (10) into an armour penetrating warhead (30) is disclosed. The practice warhead (10) is the type having a plastic shell (11) with sockets (20,22) at both ends for receiving a metal ballast, such as a steel rod (24). The conversion assembly consists of a penetrator rod (32) of heavy metal with an outside diameter (D.sub.R) substantially less than the inside diameter of the sockets (20,22) in the shell (11) and two adaptor cups (34) of elastomeric material that are stretched over the ends of the penetrator rod (32) and then fitted into the sockets in the shell. The adaptor cups (34) each have, in the relaxed state, a substantially uniform peripheral wall thickness, an inner diameter slightly less than the outside diameter (D.sub.R) of the penetrator rod (32) and an outside diameter slightly less than the inside diameter of the sockets (20,22) in the shell (11).

Abstract: A practice bomb comprised of a hollow two piece plastic shell having lug assemblies therein which aid in retaining the shell halves together notwithstanding the large stresses and strains placed on the bomb during its flight and launching and also releasably suspend the bomb during the transportation of the bomb to the target.

Abstract: A bullet for muzzle loading black powder rifles having an elongated cylindrical metal body. The metal body includes a front paraboloidal segment and a recessed base. A rear expansion band for initially guiding the bullet into the rifled bore and for tightly sealing the explosive gases upon firing of the rifle. A front rifling band which is cut by the lands of the rifling to cause rotation about the longitudinal axis of the bullet. An intermediate knife-like cleaning band which removes residue from the rifled bore as the bullet is propelled outwardly by the explosive gases.

Abstract: A frangible projectile comprising a plurality of interfitting, filled polymeric portions is provided with controlled properties.

Abstract: A supersonic nonspinning training projectile has a projectile body extending along an axis and having axially spaced front and rear ends and an aerodynamic rod projecting axially forwardly from the front end of the body. Thus when the projectile is fired axially forward the rod creates turbulence effective laterally on the projectile body at a wind-attack point which moves axially forward from a rear point to a front point as projectile speed drops. It is possible according to the invention to vary the mass distribution of the projectile and thereby displace the center of mass of the projectile axially between the front and rear points. Thus when the wind-attack point moves axially forward of the center of mass the flight of the projectile destabilizes. Such an arrangement works well even at supersonic speeds, so that the projectile can be set to only fly accurately through a relatively short range, as the principal factor determining range after elevation is projectile speed and shape.

Abstract: A pointed splitter is placed in the body of a soft, rocket-powered training issile with the point toward the rocket motor in the rear. Upon impact, the motor is split and fragments thereof spread transversely so that the force of impact of the motor is reduced.

Abstract: The present invention contemplates electronic ammunition for simulating live ammunition detonation when utilized with an ammunition firing device having a mechanism for firing ammunition when triggered wherein an electronic sound assembly is disposed within a component space within a shell and the shell is loaded within the ammunition firing device. The electronic sound assembly has recorded therein the sound of the detonation of live ammunition and is adapted for providing the live ammunition sound in an audibly perceivable form in a play mode in response to receiving a triggered signal.

Abstract: The specification discloses a plastic bullet having improved accuracy and reusability. The bullet comprises a projectile, including a body and a stud, and a casing, defining a chamber for closely receiving the projectile stud. The projectile body has a reverse frustoconical shape and a blunt forward end defining a spherical segment depression. A plurality of pockets are defined by the body about its circumference. Both the case chamber wall and the projectile stud include interfitting serrations having different axial spacings to improve compression and releasability during firing. The projectile is hollow having a wall-mass-to-diameter ratio providing an improved gyroscopic effect. The casing includes a thick-wall blast chamber providing improved strength and reusability and enabling the use of high force primers.

Abstract: A practice projectile for large-caliber cannons corresponds, over a first flight trajectory portion, to a combat projectile in trajectory and target strike position. At the beginning of a second flight portion, the projectile self-destructs to prevent flight of projectile parts out of the second flight portion. This is attained by a plurality of mutually independent pyrotechnic delay charges which are triggered upon firing and, after burning down, ignite gas generators. The pressurized gas generated by the gas generators ruptures the suitable designed projectile connection. The individual projectile components are separated from each other either by the pressurized gas and/or through the static air pressure and through the residual rotation of the projectile.

Abstract: The practice projectile of this invention has a variable projectile range when fired from the barrel of a firearm. The projectile comprises a shell body portion having a front end section and a rear end section and includes an outer surface, an inner gas-conveying passage, propellant gas ingress openings and propellant gas exit openings. The outer surface includes an outer, caliber section which contacts the inside surface of the barrel out of which the projectile is fired. The outer caliber section is located intermediate the front and rear end sections. The inner gas-conveying passage extends between the front end and rear end sections. The propellant gas ingress openings are located in the rear end section and openly connect the rear end section of the inner gas-conveying passage to the outside of the shell body. The propellant gas exit openings are located in the front end section and openly connect the front end section of the inner gas-conveying passage to the outside of the shell body.

