On the basis of the preliminary Scout trajectory plan, a launch window is defined for the revised X4 mission, which uses an Algol III Scout to inject the satellite into a nominally circular orbit at a height of 750 km. The effects of launch vehicle injection errors are taken into account using a stochastic simulation method.


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    Titel :

    Launch Window for the X4 Satellite on a Scout Rocket


    Beteiligte:
    G. E. Cook (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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