The disclosed propulsion system of a space vehicle and the methods of operating the propulsion system use a microwave energy source to heat propellant in a propellant chamber that pierces and traverses a waveguide carrying the microwave energy. In some implementations, the microwave energy ionizes and further heats the propellant in the propellant chamber. The partially ionized and heated propellant may exit the propellant chamber via a nozzle to generate thrust.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Pierced waveguide thruster


    Beteiligte:
    HUMMELT JASON (Autor:in) / PODOLSKY VLADLEN (Autor:in) / GASCON NICOLAS (Autor:in)

    Erscheinungsdatum :

    2023-02-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen




    Flow through a pierced membrane in a vacuum

    TILTON, D. / CHOW, L. | AIAA | 1986


    Fatigue Life of Self Pierced Rivets (SPR) in Car Body

    Blows, Andrew / Agrawal, Hari / Potty, Kesavan et al. | SAE Technical Papers | 2003


    Fatigue Life of Self Pierced Rivets (SPR) in Car Body

    Agrawal, H. / Li, W. / Bollimunta, S. et al. | British Library Conference Proceedings | 2003


    Static and Impact Behavior of Self-Pierced Rivet Connections in Aluminum

    Madasamy, C. / Faruque, O. / Tyan, T. et al. | British Library Conference Proceedings | 2001