The invention discloses a multi-spacecraft separation test method, which comprises the following steps of: mounting spacecrafts on an adapter, and suspending the adapter at a position with a specified distance from the bottom surface through a suspension release mechanism; mounting the inertial measurement combination on a spacecraft and connecting the inertial measurement combination with inertial measurement equipment through a cable; the ignition control equipment is connected with the suspension release mechanism, the pneumatic separation mechanism on the spacecraft and the separation firer system on the adapter through cables; and carrying out a multi-spacecraft separation test according to the designed test process.

    本发明公开一种多航天器分离试验方法,包括:将航天器安装在适配器上,并通过悬吊释放机构将适配器悬吊在距离底面规定距离的位置;将惯性测量组合安装到航天器上通过电缆与惯性测量设备连接;将发火控制设备分别通过电缆与悬吊释放机构,航天器上的气动分离机构,适配器上的分离火工系统连接;根据设计的试验流程进行多航天器分离试验。


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    Titel :

    Multi-spacecraft separation test method


    Weitere Titelangaben:

    一种多航天器分离试验方法


    Beteiligte:
    LI ZHIJUN (Autor:in) / WU MIAO (Autor:in) / FAN BOJUN (Autor:in) / WANG YUSHU (Autor:in)

    Erscheinungsdatum :

    04.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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