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Fairing, rocket provided therewith, and method for separating fairing

机译:整流罩,具有该整流罩的火箭以及分离整流罩的方法

摘要

PROBLEM TO BE SOLVED: To provide a fairing with which production costs can be reduced.SOLUTION: A fairing 100 is fitted to an end of a rocket 200 and includes: a first fairing piece 100a and a second fairing piece 100b which separate and open in the direction orthogonal to an advancing direction of the rocket 200. On a bonding surface of the first fairing piece 100a and the second fairing piece 100b, there are arranged a first separation mechanism 11 and a second separation mechanism 12. The second separation mechanism 12 is higher in simultaneity of operation than the first separation mechanism 11 and is shorter in operation time.SELECTED DRAWING: Figure 1
机译:解决的问题:提供一种可以降低生产成本的整流罩。解决方案:整流罩100安装在火箭200的一端,包括:第一整流罩100a和第二整流罩100b,它们分开并打开。在第一整流罩片100a和第二整流罩片100b的结合面上,配置有第一分离机构11和第二分离机构12。与第一分离机构11相比,操作同时性更高,操作时间更短。

著录项

  • 公开/公告号JP6688079B2

    专利类型

  • 公开/公告日2020-04-28

    原文格式PDF

  • 申请/专利权人 川崎重工業株式会社;

    申请/专利号JP20160001548

  • 发明设计人 迎田 健一;

    申请日2016-01-07

  • 分类号B64G1/64;

  • 国家 JP

  • 入库时间 2022-08-21 11:32:44

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