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rocket propulsion systems and rocket propulsion systems Assembly

机译:火箭推进系统和火箭推进系统总成

摘要

The present invention relates to a device and rocket-propelled rocket propulsion systems assemble the rocket propulsion systems to promote I and the embedded part forms the tubular case and , at least some part in the case is inserted and the nozzle unit to discharge the gas generated by combustion of the propellant , and being arranged to sense parts of the nozzle , formed in both ends of the belt-like opening which includes a lock and , in a region of the case portion circumferentially formed ball can be inserted through the locking portion and in the region facing the work area and is characterized in that the locking portion is disposed at both ends . This makes the structure simple and easy alignment of the line of thrust rocket propulsion system is implemented .
机译:装置和火箭推进系统技术领域本发明涉及一种装置和由火箭推进的火箭推进系统,其组装成火箭推进系统以促进I,并且嵌入部分形成管状壳体,并且至少一部分插入壳体中并且喷嘴单元用于排出产生的气体。通过推进剂的燃烧,并布置成感测喷嘴的部分,该部分形成在包括锁的带状开口的两端,并且在壳体部分的区域中,周向形成的球可以通过锁部分插入,并且在面对工作区的区域内,其特征是锁定部设置在两端。这使得推力火箭推进系统的线路结构简单易行。

著录项

  • 公开/公告号KR101055669B1

    专利类型

  • 公开/公告日2011-08-10

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20080107368

  • 发明设计人 이방업;박재범;박성한;문순일;

    申请日2008-10-30

  • 分类号F41F3/04;F41F3/00;

  • 国家 KR

  • 入库时间 2022-08-21 17:49:56

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