A thermal management system (5) for a magnetoplasmadynamic thruster (10) for a space craft is disclosed. The thermal management system (5) is located between at least one superconducting magnet (120) and a plasma discharge unit (15 and comprises a thermal barrier (40, 60) located adjacent to the plasma discharge unit (15), —a multilayer insulation (70) located between the thermal barrier (40, 60) and the cryostat insulation (80), and a radiation gap (50) located in the thermal barrier (40, 60).


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    Titel :

    Thermal Management System for Spacecraft Thruster


    Beteiligte:

    Erscheinungsdatum :

    2024-07-18


    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 / H01F MAGNETS , Magnete / H05H Plasmatechnik , PLASMA TECHNIQUE



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