NEC is developing a multi-mission spacecraft for the next generation. This spacecraft is applicable to various LEO (Low earth Orbit) missions (i.e. earth observation, scientific observation and communication) and GEO (Geostationary Orbit) missions. The design concepts are wide adaptability for missions and orbits, compact size for maximizing the mission ratio and easy modification for short-time delivery and low-cost. Now, the core avionics for this spacecraft (compact electronics, high-performance flight computer and integrated flight software) is being developed by NEC. This paper introduces the system configuration, performances and newly applied technologies that are required from study of multi-mission adaptability.


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    Title :

    NEC multi-mission spacecraft concepts and technologies


    Additional title:

    Multi-Missions-Raumfahrzeug-Konzepte und -Technologien von NEC


    Contributors:
    Adachi, M. (author) / Kawaguchi, M. (author)

    Published in:

    Publication date :

    2001


    Size :

    6 Seiten, 4 Bilder, 1 Tabelle, 1 Quelle



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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