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System for recovering a spacecraft at sea, method of recovery and use associated therewith

机译:海上航天器的回收系统,回收方法及与其相关的用途

摘要

The invention relates to a system (100) for recovering a spacecraft at sea comprising a frame (110) intended to be kept at distance from the water, a first flexible net (120) for capturing the spacecraft after its fall, the first net being stretched inside the frame, a damping system (130) connected to the first net and configured to cushion the fall of the spacecraft, and a second rigid net (140) fixed to the frame under the first net to guide and recover the spacecraft once captured in the first net, the second net having the shape of a funnel comprising an upper opening (141) and a lower opening (142) having a section smaller than that of the upper opening. The invention also relates to a method of recovering a spacecraft and to using the recovery system to recover a part of a space launcher. Figure for the abstract: Fig. 1.
机译:本发明涉及一种用于在海上回收航天器的系统(100),该系统包括旨在与水保持一定距离的框架(110),用于在航天器坠落后捕获航天器的第一柔性网(120),第一网是在框架内伸展的阻尼系统(130)连接到第一网并配置为缓冲航天器的下落,第二刚性网(140)固定在第一网下的框架上,以在捕获后引导和回收航天器在第一网中,第二网具有漏斗形状,其包括上部开口(141)和下部开口(142),下部开口的截面小于上部开口的截面。本发明还涉及一种回收航天器的方法,并且涉及使用该回收系统来回收空间发射器的一部分。图为摘要:图1。

著录项

  • 公开/公告号FR3088894A1

    专利类型

  • 公开/公告日2020-05-29

    原文格式PDF

  • 申请/专利权人 ARIANEGROUP SAS;

    申请/专利号FR1871786

  • 发明设计人 CÉDRIC CHEYROU;GUILLAUME BARON;

    申请日2018-11-23

  • 分类号B63B7;B63B35;B64F1;B64G1/62;

  • 国家 FR

  • 入库时间 2022-08-21 11:00:27

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