FIELD: weapons.
SUBSTANCE: invention concerns devices for change of atmospheric conditions, in particular, to rockets for influence on clouds. The rocket contains a head part with the aerodynamic shroud with exhaust outlets, a channel draught of an active smoke and the executive mechanism of the self-liquidation including consistently established nozzle, pyrotechnic decelerator and a cap-detonator. Between the case of the head part and the aerodynamic shroud, the final collector with diffusion cell, connected with exhaust outlets is located. The nozzle of the executive mechanism of self-liquidation it is located in the diffusion cell, and a cap-detonator - it is longitudinal and screened from above by reflecting crossbeam. The invention provides increase of efficiency of action of a rocket and reliability of the executive mechanism of self-liquidation.
EFFECT: increase of efficiency of action of a rocket and reliability of the executive mechanism of self-liquidation.
3 cl, 1 dwg
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Authors
Dates
2008-12-10—Published
2007-03-19—Filed