This report focuses on the reference lander design developed at the Johnson Space Center, describing a small lunar soft lander with the capability to soft land about 64 kilograms of payload at any lunar latitude and longitude. The Artemis lander is a sun-pointing, three-axis vehicle that contributes to the translunar injection burn and performs the lunar orbit insertion, deorbit, descent and landing maneuvers with a single liquid bipropellant lander stage. Attention is given to mission profile and performance, the guidance, navigation and control subsystem, the propulsion subsystem, and the flight data subsystem.


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    Titel :

    Common lunar lander


    Beteiligte:
    Bailey, S. (Autor:in) / Stecklein, J. (Autor:in) / Chen, H. (Autor:in) / Culpepper, W. (Autor:in) / Hyatt, C. D. (Autor:in) / Kluksdahl, E. (Autor:in) / Pelischek, T. (Autor:in) / Pruett, D. (Autor:in) / Rickman, S. (Autor:in) / Wagner, L. (Autor:in)

    Erscheinungsdatum :

    1992-03-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Common lunar lander

    BAILEY, S. / STECKLEIN, J. / CHEN, H. et al. | AIAA | 1992




    Common Lunar Lander (CLL) trajectory analysis

    Wagner, Lynn A., Jr. / Wilks, Nancy A. | NTRS | 1991


    Artemis: Common lunar lander project status

    Bailey, Stephen | NTRS | 1992