A system for fluid management in low or micro gravity environment, the system including: a two-phase gas-liquid tank suitable for storage of a two-phase gas-liquid, the two-phase gas-liquid tank including an outer surface, an inner cavity, and an outlet between the inner cavity and the outer surface. The system further includes a thermal or electromagnetic device disposed on or proximal to the two-phase gas-liquid tank. The system further includes a controller operatively coupled to the thermal or electromagnetic device, the controller being configured to energize the thermal or electromagnetic device in a controlled manner (i) to generate a thermal or electromagnetic gradient heat in the two-phase gas-liquid and (ii) urge a portion of the two-phase gas-liquid to the outlet of the two-phase gas-liquid tank.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    THERMOELECTROMAGNETIC SPACECRAFT PROPELLANT POSITIONING


    Beteiligte:

    Erscheinungsdatum :

    2024-08-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F17C Behälter zum Aufnehmen oder Speichern verdichteter, verflüssigter oder verfestigter Gase , VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES



    Thermoelectromagnetic SmallSat propellant positioning

    Hart, Samuel T. / Lightsey, E. Glenn / Romero-Calvo, Álvaro | Elsevier | 2023



    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

    Spacecraft propellant management system

    WU GORDON / TORRES MARIA EUGENIA / MELANI DIEGO A et al. | Europäisches Patentamt | 2021

    Freier Zugriff