发明名称 BALLAST-TYPE PULSEJET ENGINE
摘要 FIELD: rocketry, applicable in production of rockets of various purpose. ^ SUBSTANCE: the engine has a guide, to which a ballast limiting the unconfined space of the guide is fastened with the aid of fixing members. The ballast has a cavity, in which the propellant powder charge is positioned. Powder is ignited by a pyroinitiator, whose combustion products get into the unconfined space of the guide. The ballast inner cavity through a discharge opening is gas coupled to the unconfined space of the guide. ^ EFFECT: enhanced reliability of the ballast-type pulsejet engine and improved mass characteristics due to organization of stable burning of the powder charge. ^ 1 dwg
申请公布号 RU2247913(C1) 申请公布日期 2005.03.10
申请号 RU20030134356 申请日期 2003.11.26
申请人 发明人 ZAKHAROVA T.I.;IOFFE E.I.;KONJUKHOV I.V.
分类号 F41A1/00 主分类号 F41A1/00
代理机构 代理人
主权项
地址