• DocumentCode
    3205696
  • Title

    Constellation lunar capability point of departure architecture

  • Author

    Muirhead, Brian K.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    This paper describes and discusses the Constellation point of departure lunar capability architecture. Constellation is NASA´s program to implement the human exploration of the moon and Mars. This paper focuses on the overall design and operational strategy for the Constellation lunar transportation system architecture including the Ares V heavy lift launch vehicle, Altair lunar lander and early concepts for lunar surface systems including habitats and mobile vehicles. The architecture builds on the initial capability vehicles of Ares I and Orion as they will initially fly to the international space station. The architecture is based on extensive trade studies of surface system objectives, lunar lander design options and Ares V design options. In addition to the description of the architecture this paper will briefly provide status of the initial capability building blocks of Ares I and Orion.
  • Keywords
    design engineering; space research; space vehicles; Altair lunar lander design; Ares V; Constellation lunar transportation system; constellation lunar capability point-of-departure architecture; human exploration; launch vehicle; mobile vehicles; Moon;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839548
  • Filename
    4839548