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:

    Kongress:

    34th AIAA/AAS Space Flight Mechanics Meeting ; 2024 ; Orlando, FL, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Transfers from TLI to Lunar Frozen Orbits with Applications to NASA's CLPS & ARTEMIS Programs

    Genova, Anthony L. / Morrison-Fogel, Dylan / Levinson-Muth, Paul | AIAA | 2024


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

    A. L. Genova / D. Morrison-Fogel / P. Levinson-Muth | NTIS | 2023




    NASA’s Artemis Human Landing Systems: Enabling Lunar Exploration

    Lisa Watson-Morgan / Thomas Percy / Jason Turpin et al. | NTRS