The invention provides a reusable horizontal take-off and landing two-stage aerospace vehicle. A first-stage structure is a reusable winged sub-orbital aircraft, and the whole aircraft is of an aerospace aircraft structure; and the second-stage structure is a traditional rocket structure. Wherein the first stage can realize horizontal rising and landing, and the second stage adopts a recovery scheme of maritime splashing recovery. The aircraft can be recycled and reused while efficient carrying is ensured.

    本发明提供一种可重复使用的水平起降二级空天运载器,一级结构为可重复使用的带翼亚轨道飞行器,整体为空天飞机构型;二级结构为传统火箭构型。其中一级可实现水平起降,二级采用了海上溅落回收的回收方案。本发明在确保高效运载的同时实现飞行器回收和可重复使用。


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    Titel :

    Reusable horizontal take-off and landing two-stage aerospace vehicle


    Weitere Titelangaben:

    一种可重复使用的水平起降二级空天运载器


    Beteiligte:
    SHI PENG (Autor:in) / WANG ZHUXUAN (Autor:in) / LI QILING (Autor:in) / GAO LU (Autor:in) / XU XIAODONG (Autor:in) / LYU PENGFEI (Autor:in) / LI ZEKUN (Autor:in) / TONG ZHENYU (Autor:in)

    Erscheinungsdatum :

    12.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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