Miniaturization technologies such as Micro-Electro-Mechanical Systems (MEMS) have been used to fabricate a prototype 100-gm class cold gas propulsion system suitable for use on a Co-Orbiting Satellite Assistant (COSA). The propulsion system is fabricated from bonded layers of photostructurable glass (Foturan glass; the design is based on fabricating integrated modular parts. Thus, the propulsion system is mass producible, expandable, expendable (low unit cost), and highly integrated.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Microengineered cold gas thruster system for a co-orbiting satellite assistant (COSA)


    Beteiligte:

    Kongress:

    MEMS Components and Applications for Industry, Automobiles, Aerospace, and Communication ; 2001 ; San Francisco,CA,United States


    Erschienen in:

    Erscheinungsdatum :

    01.10.2001





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Lunar orbiting satellite system, and ground station of lunar orbiting satellite system

    IMAMURA NAOKI / YOSHIKAWA SHOJI / MITSUDA KENRO et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    SATELLITE DE-ORBITING SYSTEM

    BOYCE BRIAN P | Europäisches Patentamt | 2024

    Freier Zugriff

    LUNAR ORBITING SATELLITE SYSTEM, AND GROUND STATION OF LUNAR ORBITING SATELLITE SYSTEM

    IMAMURA NAOKI / YOSHIKAWA SHOJI / MITSUDA KENRO et al. | Europäisches Patentamt | 2021

    Freier Zugriff