发明名称 NOSE CONE OF ROCKET FOR ACTIVE ACTION ON CLOUDS
摘要 FIELD: hydrometeorological service, meteorological rockets for active action on clouds with the aim of prevention of hail-damage, causing of precipitation. SUBSTANCE: nose cone has a remote-control device with an igniting assembly installed in threaded cavity of nose cone, body with an axial duct filled with igniting- retarding compound and radial ducts accommodating the active smoke generators. The central duct of the nose-cone body with a diameter of 0.098 to 0.17 of the rocket caliber, beginning from depth of 0.14 to 0.27 of the rocket caliber, expands on the taper surface with an angle at the top within 55 to 90 deg. The igniting-retarding compound is positioned below the level of the hole communicating the axial duct with the radial duct at a depth of 0.28 to 0.39 of the rocket caliber. The end of the nose-cone body is positioned at a distance of 1.2 to 3.2 of the rocket caliber from the igniting remote-control device. EFFECT: enhanced efficiency. 2 dwgw
申请公布号 RU2113687(C1) 申请公布日期 1998.06.20
申请号 RU19950114176 申请日期 1995.08.08
申请人 PROIZVODSTVENNOE OB"EDINENIE IM.V.I.CHAPAEVA 发明人 GRISHIN JU.P.;IMBRO G.A.;NESMEJANOV P.A.;SIDOROV A.I.;PONOSOV V.S.;KHOROSHEV G.I.
分类号 F42B12/02;A01G15/00;(IPC1-7):F42B12/02 主分类号 F42B12/02
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