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TEST SYSTEM OF HYDRAZINE-LIQUID THRUSTER

机译:肼液体冲击器测试系统

摘要

PROBLEM TO BE SOLVED: To provide a test system of a hydrazine-liquid thruster capable of visualizing and acquiring accurately a fluidization state on a catalyst layer of a propellant.;SOLUTION: This test system of the hydrazine-liquid thruster is equipped with a feed tube 14 for supplying a colored simulated propellant having lower toxicity than hydrazine, an injector cover 16 penetrated by the tip part of the feed tube 14, a cylindrical transparent test cell 18 having one end blocked by the injector cover 16, transparent simulated catalyst particles 28 filled in the test cell 18, and a photographing device 30 arranged outside the test cell 18 and photographing the inside of the test cell 18.;COPYRIGHT: (C)2009,JPO&INPIT
机译:解决的问题:提供一种肼液推进器的测试系统,该系统能够可视化并准确获取推进剂催化剂层上的流化状态。解决方案:该肼液推进器的测试系统配有进料用于提供毒性比肼低的有色模拟推进剂的试管14,由进料管14的尖端部分穿透的注射器盖16,一端被注射器盖16堵塞的圆柱形透明测试池18,透明的模拟催化剂颗粒28填充在测试单元18中,并且在该测试单元18的外部布置有照相装置30,并且在该测试单元18的内部照相。;版权所有:(C)2009,JPO&INPIT

著录项

  • 公开/公告号JP2008286581A

    专利类型

  • 公开/公告日2008-11-27

    原文格式PDF

  • 申请/专利权人 IHI CORP;

    申请/专利号JP20070130320

  • 发明设计人 IMAI RYOJI;MATSUNO SHINSUKE;IDETA TAKEOMI;

    申请日2007-05-16

  • 分类号G01M15/14;F02K9/96;F02K9/42;G01P5/20;

  • 国家 JP

  • 入库时间 2022-08-21 19:42:11

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