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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    Title :

    Common lunar lander


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

    Publication date :

    1992-03-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Common lunar lander

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    Artemis: Common lunar lander project status

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