Requirements imposed on logistics system that is launched into low earth orbit are established and importance of orbit selection is considered, taking phasing and cross-range penalties into account as well as availability of launch opportunities for logistics mission; it is concluded that low inclinations should be near 29.6° except for one very specialized case; logistics vehicle is described that is compatible with Titan III and meets requirements of flexibility.


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    Title :

    Integrated orbital logistics support


    Additional title:

    J Spacecraft Rockets


    Contributors:
    Lea, R.H. (author)

    Published in:

    Publication date :

    1967


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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