This invention relates to fragmentation beam ammunition capable of simultaneous axial and circular fields of injury.
Known is a fragmentation-beam projectile comprising a casing with a monolithic head section having an axial channel, an explosive charge with a detonator located in the middle section of the charge, a head section trajectory-contact fuse electrically connected to the detonator, a fragmentation unit located between the casing and the fuse and externally enveloping the projectile head section, and a screw-in bottom with stabilizing fins (RU 2327948, publ. Jun. 27, 2008).
Said composite fragmentation unit comprises fabricated destructive elements in a binder matrix.
The main disadvantage of said known projectile is the fixed axial field shape of the fabricated destructive elements which does ensure reliable destruction of tank threatening targets of different classes (single, grouped including groups of different configurations, ground, air etc.). Another disadvantage is the possibility of incomplete destruction of the fragmentation unit following explosive charge detonation in the projectile. Yet another disadvantage is the large diameter of the axial channel in the charge necessitated by the installation of a detonator with a safety device and reducing the strength of the projectile casing head section.
The object of this invention is to provide a projectile while eliminating the above disadvantages.
In accordance with the technical result of this invention, the projectile comprises an elongated explosive charge with a detonator located coaxially with the fragmentation unit wherein said detonator is electrically connected with the fuse and said fuse comprises a device (an adapter booster) for varying the time interval between the activation of both detonators depending on the setting, said detonators comprising safety devices.
This invention will now be illustrated with the drawings hereinbelow:
The projectile comprises the casing 1 with a monolithic conical or ogival head section filled with the composite explosive charge 2. The head section has the small-diameter axial channel 3. Adjacent to the projectile head section is the fragmentation unit 4 with the electronic trajectory-contact fuse 5. The fuse comprises the head contact unit 6 and the settings receiver device 7. The multi-cored electrical conductor 8 connects the fuse with the detonator-safety device unit 9 of the fragmentation unit charge 10 and the projectile charge detonator 11. The unit 11 is located in the head section of the projectile 2 and is flush with its rear surface. The rear projectile section has the screw-in bottom 12 with the stabilizing fins 13 attached thereto.
The fragmentation unit 4 is a composite structure comprising fabricated destructive elements fabricated of steel or tungsten base heavy alloys and a binder matrix e.g. cold cured epoxy compound. The fabricated destructive elements can have a shape allowing their tight packing. One possible embodiment is the use of metallic powder as the binder (powder pressing technology of the fragmentation unit).
Also possible is fragmentation unit embodiment in the form of a predesigned disintegration unit. The whole-bodied unit can be fabricated by sequentially coating the projectile surface with molten metal drops formed by exposing an electrode inserted into the melting zone to a laser or electron beam (V. A. Odintsov, Fragmentation-Beam Tank Projectiles with Additional Penetration and High-Explosive Capability. Defense Engineering, 2010, No. 3).
The fragmentation unit should satisfy two competitive requirements:
The choice of size ensuring sufficient fragmentation unit strength is discussed elsewhere (RU 2327948, publ. Jun. 27, 2008).
A gap with the dimension Δ filled with an inert and easily compressible material is provided between the fragmentation unit charge 10 and the casing 1. The gap dimension calculated based on the admissible impact of fragmentation unit charge explosion on the projectile casing is 6-8 mm.
Possible subcaliber projectile embodiment (
The projectile is programmable and provides the following functionality depending on the settings:
Before the shot the tank fire control system determines target type, distance, azimuth relative to the tank, target configuration for grouped targets and the required fuse settings.
For trajectory destruction the tank's fire control electronics calculates the flight to destruction time, the destruction height, the optimum projectile and fragmentation unit charge explosion time interval and the gun firing elevation.
Fuse settings are contact or contactless entered into the fuse through the settings receiver device 7.
For trajectory destruction the axial field and the meridian beam angle distribution of the fabricated destructive elements depend on the preset time interval between the explosions of the two charges.
The projectile charge detonator location in the middle section of the charge increases the meridian emission angle Ψc of natural casing fragmentation particles (
Correct choice of the projectile head section components and the time interval between the explosions of the two charges provides for a close to zero “dead” angle between the two fields, i.e. the local damage zones (zone I developed by the radial field of the projectile natural fragmentation particles and zone II developed by the fabricated destructive elements of the axial beam) should be “patched”.
The condition of ground target T coverage by the joint field at the projectile explosion height H is expressed as L>6σz, where σz is the RMS deviation of the explosion point from the design position.
For large air targets, primarily, antiarmor helicopters, the optimum projectile destruction distance and the time interval between the explosions of the two charges are set taking into account the coordinates and projections sizes of equally vulnerable target components on the projection plane. The latter are determined by the tank fire control system before the shot.
For firing with impact action fuse setting, special attention is paid to the destruction of strong (concrete and brickwork) walls for which the fuse is set to large deceleration (penetration and high-explosive action) because it is this setting that provides for successful tank self-defense in urban battle conditions. The projectile strength at the concrete impact moment is provided by its whole-head design and the small axial channel diameter. Strong obstacles are typically destructed with the fragmentation unit safety device activated to prevent the fragmentation unit charge from exploding upon impacting the obstacle. The impact causes destruction of the fragmentation unit followed by partial penetration of the fabricated destructive elements to beyond the obstacle. This largely increases the after-penetration effect of the projectile.
The subcaliber projectile as depicted in
The use of two-component fragmentation unit with low weight of fine sized fabricated destructive elements (0.1-0.3 g), while providing for the destruction of a wide range of targets, also provides for the reliable destruction of tank threatening personnel located within the front projectile emission hemisphere.
The truncated cone shaped intermediate section provided between the cylindrical projectile section and the stabilizing fins improves projectile flowaround and reduces its bottom impedance. Impedance is further reduced by the smaller span of the rigid stabilizing fins. This reduces trajectory velocity loss.
Also considered is fragmentation unit charge embodiment comprising a pyrotechnical charge wherein the detonator is replaced for an igniter.
Number | Date | Country | Kind |
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2011148107 | Nov 2011 | RU | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/RU2012/000653 | 8/9/2012 | WO | 00 | 5/28/2014 |