A satellite propulsion system comprises: at least one tank containing a propulsion reagent, and at least one tank containing a pressurizing gas that pressurizes the propulsion reagent, at least one transport means for transporting the pressurizing gas from the pressurizing gas tank to the propulsion reagent tank, the transport means comprising at least one opening allowing a continuous leak-off of pressurizing gas, and at least one device intended, after the satellite has entered operational orbit, to isolate a zone comprising the opening from the rest of the propulsion system.


    Access

    Download


    Export, share and cite



    Title :

    SATELLITE PROPULSION DEVICE ALLOWING PASSIVE ELIMINATION OF PRESSURIZING GAS


    Contributors:

    Publication date :

    2016-01-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Satellite propulsion device allowing passive elimination of pressurizing gas

    FONTAINE LAURENT | European Patent Office | 2018

    Free access

    Dynamics Simulation of Pressurizing in Propulsion System Configuration

    H. R. Ali Mohammadi / D. Ramesh / M. R. Heidary et al. | DOAJ | 2013

    Free access

    Variable water inlet pressurizing water jet propulsion system of superspeed boat

    FU HAOBO / ZHANG JIANLI / LIU YONGHUI et al. | European Patent Office | 2024

    Free access


    ELECTRODE BODY PRESSURIZING DEVICE

    MURABAYASHI MASANAO / TERADA KOJI | European Patent Office | 2016

    Free access