A spacecraft propulsion system comprises an attitude adjustment thruster system with multiple thrusters (488a-d) receiving heated propellant via a shared thermal capacitance block (275). The thermal capacitance block (275) with integrated fluidic channels receives energy from a solar concentrator (320) and stores the heat.


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    Titel :

    Thermal Capacitor Block with Integrated Fluidic Channels


    Beteiligte:

    Erscheinungsdatum :

    25.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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