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Shield for protecting rocket payload - comprises shells which form releasable envelope for load to protect from rockets of adjacent stage

机译:保护火箭有效载荷的防护罩-包括形成可释放包壳的壳,以承受载荷,以保护相邻级火箭

摘要

The shield for protecting the payload of a rocket from the rockets of an adjacent stage during deployment comprises individual shells (11,12,13) each made up of a rigid frame covered by a flexible sheet. The shells form an envelope which is secured to at least part of the periphery of the load (2). The shells are held together about the load by at least two belts (5,6) which are destructible on command allowing the load to be released into orbit. The shells and belts are in the space between the load and an outer protective housing.
机译:用于在部署期间保护火箭的有效载荷免受相邻阶段的火箭影响的防护罩包括单独的壳体(11、12、13),每个壳体由被柔性片覆盖的刚性框架组成。壳形成包壳,该包壳固定到负载(2)的外围的至少一部分上。壳体通过至少两条皮带(5,6)围绕负载保持在一起,这些皮带可根据命令破坏,从而允许将负载释放到轨道上。外壳和皮带位于负载和外部保护罩之间的空间中。

著录项

  • 公开/公告号FR2522613B1

    专利类型

  • 公开/公告日1984-04-20

    原文格式PDF

  • 申请/专利权人 SOCIETE NALE INDLE AEROSPATIALE;

    申请/专利号FR19820003413

  • 发明设计人

    申请日1982-03-02

  • 分类号B64G1/22;B64C1/32;B64G1/10;

  • 国家 FR

  • 入库时间 2022-08-22 08:45:32

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