The invention discloses a spacecraft launching method and a launching platform formed on the basis of the basic principle of the method. The spacecraft launching method is technically characterized inthat the launching speed is low, the low-speed flight height is high, and the spacecraft launching method is called a low-speed high-throwing type launching method for short. A low-speed high-throwing type launching platform developed on the basis of the invention mainly comprises auxiliary system equipment and materials such as a platform body, a power system, an attitude adjustment system, an instrument measurement and control system, buffer column feet and the like, and the flight mode of the low-speed high-throwing type launching platform has the technical characteristic of low-speed high-throwing type.

    本发明公开了一种航天器的发射方法以及基于这种方法的基本原理形成的发射平台,本发明的一种航天器的发射方法,其技术特征是:发射速度低,慢速飞行高度高,简称为慢速高抛式发射方法。基于本发明开发的慢速高抛式发射平台,主要包括平台本体,动力系统,姿态调整系统,仪表测控系统,缓冲柱脚等辅助系统设备及材料,其飞行方式具有慢速高抛式的技术特征。


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    Titel :

    Spacecraft low-speed high-throwing type launching method and launching platform


    Weitere Titelangaben:

    一种航天器慢速高抛式发射方法及发射平台


    Beteiligte:
    YAO HONGWEI (Autor:in)

    Erscheinungsdatum :

    2020-04-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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