FIELD: weapons.
SUBSTANCE: invention relates to ammunition with a cape for hitting flying drones. Ammunition with a cape for hitting flying drones comprises a body open in front, having an imaginary longitudinal axis, a means of air blasting of an explosive charge, blowing charge, cape with weights and connecting threads. Weights are arranged around an imaginary longitudinal axis. Weights are located with their rear part inside the body. Each load is equipped with a thread. Each thread is attached to the corresponding weight by the first end. In addition, a cartridge is introduced into the ammunition design. Cartridge includes a bushing, rear and front flanges. Outer diameter of the bushing is less than the outer diameters of the flanges. On an imaginary longitudinal axis in the cartridge there is a running hole. In addition, a cover with a front piston is introduced. Front end of front piston is fixed in cover. Rear end of the front piston is located in the running hole of the cartridge. Additionally, rear piston is introduced. Rear end of rear piston is fixed in housing. Front end of the rear piston is located in the running hole of the cartridge. Blow-out charge is located in the running hole of the cartridge between the rear end of the front piston and the front end of the rear piston. Weights are located with their front part inside the cover. In addition, a ring is introduced, which is located outside the bushing of the cartridge. Inner diameter of the ring in the expanded state is greater than the outer diameter of the cartridge bushing. Second end of each thread is attached to the ring. Each thread is compactly laid so that it can be straightened when pulled by its second end. Cover, cartridge, front and rear pistons are located on imaginary longitudinal axis.
EFFECT: increasing the probability of the flying drone hitting by the cape owing to increasing the effective hitting area, as well as reducing the time of the cape straightening.
9 cl, 13 dwg
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Authors
Dates
2024-05-14—Published
2023-09-08—Filed