发明名称 Spacecraft attack and distress ejectable recorder
摘要 A space vehicle includes an attachment system for attaching the vehicle to another space vehicle, a memory for storing data concerning 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 a planet or a different space vehicle. An ejection system enables the secondary vehicle to be ejected from the primary vehicle when predetermined criteria concerning the status data or the threat data are met. A spin system causes the secondary vehicle to be spin stabilized when ejected from the primary vehicle. When the secondary vehicle is ejected, the nature of the threat or status of the primary vehicle can be determined.
申请公布号 US6450454(B1) 申请公布日期 2002.09.17
申请号 US20000752175 申请日期 2000.12.29
申请人 SPACE SYSTEMS/LORAL, INC. 发明人 BOZ, II WALLACE S.;LEUNG YAT FAI
分类号 B64G1/52;B64G1/54;B64G1/56;B64G1/64;B64G1/66;(IPC1-7):B64G1/22 主分类号 B64G1/52
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