The Boeing Company under the teaming agreement with the Northrop Grumman Systems Corporation and in compliance with the NASA Phase 1 contract had the responsibilities for the CEV architecture development of the Environmental Control and Life Support (ECLS) system under the NASA Phase 1 contract. The ECLS system was comprised of the various subsystems which provided for a shirt-sleeve habitable environment for crew to live and work in the crew module of the CEV. This architecture met the NASA requirements to ferry cargo and crew to ISS, and Lunar sortie missions, with extensibility to long duration missions to Moon and Mars. This paper provides a summary overview of the CEV ECLS subsystems which was proposed in compliance with the contract activities.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Boeing Crew Exploration Vehicle Environmental Control & Life Support System Architecture Overview


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Lewis, John F. (Autor:in) / Saiidi, Mo (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 2007



    Erscheinungsdatum :

    2007-07-09




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Crew Exploration Vehicle Environmental Control and Life Support Development Status

    Lewis, John / Barido, Richard / Cross, Cynthia et al. | AIAA | 2010



    Crew Exploration Vehicle Environmental Control and Life Support Development Status

    Cross, Cindy / Tuan, George / Lewis, John F. et al. | SAE Technical Papers | 2008


    Crew Exploration Vehicle Environmental Control and Life Support Development Status

    Lewis, John F. / Barido, Richard A. / Cross, Cynthia D. et al. | NTRS | 2011