Abstract: A training cartridge has a plastic projectile or plastic dummy projectile wherein the projectile or dummy projectile is integrally molded on a synthetic resin sleeve open at the rear end. The sleeve is inserted in a cartridge case of metal open at its front end. The cartridge case with case shoulder and case neck formed thereon is made to be open also at the rear end so that the synthetic resin sleeve can be inserted from the rear end into the cartridge case in close contact with the inner wall thereof. A separate metallic bottom piece is inserted into the rear end of the cartridge case, sealing the case tightly toward the rear.

Abstract: A projectile is adapted to be launched from a barrel. The projectile incls a tubular housing and a structural member. The tubular housing has a forward inlet throat and aft nozzle. An annular layer of solid fuel combustible material is mounted within the housing between the inlet throat and nozzle. The structural member is detachably mounted over the nozzle. The structural member is sized to cover the nozzle so that pressurized gas applied to the structural member forwardly thrusts the housing. Thus, the projectile is gun-launchable and can produce a ramjet action.

Abstract: In a practice ammunition including a self-destruct, fin-stabilized subprotile containing an elongated body composed of a plurality of mating segments having means for releasably holding said segments together, the means includes a heat sensitive nose cap including a pyrotechnic composition, which contains a fuel and an oxidizing agent. The nose cap holds the forward portions of the segments together, and due to the pyrotechnic composition, is adapted to burn and disintegrate essentially instantaneously in flight at a predetermined aerodynamic temperature to release the segments, whereby the distance at which the subprojectile self-destructs in its trajectory can be realized more accurately and reliably.

Abstract: A device comprising an infrared signature cloaking round forming part of the ammunition load of a cannon-armed vehicle provides an immediate response to a hostile threat from IR tracked or IR guided weapons by forming, when fired from the cannon, a mist that absorbs, scatters, reflects, refracts, or diffracts the infrared signature of the vehicle.

Abstract: A spin-stabilized training missile is equipped with a stabilizer device for reducing spinning in order to decrease the flight range. The training missile is designed so that its stabilization attainable solely by the spin upon firing is not sufficient for a stable flight in the practice range. The required additional stabilizing in the practice range is obtained by a stabilizer device or control airfoil effecting simultaneously, after leaving the practice range, such a spin reduction that the training missile becomes unstable and the range of flight is controlled.

Abstract: A testing and/or practice projectile assembly for preselected use in an artillery weapon in lieu of conventional live ammunition. The projectile assembly includes a casing which has an axial length which is less by a predetermined distance than that of the conventional live projectile. An insert member is operatively mounted in said casing. The length and diameter of the insert member is such that the exterior contour and total length of the projectile assembly (insert member and casing) corresponds to that of a conventional live projectile when the insert member is operatively mounted on the casing. The insert member has an annular recess and guide band segments are mounted in the recess. The guide band segments are pressed outwardly to conform to a predetermined exterior guide band diameter and can be selectively retractably released. A pull rod is coaxially connected to the insert member and band segments via a biasing cone so as to selectively release the band segments.

Abstract: A training cartridge has a synthetic resin projectile or dummy projectile wherein the projectile or dummy projectile is integrally molded to a synthetic resin sleeve or tube open at the rear end. The sleeve is inserted from the front end of a cartridge case of metal that is open at its front end. The sleeve is held within the cartridge case by drawing the cartridge case inwards, after insertion of the synthetic resin sleeve, in its frontal zone to form a conical case shoulder and a cylindrical case neck, which shoulder and neck encompass the synthetic resin sleeve in firm contact therewith. This arrangement achieves clean separation of the projectile from the remainder of the synthetic resin sleeve and/or avoids uncontrolled tearing off of parts of the synthetic resin sleeve.

Abstract: The invention disclosed relates to an inexpensive practice warhead for use in conjunction with combat rockets. The novel warhead is basically the same configuration and weight as conventional metal warheads, but is constructed of an inexpensive plastic material, the weight difference being made up by providing ballast means within the hollow core of the warhead.

Abstract: A target practice system including reusable cartridges for firearms and a bullet trap for stopping the flight of projectiles from the cartridges. The case of the cartridge is adapted to receive the projectile, or alternative standard cases may be used. The projectile has a cylindrical core of a diameter less than the rifling of the firearm and axially spaced-apart, outwardly opening channels extend circumferentially about the core. Endless resilient rings are inserted into the channels. A powder-receiving hole is provided in the rearward end of the projectile. When fired, the projectile rides on the resilient rings as it travels down the barrel of the firearm. The core does not come in contact with the barrel, and the resilient rings center the core in the barrel during travel down it for improved accuracy. A rocket-like effect is realized from the rearward discharge of gases liberated by combustion. Also, methods of loading the reusable cartridges are disclosed.

