Concurrent rocket engine pre-conditioning and tank filling is disclosed. A disclosed example apparatus includes an inlet valve to supply a rocket propellant tank that is associated with a rocket engine with rocket propellant, and a flow director to direct at least a portion of a flow of the rocket propellant from the inlet valve to a chill line of the rocket engine to thermally condition the rocket engine as the rocket propellant tank is being filled with the rocket propellant.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CONCURRENT ROCKET ENGINE PRE-CONDITIONING AND TANK LOADING


    Beteiligte:

    Erscheinungsdatum :

    2020-04-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    Concurrent rocket engine pre-conditioning and tank loading

    SWENSON KEVIN / RODRIGUEZ JR HENRY / VANIMAN BRIAN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    ROCKET PROPELLANT TANK ARRANGEMENT, ROCKET PROPULSION UNIT, AND ROCKET

    BAEKBY BJARNOE JONAS / VON BENGTSON KRISTIAN | Europäisches Patentamt | 2019

    Freier Zugriff

    Rocket propellant tank arrangement, rocket propulsion unit, and rocket

    BAEKBY BJARNOE JONAS / VON BENGTSON KRISTIAN | Europäisches Patentamt | 2024

    Freier Zugriff

    ROCKET ENGINE, ROCKET, AND METHOD FOR STARTING ROCKET ENGINE

    KAWAMATA YOSHIHIRO / OBASE KIMIHITO | Europäisches Patentamt | 2016

    Freier Zugriff

    ROCKET ENGINE, ROCKET, AND METHOD FOR STARTING ROCKET ENGINE

    KAWAMATA YOSHIHIRO / OBASE KIMIHITO | Europäisches Patentamt | 2015

    Freier Zugriff