FIELD: ammunition.
SUBSTANCE: anti-drone ammunition (2) for grenade launcher includes calibre tail part (4) with axial load-carrying rod (5) of front location and calibre head part (6) fixed on the end of the latter with fairing, which form annular cargo compartment (7) for payload. Tail part (4) includes powder propellant charge (7) with ignition cap (8) and rear leading (guide-obturator) band (9), and head part (6) includes front leading (guide-obturator) band (10) and powder burster charge (11). Rod (5) is equipped with powder igniter (12) from propellant charge (7) to burster charge (11). Payload is made in the form of inseparable, by means of leash (13), trapping net (14) with evenly distributed and fixed thereon peripheral metal elements (15) in a stowage. Possibility of dome-shaped opening of trapping net (14) is provided at actuation of burster charge (11), with midsection of opened trapping net (14) exceeding midsection of ammunition (2).
EFFECT: higher reliability of trapping net opening behind ammunition tail part.
5 cl, 5 dwg
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