FIELD: weapons.
SUBSTANCE: invention concerns devices for change of atmospheric conditions, in particular to solid fuel rockets for active influence on clouds. The rocket contains a receiver located between the amplifier of the firing impulse and the electrocapsular plug, a nozzle block with central electrocapsular plug, two longitudinal located channel powder draughts established with radial backlashes concerning the case, the amplifier of the firing impulse, a transfer pyrotechnic charge in the form of the cumulative funnel adjoining to the nozzle, executed in a kind of decelerator from the pyrotechnic structure which time of burning exceeds time of burning of channel powder draughts, and a channel draught of an active smoke. The powder draughts are executed with the equal arches of burning, divided by a diaphragm and established in the general case. The relation of sizes of a radial backlash between the case and channel powder draughts inversely proportional to the relation of diameters of channels of the mentioned draughts, and lengths L1, L2 the mentioned draughts are defined from following parities: and where - criterion of Pobedonostsev. Simplification of a design of the jet engine at increase of its functional reliability and more effective influence of a rocket on clouds is provided.
EFFECT: simplification of a design of the jet engine at increase of its functional reliability and more effective influence of a rocket on clouds.
2 dwg
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Authors
Dates
2008-12-10—Published
2007-03-19—Filed