The Italian Research Interim Stage (IRIS) is described. It consists of a Shuttle upper stage system designed to inject light payloads up to 900 kg mass from the Shuttle circular parking orbit into a geostationary transfer orbit. A summary of the information included in the IRIS user's manual provides users with the necessary performance data, environment and interfaces for their payloads. A review of the status of the project is presented. The first flight unit will be launched in Aug. 1991.


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    Titel :

    IRIS System and Future Application to Expandable Launchers


    Beteiligte:
    L. Bussolino (Autor:in) / F. Varesio (Autor:in) / G. Rum (Autor:in) / C. Portelli (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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