Mission applications have been studied that use solar electric propulsion (SEP) to inject payloads into geocentric orbits. Two specific applications feasible with current technology are described that approximate practical bounds for the next decade. In the lower extreme, SEP is used on a Thor-Delta launched satellite to maximize the weight injected into synchronous orbits. In the other extreme, SEP is used in a reusable interorbital tug together with an all-chemical shuttle/tug transportation system. Different trajectory profiles are required to most efficiently accomplish the overall mission objectives in the two cases.


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    Title :

    Geocentric solar electric propulsion vehicle design.


    Contributors:

    Conference:

    Joint Propulsion Specialist Conference ; 1972 ; New Orleans, LA, US


    Publication date :

    1972-11-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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