The invention relates to an aerostat-carried planet sampling return cabin recovery test method, which comprises the following steps: S100, in an issuing stage, an aerostat-carried planet sampling return cabin recovery test system is assembled and debugged, and the test system is issued when a wind field meets an issuing requirement; S200, in an ascending stage, by combining high-altitude wind field data and controlling the lift-off speed of the test system, the test system can reach a design area when reaching a design height; S300, in a level flight stage, a planet sampling return cabin is put in and recycled; S400, in a descending stage, a nacelle of an aerostat platform is put in and recycled; and S500, flight data of the aerostat platform and the planet sampling return cabin are analyzed, and the recovery performance of the planet sampling return cabin is verified.

    本发明涉及一种浮空器搭载行星采样返回舱回收试验方法,包括以下步骤:步骤S100,发放阶段,将浮空器搭载行星采样返回舱回收试验系统装配调试,风场满足发放要求时,发放试验系统;步骤S200,上升阶段中,结合高空风场数据,通过控制试验系统的升空速度,使试验系统到达设计高度时,能够抵达设计区域;步骤S300,平飞阶段,投放和回收行星采样返回舱;步骤S400,下降阶段,投放和回收浮空器平台的吊舱;步骤S500,分析浮空器平台和行星采样返回舱飞行数据,验证行星采样返回舱的回收性能。


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    Titel :

    Aerostat-carried planet sampling return cabin recovery test system


    Weitere Titelangaben:

    一种浮空器搭载行星采样返回舱回收试验系统


    Beteiligte:
    LIU QIANG (Autor:in) / YANG YANCHU (Autor:in) / WANG ZIHAO (Autor:in) / HAO YONG (Autor:in)

    Erscheinungsdatum :

    2020-05-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



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