发明名称 MISSILE
摘要 FIELD: rocketry; guided missiles with aerodynamic actuators. ^ SUBSTANCE: proposed missile is made according to standard aerodynamic configuration. It has body where engine, guidance equipment and control systems, fighting equipment, four fixed wings and four aerodynamic control surfaces are arranged. Wings and control surfaces are smoothly distributed relative to longitudinal axis of body. ^ EFFECT: enhanced maneuverability. ^ 6 dwg
申请公布号 RU2234667(C1) 申请公布日期 2004.08.20
申请号 RU20020131042 申请日期 2002.11.18
申请人 发明人 AKIMOV V.N.;BULGAKOVA R.G.;GOL'DENBERG A.M.;KUVSHINOV E.M.;EHKTOV V.P.
分类号 F42B15/00 主分类号 F42B15/00
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