Abstract: A high efficiency, blow-by reducing obturator for a 105 mm tube-launched projectile is a generally annular ring having a central longitudinal axis and an outer circumferential surface. The outer surface has a first portion parallel to the central longitudinal axis and a second portion adjacent to the first portion. The second portion extends forward and radially inward at an angle of about six degrees with the central longitudinal axis. In some embodiments, one or more grooves are formed in the inner circumferential surface of the ring.

Abstract: The invention relates to a safety arming system for an explosive charge. According to the invention, the system comprises: an arming actuator (4) for moving a sleeve (19), supporting a detonator (20), from a fixed safety position to a fixed armed position; and a disarming actuator (5) arranged opposite the arming actuator (4) and capable of returning the sleeve (19) from the fixed arming position to the fixed safety position.

Abstract: A stab type fuze mechanism, such as the 30 mm M759 fuze mechanism, which utilizes a generally horse shoe shaped configuration anti-setback spin clip initially lodged in a grove within the body of a target sensing probe, but extending partially therefrom, which extending part rests against a ledge within the aluminum o-give—located rearward from the target sensing probe; thereby preventing the target sensing probe from moving rearward within the fuze during firing and setback. After firing, with the onset of spin, the anti-setback spin clip will open, expanding away from, out of, and clear of the grove and into a cylindrical channel in which the target sensing probe is lodged. Due to a thinned area at the apex of the clip, the expansion of the anti-setback spin clip will be a plastic deformation and the clip will remain expanded.

Abstract: An anti-mine dart includes a body containing an explosive payload and having a flyer-plate port. The dart is operable responsive to the payload being detonated to propel through the flyer-plate port a flyer plate having sufficient energy to detonate an explosive material surrounding the dart. The darts may include a plurality of explosive payloads, flyer-plate ports and flyer plates. The darts may be formed in a stack arrangement within a missile such that the flyer-plate port of each dart is not aligned with the flyer-plate ports of any of the adjacent darts in the stack arrangement. The darts may contain a simplified safe-and-arm mechanism or no safe-and-arm mechanism at all.

Abstract: An impact part on a projectile permits the activation of detonation systems within a large angular range of contact with a target. The impact part is provided with annular recesses with embedded circular rings that engage with the target and prevent the projectile from rebounding. A thin-walled, dome-shaped tip prevents relatively large disruptive effects upon the projectile's hollow charge. As a result of dimensioning the impact part in accordance with the rules of fracture mechanics, it is possible to achieve a desired fragmentation on the target.

Abstract: A fuze device for use with a detonator on munitions. A cup and ogive assembly includes an ogive post for aft axial movement upon impact of the device and activation of a spitback lead on the cup. An ogive post activates a first firing pin when the ogive is crushed. A first safe and arm (S&A) device is aligned with the centerplate assembly to provide a first detonator in both the safe and the armed condition by movement of a rotor. A second firing pin is positioned below the first S&A device. It has a blowthrough hole for alignment of the first detonator with the spitback lead. A second S&A device is below the first S&A device, and has a second detonator and rotor that rotates during spin to an armed position to expose the second detonator to the second firing pin. The second rotor is sized and shaped to always permit alignment of the first detonator with the spitback lead.

Abstract: A fuse-less ballistic explosive projectile (1) with a great fragmentation effect has a secondary explosive (50) with a special structure (75), the secondary explosive detonating upon impact. The secondary explosive (50) surrounds within a projectile cap (24) a conical projection (30) of a penetration core (18). Transmission of the firing effect from the secondary explosive (50) is effected through a central through bore (40) of the penetration core (18) to a large-volume bursting charge (60) arranged in a projectile body (10).

Abstract: The invention relates to a tandem warhead with a preliminary charge (1) and a main charge (2) respectively each with an associated fuse (3, 4).So that on ignition two fuses (3, 4) which are completely identical can be used, piezoelectrical percussion fuses (3, 4) are used which can be triggered by shockwaves. To establish the delay period of the fuses (3, 4) the housing construction, the arrangement of the fuses (3, 4) and the material composition of the housing (5) are to be selected in such a way that the propagation time of the shockwave imparts the required delay period.

Abstract: Triggering a pyrotechnic charge. The contactor comprises:a supporting base (6), made of insulating material, having at least two conducting terminals (7 and 8),a contact sleeve (13) centered coaxially on the base, in contact with one of the terminals and having fingers urged centrifugally by elastic elements (22),a deformable conducting case (24) in contact with the second terminal,and a conducting slide (28) movable by inertia on the axis of symmetry against the action of a retaining spring (31).Application as an impact contactor for projectiles.

Abstract: In a fuse arrangement, which can be used in both low velocity and in high velocity gun-launched grenades, which has a rotationally responsive fuse timing mechanism arranged in a fuse casing, The fuse casing being tiltable and axially movable upon impact of the grenade thereby forcing the entire fuse housing toward a fixed firing pin and detonating the grenade.

Abstract: The base fuze of a spinning projectile possesses a detonator capsule which is pierced by a firing pin. The firing pin is connected to a hammer sleeve. An inertia body is arranged behind the hammer sleeve in order to improve the response sensitivity of the base fuze. Upon impact of the projectile at the target, the inertia body, due to the inertia thereof, drives the firing pin conjointly with the hammer sleeve against the detonator capsule. This inertia body is subdivided into a number of sector-shaped portions which contain substantially cylindrical sections and truncated conical sections. A bore of a fuze housing within which the inertia body is arranged possesses a shoulder. This shoulder serves to support the truncated conical sections of the inertia body such that due to the spin of the projectile an axial force is produced which acts upon the inertia body causing it to impact against the hammer sleeve.

