Fundamentals of electric propulsion; description and characteristics of three types of thrust devices -- electrostatic accelerators, electromagnetic accelerators, and thermal arc jets; possible missions listed which could be applicable for electric propulsion; power requirements presented in parametric form for specific missions of low-altitude sustainer and orbit transfers; off-optimum operations are considered in case of 200 to 22,300 mi orbit transfer.


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    Title :

    Electric propulsion and power requirements for space vehicles


    Additional title:

    SAE -- Paper


    Contributors:
    Stull, F.D. (author) / Shiel, V.W. (author)

    Conference:

    SAE Meeting ; 1960 Electric propulsion



    Publication date :

    1960


    Size :

    14 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    ELECTRIC PROPULSION AND POWER REQUIREMENTS FOR SPACE VEHICLES

    STULL, FRANK D. / SHIEL, VINCENT W. | SAE Technical Papers | 1960


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