The invention relates to a ram Laval nozzle effect propulsion and oxygen production rocket, in particular to a working method of the ram Laval nozzle effect propulsion and oxygen production rocket and belongs to the technical field of aerospace aviation. The working method is used for an aerospace plane engine and an aerospace flying vehicle engine. According to the working principle of the Laval nozzle effect rocket, a Laval nozzle is used by an American engineer to establish positive pressure at one end and negative pressure at the other end, and table tennis balls are made to crush table tennis bats at a supersonic speed (please see substantive examination reference data). The technology is used in a rocket propulsion and oxygen production system, so that the flying speed of the rocket is higher, and oxygen production efficiency in the flying process of the rocket is made higher. The rocket can take off at a zero speed, the functions of ramming and air suction are achieved, and the rocket can return to the ground again after aerospace work is completed. The rocket can be used repeatedly.


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    Titel :

    Working method of ram Laval nozzle effect propulsion and oxygen production rocket


    Beteiligte:
    DU SHANJI (Autor:in)

    Erscheinungsdatum :

    09.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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    Falkovich, S. V. | TIBKAT | 1949