FIELD: armament.
SUBSTANCE: the guided missile with a radial non-isotropic fragmentation warhead has a control section including the guidance system, roll-stabilized system and the system of non-contact destruct, control surfaces and wings, explosive charge, and a jet solid-propellant engine with a change of solid propellant. The charge of the jet engine is made of a detonationable solid propellant and positioned in the body in parallel with the explosive charge with a tight engagement with it on the lateral surface through an explosion-conducting longitudinal partition.
EFFECT: more rational use of the energy of solid propellant.
10 cl, 7 dwg
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Authors
Dates
2006-08-27—Published
2004-10-28—Filed