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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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