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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    Title :

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


    Contributors:
    A. E. Kuhn (author)

    Publication date :

    1975


    Size :

    49 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English