FIELD: military equipment.
SUBSTANCE: invention relates to jet munitions intended for firing from sea (shipborne) grenade launcher systems. Reactive ammunition containing head part with detonating fuze, jet engine with boosting assembly, in parallel connected electric igniter and condenser, arranged in nozzle of jet engine and connected freely laid conductors with external contact buses located on stabilizer. Capacitor is located in the forcing assembly together with the electric igniter on the ammunition rotation axis. Electric igniter is installed in the forcing assembly on the side of the head part, the capacitor is mounted on the opposite side. Conductors are twisted to each other in a single bundle and installed in a protective casing.
EFFECT: technical result consists in improvement of reliability of action and safety of ammunition.
1 cl, 1 dwg
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