Analysis of various transfer missions between parking orbits in cislunar space starting from initial 200 km parking orbit under optimum payload condition discloses interesting correlations between various systems of electric thrustors and missions performed; optimum payload can be calculated from basic formula for electric propulsion systems, which is given; calculated orbits can be correlated to different types of electric propulsion systems, with respect to exhaust velocity and total efficiency. In German with English and French abstracts.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Electric propulsion for cislunar missions


    Additional title:

    Elektrische Antriebe fuer cislunare Missionen


    Contributors:
    Au, G.F. (author)

    Published in:

    Publication date :

    1966


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    High Power Nuclear Electric Propulsion (NEP) for Cargo and Propellant Transfer Missions in Cislunar Space

    Falck, R. D. / Borowski, S. K. / Institute for Space and Nuclear Power Studies | British Library Conference Proceedings | 2003





    Neuro-adaptive Model Reference Tracking Controller for Cislunar Missions

    Thulaseedharan Pillay, Yrithu / Chace, Matthew / Steck, James et al. | AIAA | 2024