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Spacecraft attack and distress ejectable recorder

机译:宇宙飞船遇险遇险记录仪

摘要

A space vehicle including an attachment system for attaching the vehicle to another space vehicle, a memory for storing data concerning at least one of the status of the other space vehicle and threats experienced by the other space vehicle, and a transmission system for transmitting data stored in the memory to at least one of a planet or a different space vehicle. An ejection system causes the secondary vehicle to be ejected from the primary vehicle when predetermined criteria concerning the status data or the said threat data are met. A spin system causes the secondary vehicle to be spin stabilized when ejected from the primary vehicle. The vehicle serves as, at least, one of a plurality of secondary vehicles, attached to the other (primary) vehicle. In accordance with the method of the invention, when the secondary vehicle is ejected the nature of the threat or status of the primary vehicle can be determined.
机译:一种太空飞行器,包括:用于将其附着到另一太空飞行器的附接系统;用于存储与另一太空飞行器的状态和另一太空飞行器所经历的威胁中的至少一个有关的数据的存储器;以及用于传输所存储的数据的传输系统存储器中的至少一个存储在行星或其他航天器中。当满足关于状态数据或所述威胁数据的预定标准时,弹出系统使次要车辆从主车辆中弹出。当从主车辆弹出时,自旋系统使次车辆稳定旋转。该车辆用作附接到另一(主要)车辆的多个第二车辆中的至少一个。根据本发明的方法,当次要车辆被弹出时,可以确定主要车辆的威胁或状态的性质。

著录项

  • 公开/公告号US2002084385A1

    专利类型

  • 公开/公告日2002-07-04

    原文格式PDF

  • 申请/专利权人 BOZ WALLACE S.;LEUNG YAT FAI;

    申请/专利号US20000752175

  • 发明设计人 WALLACE S. BOZ;YAT FAI LEUNG;

    申请日2000-12-29

  • 分类号B64G1/52;

  • 国家 US

  • 入库时间 2022-08-22 00:50:15

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