In various embodiments, an electrothermal propulsion system for imparting velocity to a spacecraft features a joint-free monolithic integrated thruster component including an inlet section, a resistively heated heat-exchanger section, and a nozzle section.


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    Title :

    High-temperature electrothermal propulsion system


    Contributors:

    Publication date :

    2021-08-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B33Y ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING , Additive (generative) Fertigung, d. h. die Herstellung von dreidimensionalen [3D] Bauteilen durch additive Abscheidung, additive Agglomeration oder additive Schichtung, z. B. durch 3D- Drucken, Stereolithografie oder selektives Lasersintern



    Electrothermal propulsion

    Martinek, F. | Engineering Index Backfile | 1960


    ELECTROTHERMAL PROPULSION TESTING TECHNIQUES

    DUCATI, ADRIANO / MUEHLBERGER, ERICH / TODD, JAMES | AIAA | 1964


    Electrothermal propulsion testing techniques

    Ducati, A.C. / Muehlberger, E. / Todd, J.P. | Engineering Index Backfile | 1964



    MICROWAVE ELECTROTHERMAL THRUSTER ADAPTED FOR IN-SPACE ELECTROTHERMAL PROPULSION

    GANAPATHY ROHAN M / NOWAL VINOD | European Patent Office | 2018

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