Abstract: A polyamide molding composition filled with fine particulate metals for injection molding into practice hand grenades and shells which disintegrate into small pieces.

Abstract: A round of ammunition for use in training comprises a standard brass cartridge case (1) containing a reduced propellant charge (14) and a bullet (2) of standard shape comprising a core (3) of rigid polyurethane foam and an external skin (14) of unfoamed polyurethane. The core and skin can be moulded integrally. The round is designed for firing in an automatic weapon and actuating its automatic mechanism. The skin of the bullet should be not less than 0.02 mm thick to withstand handling, and not more than 0.10 mm thick to avoid production of large fragments thereof on firing. The bullet can have opposite ends both of ogival form to facilitate manufacture and operation. The round is mainly for small arms up to 10 mm caliber.

Abstract: A dummy cartridge or ammunition is disclosed comprising a cartridge case containing a case floor portion, a substantially cylindrical case wall, a substantially conical shoulder portion and a mouth portion. A dummy body member or projectile is inserted into the cartridge case and bears against the case floor portion. Means serve for securing one end of the dummy body member to the floor portion of the cartridge case, whereas a further portion of the dummy body member is attached to the mouth portion of said cartridge case. The dummy body member possesses a substantially cylindrical hollow compartment having a forward portion. An adjustable trim body is inserted into the forward portion of the hollow compartment, in order to place the center of gravity of the dummy cartridge at a predetermined desired position.

Abstract: A full-caliber shell for training purposes to be fired with a low charge in a large-caliber firearm, e.g. a howitzer or a gun. THe shell comprises a front part (1) made of heavy material and an effect part casing (2) and a bottom unit (3) substantially made of plastic material which is highly resistant to high pressures. The effect part casing comprising the effect part and the bottom unit is arranged to withstand the great stress forces which arise in connection with the firing of the shell in the howitzer when the heavy front part is to be accelerated by means of said effect part and bottom unit. The stress forces are then very pronounced, and are of the magnitude of those arising in connection with the firing of a steel shell with the corresponding charge.

Abstract: A fin-stabilized projectile having a sabot which forms a practice projectile with a sub-caliber projectile including a sabot whose base includes a passageway for propellant charge gases and a projectile component which is displaceable by the gases.

Abstract: A finless non-spinning round is able to maintain range accuracy and reduced un tube wear by the use of a single base cool burning propellant, an improved shape wear liner, and a warhead projectile configured to position the center of gravity of the warhead so that it is equal to or greater than 0.5 calibers forward of the warhead's aerodynamic center of pressure.

Abstract: Exercise projectile substantially of a configuration defined by a pointed head prolonged by a tail-piece, characterized in that the projectile contains at least one explosive charge and an associated device for delayed firing, the duration of the delay substantially corresponding to the statistical flight time of the projectile from its starting time to the end of its intended useful trajectory.

Abstract: An aerodynamic braking arrangement for projectile components which are to be salvaged, such as detonators, consisting of a drag parachute having a high air-resistance index and of cables which connect the projectile components with the parachute. The drag chute is formed as a brake basket which consists of two cup-shaped tops at the ends thereof constituted of metal or plastic material, which are separated from each other along the axial direction of the projectile through the intermediary of at least one space formed of metal or plastic material, wherein the cables are fastened to one of the tops.

Abstract: A non-ablative heat sensitive nose cap uses a highly conductive solid ford ogive and rear segmented ogive member, in contact with a low melting point locking ring which is thermally isolated from the main projectile body. The locking ring holds the rear ogive segments together until the desired time for projectile-break. Break-up occurs when a zinc alloy locking ring fails under the combined influence of decreasing yield strength and centrifugal force due to launch and free flight imposed spin.

Abstract: An improved multipurpose projectile obturator of composite, frangible conuction where the obturator preferably forms part of a projectile that is launched from an upstanding tube. The tube interior is provided with an alternating series of helically arranged groove and land means. A projectile at its propellant end is provided with an annular shoulder that faces in a direction toward the propellant end. An obturator is generally made up of an elastomeric band of a suitable grade of rubber. The band in being placed about the projectile surface and against the shoulder is positively retained as the projectile is inserted in the tube and launched therefrom. The outer periphery of the band has an annular groove for receiving a ring-like element. This element is preferably of three-ply construction and is also preferably made up of two half sections that are suitably bonded to the groove about the band periphery.

Abstract: The bullet for a training cartridge has a thin probe extending therefrom to reduce its maximum range. The training cartridge provides realistic trajectory, sound, recoil and sighting accuracy and produces identifiable target penetration with reduced risk of richochet and to create the same cartridge profile as a conventional round but with limited range suitable to training purposes. The thin, elongated probe has a blunted nose and joins the main body of the bullet on a tapered surface.