首页> 外国专利> Multilayered hypervelocity impact shield for spacecraft

Multilayered hypervelocity impact shield for spacecraft

机译:航天器的多层超高速冲击防护罩

摘要

A hypervelocity impact shield assembly (10) for protecting a spacecraft surface (12) from hypervelocity impactors. The shield assembly (10) includes at least one sacrificial impactor disrupting/shocking layer (16) of hypervelocity impactor disrupting/shocking material. A primary spacing element (18), including space-rated open cell foam material, is positioned between the at least one sacrificial impactor disrupting/shocking layer (16) and a spacecraft surface (12). a cover member (20) is arranged and disposed relative to the sacrificial impactor disrupting/shocking layer (16) and the primary spacing element (18) to maintain the integrity of the hypervelocity impact shield assembly (10). In the event of exposure to a hypervelocity impactor, the sacrificial impactor disrupting/shocking layer (16) is perforated while shocking the impactor breaking it into fragments, and/or melting it, and/or vaporizing it, thus providing a dispersion in the form of an expanding debris cloud/plume which spreads the impact energy of the impactor over a volume formed by the primary spacing element (18) between the sacrificial impactor disrupting /shocking layer (16) and the spacecraft surface. This significantly reduces impact lethality ar the spacecraft surface (12). The space-rated open cell foam material provides an extremely lightweight, low-cost, efficient means of spacing and supporting the at least one sacrificial impactor disrupting/shocking layer (16) before, during, and after launch. In a preffered embodiment, the invention is in the form of a multi-shock assembly including a plurality of sacrificial impactor disrupting/shocking layers. In such instance, the hypervelocity impact shield assembly (10) includes a plurality of secondary spacing elements. Each secondary spacing element is positioned adjacent an associated sacrificial impactor disrupting/shocking layer (16) to form a multi-shock subassembly. Thus, a plurality of multi-shock subassemblies are provided which include alternating layers of sacrificial impactor disrupting/shocking layers (16) and secondary spacing elements (30,32,34).
机译:超高速冲击防护罩组件(10),用于保护航天器表面(12)免受超高速冲击器的撞击。防护罩组件(10)包括超速冲击器破坏/冲击材料的至少一个牺牲冲击器破坏/冲击层(16)。包括间隔开孔泡沫材料的主要间隔元件(18)位于至少一个牺牲冲击器破坏/冲击层(16)和航天器表面(12)之间。相对于牺牲冲击器破坏/冲击层(16)和主要间隔元件(18)布置和布置了盖构件(20),以保持超高速冲击屏蔽组件(10)的完整性。在暴露于超高速冲击器的情况下,牺牲冲击器破坏/冲击层(16)被穿孔,同时冲击冲击器,使其破碎成碎片,和/或使其熔化,和/或蒸发,从而提供以下形式的分散体:膨胀的碎屑云/团块,其将冲击器的冲击能量散布在牺牲冲击器破坏/冲击层(16)和航天器表面之间的主要间隔元件(18)形成的体积上。这显着降低了航天器表面(12)的冲击杀伤力。具有空间等级的开孔泡沫材料在发射之前,之中和之后提供了一种非常轻便,低成本,有效的间隔和支撑至少一个牺牲冲击器破坏/冲击层(16)的方式。在优选的实施例中,本发明为包括多个牺牲冲击器破坏/冲击层的多冲击组件的形式。在这种情况下,超高速冲击防护罩组件(10)包括多个第二间隔元件。每个次级间隔元件被定位成与相关的牺牲冲击器破坏/冲击层(16)相邻,以形成多冲击子组件。因此,提供了多个多冲击子组件,其包括牺牲冲击器破坏/冲击层(16)和辅助间隔元件(30、32、34)的交替层。

著录项

  • 公开/公告号EP1293429A1

    专利类型

  • 公开/公告日2003-03-19

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20010203545

  • 发明设计人 DVORAK BRUCE;

    申请日2001-09-18

  • 分类号B64G1/56;F41H5/04;

  • 国家 EP

  • 入库时间 2022-08-21 23:50:17

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号