Marshall Space Flight Center is developing a small lunar lander capable of delivering up to 300 kg of payload to the lunar surface near the North or South Pole. Originally designed as a lander for a small rover, the Lunar Pallet Lander, has seen several design iterations over the last couple of years. This paper will cover how the vehicle and mission design changed from being a co-manifested payload candidate in NASA’s Space Launch System to its current design, which could be launched with an Evolved Expendable Launch Vehicle (EELV), and reach a wide range of polar landing sites.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Mission Design for the Lunar Pallet Lander


    Beteiligte:
    Craig, A. S. (Autor:in) / Holt, J. P. (Autor:in) / Hannan, M. R. (Autor:in) / Orphee, J. I. (Autor:in)

    Kongress:

    AAS/AIAA Space Flight Mechanics Meeting ; 2019 ; Ka''anapali, HI, United States


    Erscheinungsdatum :

    13.01.2019


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Mission Design for the Lunar Pallet Lander

    A. S. Craig / J. P. Holt / M. R. Hannan et al. | NTIS | 2019


    Guidance and Navigation Design Trades for the Lunar Pallet Lander

    Anzaline, Evan / Braden, Ellen / Ahmad, Naeem et al. | NTRS | 2019


    Guidance and Navigation Design Trades for the Lunar Pallet Lander

    E. Anzalone / E. Braden / N. Ahmad et al. | NTIS | 2019


    Guidance and Navigation Design Trades for the Lunar Pallet Lander

    E. Anzaline / E. Braden / N. Ahmad et al. | NTIS | 2019


    Guidance and Navigation Design Trades for the Lunar Pallet Lander

    Anzalone, Evan / Braden, Ellen / Ahmad, Naeem et al. | NTRS | 2019