Low thrust trajectory analyses were used to examine the feasibility of using solar electronic propulsion for Earth escape from a negative C3 launch for deep space missions in order to significantly increase the net delivered mass capability of inexpensive launch vehicles.


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    Titel :

    Negative C3 Launch Options for Solar System Exploration


    Beteiligte:
    Leifer, S. (Autor:in) / Noca, M. (Autor:in)

    Kongress:

    Joint Propulsion Conference


    Erscheinungsdatum :

    1998-07-13


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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