FIELD: ammunition.
SUBSTANCE: anti-drone ammunition for grenade launcher includes calibre tail part (1) with axial bearing rod (5) of front location and calibre head part (2) fixed on the rod end with fairing, which form annular cargo compartment for payload. Tail part (1) comprises powder propellant charge (14) with primer and rear drive band (3). Head part includes front driving belt (4) and burster charge (15). Cargo compartment is divided axially symmetric by lengthwise baffles (8) into identical cargo sections (9). In each section there is one section (10) of the trapping net with peripheral metal elements (11). Sections (10) of the trapping net are provided with individual leashes (12) which together form said leash. Front wall (13) of tail part (1) of ammunition, which is simultaneously rear wall of cargo compartment, is arranged as inclined, with direct conicity.
EFFECT: increased reliability of trapping net opening outside behind ammunition tail part, reduced drag.
2 cl, 2 dwg
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Authors
Dates
2025-06-06—Published
2024-08-20—Filed