Thermally fragmentable fastening device

    公开(公告)号:US10378575B2

    公开(公告)日:2019-08-13

    申请号:US15473289

    申请日:2017-03-29

    申请人: Airbus DS GmbH

    IPC分类号: F16B31/00 B64G1/62 B64G1/64

    摘要: A fastening device for use in a spacecraft comprises a shaft and a head, which is connected by a first solder to the shaft. The first solder comprises a material of which the melting point is lower than the temperature acting on the fastening device on re-entry of a spacecraft equipped with fastening device into the earth's atmosphere.