An engine start system includes a facility that has a ground based hydraulic pressurization system and a combustor of a liquid propellant rocket engine. The engine is fluidly coupled to the ground based hydraulic pressurization system. The liquid propellant rocket engine is operably detachable from the ground based hydraulic pressurization system.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    GROUND HYDRAULIC SYSTEM HYPERGOLIC SLUG INJECTION


    Beteiligte:
    PARKER DOUGLAS (Autor:in) / DODD FREDERICK (Autor:in)

    Erscheinungsdatum :

    2019-10-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    GROUND HYDRAULIC SYSTEM HYPERGOLIC SLUG INJECTION

    PARKER DOUGLAS / DODD FREDERICK | Europäisches Patentamt | 2018

    Freier Zugriff

    GROUND HYDRAULIC SYSTEM HYPERGOLIC SLUG INJECTION

    PARKER DOUGLAS / DODD FREDERICK | Europäisches Patentamt | 2020

    Freier Zugriff

    Ground hydraulic system hypergolic slug injection

    PARKER DOUGLAS / DODD FREDERICK | Europäisches Patentamt | 2021

    Freier Zugriff

    Ignition of hypergolic propellants

    Dambach, Erik Michael | TIBKAT | 2010


    Hypergolic Propellant Ignition Phenomenon Associated with Two-Phase Oxidizer Flow Injection

    Matsuura, Yoshiki / Iihara, Shigeyasu / Tashiro, Yosuke | AIAA | 2014