The invention relates to the field of rocket launching, in particular to a low-impact explosive bolt unlocking satellite-rocket separation device which comprises a satellite interface platform, a satellite distributor interface platform, an explosive bolt capturing cabin cover, a locking nut, a stop spring, an explosive bolt, a separation spring and a travel switch. According to the satellite-rocket separation device for unlocking the low-impact explosive bolt, the impact environment when an initiating explosive device explodes can be improved, and the separated spacecraft is prevented from being affected.

    本申请涉及火箭发射领域,尤其涉及一种低冲爆炸螺栓解锁的星箭分离装置,包括:卫星接口平台、星分配器接口平台、爆炸螺栓捕获舱盖、锁紧螺母、止动弹簧、爆炸螺栓、分离弹簧和行程开关。本申请所提供的低冲爆炸螺栓解锁的星箭分离装置,可以改善火工品爆炸时的冲击环境,避免了影响分离后的航天器。


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    Titel :

    Satellite-rocket separation device for unlocking low-impact explosive bolt


    Weitere Titelangaben:

    一种低冲爆炸螺栓解锁的星箭分离装置


    Beteiligte:
    ZHANG DONGBO (Autor:in) / YANG HAOLIANG (Autor:in) / SUN LIANGJIE (Autor:in) / MING AIZHEN (Autor:in) / SUN ZHICHAO (Autor:in)

    Erscheinungsdatum :

    2022-05-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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