The invention belongs to the technical field of manned space-ground back-and-forth transportation, and discloses a reusable escape system of a manned spacecraft based on a parachute, the parachute can adopt a ring sail parachute only having a deceleration landing capability or a parafoil having a fixed-point accurate return landing capability, and the escape system comprises a modularly designed escape cabin, the escape cabin is arranged between the modular carrier rocket and the modular manned module, and the escape cabin and the manned module are combined to form an escape system; a folded parachute pack is arranged in the escape cabin, and the parachute pack is in control connection with control equipment arranged in the escape cabin; the escape system comprises a normal launching working mode and an escape working mode which are suitable for different conditions. The unmanned aerial vehicle escape system is arranged between a carrier rocket and a manned spacecraft, the escape system is recycled through the deceleration landing capacity of the parachute, and the launching operation cost of manned space-ground back-and-forth transportation is greatly reduced; and meanwhile, the life safety of astronauts can be guaranteed when dangers occur.

    本发明属于载人天地往返运输技术领域,公开了一种基于降落伞的载人飞船可重复使用逃逸系统,降落伞可采用仅具备减速降落能力的环帆伞或是具备定点精确返回着陆能力的翼伞,逃逸系统包括模块化设计的逃逸舱,逃逸舱设置在模块化的运载火箭和模块化的载人模块之间,逃逸舱与载人模块组合形成逃逸系统;逃逸舱内设置有折叠的伞包,伞包与设置在逃逸舱内的控制设备控制连接;逃逸系统包括正常发射工作模式和逃逸工作模式两种适于不同的状况。本发明设置在运载火箭和载人飞船中间,利用降落伞的减速降落能力将逃逸系统进行回收利用,极大降低载人天地往返运输的发射运营成本;同时还能在出现危险时保障航天员生命安全。


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    Titel :

    Reusable escape system of manned spacecraft based on parachute


    Weitere Titelangaben:

    一种基于降落伞的载人飞船可重复使用逃逸系统


    Beteiligte:
    LEI SHIQING (Autor:in) / ZHANG MINJIE (Autor:in) / WANG JUN (Autor:in)

    Erscheinungsdatum :

    10.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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