发明名称 SUPERSONIC CONTROLLED PROJECTILE
摘要 FIELD: weapons and ammunition. ^ SUBSTANCE: projectile is arranged in accordance with the "canard" aerodynamic design. The projectile comprises a body with a sharpened nose part, a stabiliser and aerodynamic control elements - steers. The shape of the nose part is arranged as combined and comprises the front and rear parts. The front part is arranged with a stepped profile having a spherical blunting with a radius of 0.03Ç0.06 of the projectile calibre. The rear part is arranged with a conical shape having a cone semi-opening angle that does not exceed the angle of inclination of a tangent to the stepped profile of the front nose part in place of their connection. The length of the section with the stepped profile makes 0.25Ç0.75 of the nose part length. The stabiliser is arranged in the form of opening blades, the root chord of which is parallel to the longitudinal axis of the projectile. Swing of aerodynamic control elements - steers - does not exceed swing of stabiliser blades. ^ EFFECT: increased combat effectiveness of a projectile. ^ 1 dwg
申请公布号 RU2459177(C1) 申请公布日期 2012.08.20
申请号 RU20110114483 申请日期 2011.04.13
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "GOSUDARSTVENNOE NAUCHNO-PROIZVODSTVENNOE PREDPRIJATIE "SPLAV" 发明人 MAKAROVETS NIKOLAJ ALEKSANDROVICH;DENEZHKIN GENNADIJ ALEKSEEVICH;BELOBRAGIN BORIS ANDREEVICH;BORISOV OLEG GRIGOR'EVICH;ZAKHAROV OLEG L'VOVICH;PETROV IGOR' PAVLOVICH;BATOV ALEKSANDR GENNAD'EVICH;BAZARNYJ ALEKSEJ NIKOLAEVICH;KALJUZHNYJ GENNADIJ VASIL'EVICH;ZAKHAROV SERGEJ OLEGOVICH;PETROV VALERIJ LEONIDOVICH;VAN'KOV VIKTOR TIMOFEEVICH
分类号 F42B10/38;F42B15/00 主分类号 F42B10/38
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