发明名称 SUPERSONIC MISSILE WITH POWDERED METALLIC FUEL ENGINE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: ultrasonic missile contains the body where there located is guidance system equipment, control system equipment, missile warhead, starting power plant and propulsion power plant. Air-intake devices and aerodynamic surfaces are located outside the body. Propulsion power plant is performed in a form of ramjet engine that consists of pre-combustion chamber and combustion chamber connected to air-intake devices and powdered metallic fuel supply system that uses a piston. ^ EFFECT: increase of flight range in larger flight altitude envelope. ^ 2 cl, 1 dwg
申请公布号 RU2410291(C1) 申请公布日期 2011.01.27
申请号 RU20090141287 申请日期 2009.11.10
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "KORPORATSIJA "TAKTICHESKOE RAKETNOE VOORUZHENIE" 发明人 MALININ VLADIMIR IGNAT'EVICH;VINOGRADOV SERGEJ MIKHAJLOVICH;IVANOV OLEG MIKHAJLOVICH;GUREEV VLADIMIR VALENTINOVICH;MARCHENKO ANATOLIJ IOSIFOVICH
分类号 B64D27/02;F02K7/18;F42B15/00 主分类号 B64D27/02
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