A spacecraft includes a propulsion system including an inert gas stored in a set of pressurant tanks, one or more electric thrusters operable with the inert gas, one or more cold gas thrusters operable with the inert gas; and a pneumatic arrangement including commandable valves.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Spacecraft propellant management system


    Beteiligte:
    WU GORDON (Autor:in) / TORRES MARIA EUGENIA (Autor:in) / MELANI DIEGO A (Autor:in) / BALDWIN JEFF AARON (Autor:in) / MARLOW DAVID (Autor:in)

    Erscheinungsdatum :

    2021-10-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    SPACECRAFT PROPELLANT LOADING SYSTEM

    MURPHY ASHTON / LENGUITO GIOVANNI | Europäisches Patentamt | 2023

    Freier Zugriff

    Propellant tank for spacecraft and spacecraft

    ISHIKAWA KEITARO / AOYAMA TAICHI / KINEFUCHI KIYOSHI et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    PROPELLANT TANK FOR SPACECRAFT AND SPACECRAFT

    ISHIKAWA KEITARO / AOYAMA TAICHI / KINEFUCHI KIYOSHI et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Gemini spacecraft propellant loading system

    GEHRING, W. / MANTZ, H. | AIAA | 1965


    PROPELLANT TANK FOR SPACECRAFT, AND SPACECRAFT

    ISHIKAWA KEITARO / AOYAMA TAICHI / KINEFUCHI KIYOSHI et al. | Europäisches Patentamt | 2019

    Freier Zugriff