This paper will focus on trajectory transfers from trans-lunar injection (TLI) to lunar frozen orbits with applications to NASA’s Commercial Lunar Payload Services (CLPS) and Artemis Human Landing System (HLS) programs. For a CLPS application, the CS-3 mission is explored, which will deploy a communications relay satellite in lunar elliptical frozen orbit followed by landing a payload on the lunar farside during dawn. Given HLS will land a crew near the lunar south pole with lighting and timing requirements, the effect of varying the Earth-Moon transit duration to influence the approach direction upon landing will be explored.


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    Titel :

    Transfers from TLI to Lunar Frozen Orbits with Applications to NASA’s CLPS & Artemis Programs


    Beteiligte:
    A. L. Genova (Autor:in) / D. Morrison-Fogel (Autor:in) / P. Levinson-Muth (Autor:in)

    Erscheinungsdatum :

    2023


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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