Abstract This paper examines various design parameters for missions that ascend from the lunar far-side surface and insert into a halo orbit about the Earth–Moon L2 point. These parameters include fuel costs, ascent sites of interest such as the South Pole Aiken Basin and Tsiolkovsky Crater, different sized halo orbits, and transfer durations. Halo orbit stable manifolds are studied in the simplified Circular Restricted Three-Body Problem, and transfers are targeted and optimized in high-fidelity simulations. The design parameters studied in this paper can aid in development of mission architectures in the Earth–Moon system as well as other systems with a secondary mass without an atmosphere.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Ascent trajectories from the lunar far-side to Earth–Moon L2 halo orbits


    Beteiligte:
    Dietrich, Ann (Autor:in) / Davis, Kathryn (Autor:in) / Parker, Jeffrey (Autor:in)

    Erschienen in:

    Advances in Space Research ; 56 , 11 ; 2595-2611


    Erscheinungsdatum :

    2015-09-21


    Format / Umfang :

    17 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Transfer Trajectories from the Moon to Sun–Earth Halo Orbits

    Nakamiya, Masaki / Kawakatsu, Yasuhiro | AIAA | 2014



    Design of Earth Moon Halo Orbits for a Global Lunar PNT Service

    Musacchio, Daniele / Iess, Luciano / Carosi, Mattia et al. | British Library Conference Proceedings | 2021