Abstract: A switch is adapted for use in a projectile for actuating an electrical explosives-igniter in response to impact of the projectile. The switch includes a stationary electrical contact and a movable electrical contact. An actuator moves the movable contact against the stationary contact to complete an electric circuit in response to projectile impact. The actuator comprises a ball movable toward the movable contact. The ball is seated in a conical recess to enable the ball to move toward the movable contact even when the projectile does not impact along its longitudinal axis. The movable contact may comprise a cone-like array of flexible arms which engage the ball; movement of the ball flexes one or more of the arms into engagement with the stationary contact. Alternatively, the movable contact may comprise a linearly movable bolt engaged by the ball. A movable weight may be positioned behind the ball and adapted to engage the ball upon projectile impact to urge the ball toward the movable contact.

Abstract: A multi-path impact type, inertia class, igniter for use with both rotating and non-rotating projectiles or warheads includes two or more stab type "firing pins" that are arranged in a plane which is at 90.degree. to the center-line of the projectile. The firing pins are equally spaced apart on the plane and each bears directly upon a safety rupture-disc. The rupture-discs bear directly upon stab type primers, there being one primer per disc. Each firing pin has a sloped "conic" surface forming a cam which is in direct contact with a conic body-of-rotation inertia mass which lies on the projectile center-line. Upon impact, the conic shaped mass moves forward at a high rate forcing the firing pins outward at a much reduced velocity relative to that of impact. The moving firing pins pierce the rupture-discs and enter the stab primers, thereby causing the actuation of the latter.

Abstract: A void-sensing fuze whose initiation is deferred until after impact forces have terminated. A safety device safeties the fuze until after the ordnance has fired. Thereafter, upon impact the fuze is committed to fire, but fires only after impact forces have terminated.

Abstract: An ignition system for projectiles, such as shells, bombs, or rockets is disclosed. The system has a pressure chamber defined by a double-diaphragm switch and a cap of a deformable material. The diaphragm of the double-diaphragm switch, which defines one wall of the pressure chamber, contains one or several perforations, the number and diameter of which depend on the spacing of the diaphragms, the areas thereof and the size of the pressure chamber. The double-diaphragm switch is connected to an electric ignition unit. An electrical circuit is closed only if a projectile housing a percussion fuse and the ignition system impacts on the ground or target after its flight. Any unintended ignition during firing or due to brief impact stress cannot occur.

Abstract: A device for underwater missiles for use against submerged submarines, said missiles including a housing (1) having a front portion, intended to contact the outside surface of a submarine. According to the invention, a tubular ring member (6) is rotatably attached to the front portion of the housing (1), said ring member (6) being arranged to take up a rotary movement in relation to the housing (1) when contacting the outside surface of a submarine. In order to facilitate rapid acceleration of the ring member (6) into said rotary movement, the ring member (6) is attached to the housing (1) by means of a ball bearing joint (7) or any other known low-frictional rotary joint or connection, and the mass of the ring member (6) is also considerably smaller than the total mass of the missile. The outer surface(s) of the ring member (6) is/are also preferably arranged with means intended to increase the frictional contact between the ring member (6) and the outer surface of a submarine on impact, e.g.

Abstract: A fuze has a firing pin slidably mounted in a frame. A detonator mounted in he frame is operable to slide into alignment with the pin. An impact sensor can engage and restrain the pin. This sensor is pivotally mounted in the frame and is operable to disengage the pin in response to deceleration of the frame in excess of a predetermined magnitude.

Abstract: An omni-directional impact actuating mechanism for utilization in actuating a system such as a munition device. By utilizing a multi-directional impact sensor the munition device becomes omni-directional in that it can be detonated when receiving an impact force from any angle. The omni-directional actuating mechanism includes: an actuating member which is movable between a first position and a second position, a control mechanism for switching the actuating member between its two positions and an impact sensor which serves to operate the control mechanism for switching the actuating member. The control mechanism itself is switchable between a first condition for initially applying a force for restraining the actuating member in its first position and a second condition for subsequently applying a force for moving the actuating member into its second position.

Abstract: An elongated, aerodynamically improved ballistic projectile fuse, having an overall fuse length greater than its maximum diameter by a factor of approximately two, includes a lightweight aluminum fuse body having forward and rearward portions and an interiorily disposed firing pin with a shearable flange thereon. A steel sleeve mounted in the fuse body is provided for supporting the firing pin with a head portion thereof forwardly directed and exterior to the sleeve and for guiding the firing pin through the fuse body toward the rearward portion thereof subsequent to impact of the fuse with a target. A cap, enclosing the firing pin head, is configured for collapsing and impacting the head upon fuse impact with a target, thereby causing shearing of the firing pin flange and driving of the firing pin rearwardly toward detonation means disposed within the fuse body rearward portion. The cap is in turn enclosed by a windscreen which provides an aerodynamically streamlined, forward continuation of the fuse body.

Abstract: A low cost graze sensor fuze arrangement for a point detonating spin stabzed projectile in which firing pin actuation for detonation purposes is accomplished where the projectile may only graze the target and a graze sensor element will be laterally moved a limited amount to cam a firing pin assembly rearwardly toward a rotor armed detonator.

Abstract: A low cost graze sensor fuze arrangement for a point detonating spin stabzed projectile in which firing pin actuation for detonation purposes is accomplished where the projectile may only graze the target and a graze sensor element will cam a firing pin assembly rearwardly toward a rotor armed detonator.