发明名称 METHOD OF ROCKET CONTROL
摘要 FIELD: ammunition.SUBSTANCE: in compliance with this invention, the direction of flow guide surface are varied by the inclining the rocket head and tail.EFFECT: higher aerodynamic properties.2 cl, 5 dwg
申请公布号 RU2583120(C2) 申请公布日期 2016.05.10
申请号 RU20140119312 申请日期 2014.05.13
申请人 FEDERALNOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATELNOE UCHREZHDENIE VYSSHEGO PROFESSIONALNOGO OBRAZOVANIJA "POVOLZHSKIJ GOSUDARSTVENNYJ TEKHNOLOGICHESKIJ UNIVERSITET" 发明人 KUDRJAVTSEV IGOR ARKADEVICH;SOZONOV ALEKSANDR NIKOLAEVICH;DROZDOV NIKOLAJ ANATOLEVICH;KUDRJAVTSEV ALEKSANDR IGOREVICH
分类号 B64C9/04;F42B15/01 主分类号 B64C9/04
代理机构 代理人
主权项
地址