Mission 3B is designed as a payload retrieval mission with both shuttle launch and orbiter landing to take place at the western test range. The mission is designed for direct rendezvous with a passive satellite in a 100 NMI circular orbit with an inclination of 104 degrees. The ascent portion of mission 3B is described as well as the trajectory simulation. (Author)


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    Titel :

    Reference Mission 3B Ascent Trajectory. Mission Planning, Mission Analysis and Software Formulation


    Beteiligte:
    A. E. Kuhn (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    49 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch