发明名称 SOLID-PROPELLANT CHARGE FOR ROCKET ENGINE OF AIRCRAFT ROCKET
摘要 FIELD: engines and pumps. ^ SUBSTANCE: solid-propellant charge for rocket engine of aircraft rocket includes solid-propellant grain armoured along side surface and front edge with a star-shaped channel. Star-shaped channel includes uniformly alternating projections and cavities the height and thickness of which is determined with relationships protected with this invention. Conical turned part is made at the rear edge of charge along outside diameter of the charge at the length of 0.05Ç0.07 of solid-propellant grain length, at an angle of 18Ç20 to longitudinal axis of charge. ^ EFFECT: invention allows improving specific impulse of solid propellant engine thrust and reducing the action of engine flame of the rocket that is launched from under the aircraft fuselage on operability of aircraft engine. ^ 4 dwg
申请公布号 RU2459969(C1) 申请公布日期 2012.08.27
申请号 RU20110112771 申请日期 2011.04.01
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT POLIMERNYKH MATERIALOV" 发明人 MOLCHANOV VLADIMIR FEDOROVICH;KOZ'JAKOV ALEKSEJ VASIL'EVICH;PRIBYL'SKIJ ROSTISLAV EVGEN'EVICH;MAKSJAEV LEONID ANATOL'EVICH;AMARANTOV GEORGIJ NIKOLAEVICH;ARMISHEVA NATAL'JA ALEKSANDROVNA;RYZHKOV GENNADIJ FEDOROVICH
分类号 F02K9/18 主分类号 F02K9/18
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