Systems, methods, and apparatus for a structural propellant for ion rockets (SPIR) are disclosed. In one or more embodiments, a method for in-space propulsion of a spacecraft involves removing, by a removal device, a portion of a structure of the spacecraft. The method further involves feeding, by the removal device, the portion into a Hall thruster system. Further, the method involves utilizing, by the Hall thruster system, the portion as propellant to produce thrust. In one or more embodiments, the structure is an upper stage of the spacecraft. In at least one embodiment, the upper stage comprises at least one structural support and/or at least one upper stage housing. In some embodiments, the structure is manufactured from magnesium, bismuth, zinc, and/or indium.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Structural Propellant for ion rockets (SPIR)


    Beteiligte:

    Erscheinungsdatum :

    2019-10-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Structural Propellant for Ion Rockets (SPIR)

    CHILDRESS JAMIE J / KESSLER THOMAS L | Europäisches Patentamt | 2017

    Freier Zugriff

    STRUCTURAL PROPELLANT FOR ION ROCKETS (SPIR)

    CHILDRESS JAMIE J / KESSLER THOMAS L | Europäisches Patentamt | 2020

    Freier Zugriff

    Solid Propellant Rockets

    J. De Montravel | NTIS | 1967


    Solid-propellant rockets.

    Lambert, C. H., Jr. | NTRS | 1964


    Solid propellant rockets

    Zaehringer, A.J. | Engineering Index Backfile | 1955