A microscale thruster, has been successsfully designed using MEMS technology, in that 'stacked wafer' design is adopted.The thruster is built up of stacked and bonded silicon wafer, each with its own internal structure. The MEMS technology as succeed in acheiveing good performance and relatively short heat-up transient. This paper describes the preliminary design and detailed thermal analysis. The microthruster is designed to be used on small satellites,to deliver small impulse bits micro/nano-satellites for delta V impulses.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Thermal design of an HTP microthruster


    Beteiligte:
    Halswijk, W.H.C. (Autor:in) / Moerel, J.L.P.A. (Autor:in) / Sanders, H.M. (Autor:in)


    Erscheinungsdatum :

    2005


    Format / Umfang :

    2 Seiten




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    MICROTHRUSTER ARRAY

    RODRIGUEZ CARLOS | Europäisches Patentamt | 2025

    Freier Zugriff

    Chemical Microthruster Options

    W. DeGroot / S. Oleson | NTIS | 1996


    Microthruster Propulsion

    Shiroma, Wayne A. / Thakker, Purvesh | AIAA | 2010


    Chemical Microthruster Options

    De Groot, W. A. / Oleson, S. R. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996


    Cesium microthruster system

    COLLETT, C. / DULGEROFF, C. | AIAA | 1969