Entry into orbit of planet may be assisted by entry into suitable satellite orbit around planet; circular satellite orbits for minimum energy are determined for planets of Solar System, assuming transfer along minimum energy semi-ellipse from Earth; effect is of practical interest for flights to Mercury and Mars.


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    Titel :

    Minimum energy entry into planetary satellite orbits


    Weitere Titelangaben:

    Brit Interplanetary Soc -- J


    Beteiligte:


    Erscheinungsdatum :

    1961


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Entry into circular planetary satellite orbits

    Greenwood, S.W. | Engineering Index Backfile | 1962


    Entry into circular orbits

    Lawden, D.F. | Engineering Index Backfile | 1951


    Entry into circular orbits -- 2

    Lawden, D.F. | Engineering Index Backfile | 1954


    Planetary Orbits

    Biesbroek, Robin | Springer Verlag | 2015