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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    Title :

    Launch Window for the X4 Satellite on a Scout Rocket


    Contributors:
    G. E. Cook (author)

    Publication date :

    1972


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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