Helicopter manual инструкция на русском как заряжать
The radiation pattern of these sensors is oriented perpendicular to the warhead axis, and the maximum range depends on the brightness response coefficient reflecting surface and equal to caliber rocket. Primer screens a considerable part of the expanding shell fragmentation explosive charge, reducing the efficiency of fragmentation at targets located on the ground surface, preventing loss goals hidden in the folds of the terrain. This allows for the fastest possible to obtain information about the missile approaching the goal. To minimize response time fuze in the "instant" action target probes are usually placed at the top of the front section of the rocket projectile. The essence of the proposed technical solutions graphic images illustrated in Figures 1 - 3. Installation on the "instantaneous" effect is made to ensure the operation of the warhead on the surface of the target when firing on lightly armored and soft-skinned vehicles, aircraft and helicopters parked, manpower located in the open countryside. Offered warhead operates in two modes: Conducted in flight conditions, the experimental verification of the characteristics of the harmful effect of the missile with high-explosive fragmentation warhead, developed in accordance with the proposed technical solution, confirmed the high efficiency of high-explosive action warhead on such targets as soft-skinned vehicles, vital force on the ground, in vehicles and buildings. The magnitude of the contact load sensors purpose only increase dramatically when approaching the surface of a solid explosive charge target high-explosive action.
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A significant drawback of the prototype design is the placement of the target fuse sensor at the top of the fairing.
Another serious disadvantage of the prototype is the use in all conditions approach to the goal target sensor contact action. This leads to the triggering of an explosive charge, is already partially buried in the ground. Offered warhead operates in two modes: Upon collision with the solid surface of the target at angles close to the normal, the fairing 1 of the warhead is deformed without exerting a noticeable force action on the contact sensors objectives established in the compartment fuse posted from the bottom of the booster charge high-explosive action 4.
This is done by installing a fuse on the "Slow" effect.
RUC1 Highexplosive warhead Google Patents
Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket.
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This suggests that the solution proposed is new and has a sufficient inventive step.
In this case, for example when approaching the soft ground, the missile body will slide along the surface without deformation of the fairing until missile penetration into the ground is not less than half gauge. Therefore, the construction of the profile back in flight part fragmentation shell radius end fragmentation shell zone curvature is expedient to place on the extension line passing through the front on the fly and detonator edge fragmentation shell end see FIG.
Issuance of a command for activation of the sensor occurs when the setpoint braking overload current for a predetermined length of time. A significant drawback of the prototype design is the placement of the target fuse sensor at the top of the fairing.
The essence of the proposed technical solutions graphic images illustrated in Figures 1 - 3.
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This allows for the fastest possible to obtain information about the missile approaching the goal.
Offered warhead for a guided missile comprising 1 the fairing 1detonation device with the active non-contact 2 and the contact 3 target sensors, bursting charge high-explosive action 4 in the bottom of the cavity which is placed slam actuator fuse 5.
The explosive charge is positioned between the fairing and the fuse, uniformly circumferentially positioned on the body side surface are proximity target sensors engageable with the safety-actuating mechanism, whose directional pattern is oriented perpendicularly to the warhead axis, and one or several sensing target sensors are installed on the end face surface of the fuse body, they are engageable with safety-actuating mechanism, whose directional pattern is oriented in the warhead axis.
Comprising a slam-actuator and contact target sensor - 9E product GHG piezoelectric type contact action. Each of the above essential features needed, and their combination is sufficient to achieve a new quality of novelty sverheffekta not inherent features in their separateness.
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|When operating in the "instantaneous" response against targets with a solid body, such as for example light armored vehicles, placement of the contact sensor in the head part of the front section of the rocket triggers the explosive charge at a distance from the target surface, thereby preventing the maximum possible approximation burster to the target surface and reducing the size of the joint high-explosive action.
The reference numerals 6 and 7 respectively show the front in flight and the rear border meridional angle scattering main part fragmentation field lesion. Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket.
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Reflected from the surface of the target signal of the active non-contact sensor allows issuing a signal to actuate slam-actuator fuse 5. This suggests that the solution proposed is new and has a sufficient inventive step.