NASA has begun preliminary concept work on the vehicle. Over 1,700 alternatives have been investigated since ESAS. Focused on design of EDS, payload shroud, core stage, and RS-68 core stage engines. Recent point of departure update was made following the Lunar Capability Concept Review. Adds additional performance margin using an additional RS-68. Adds half segment on the first stage boosters . Shroud size is dictated by eventual size of Altair lunar lander. Also investigating alternate uses for Ares V not related to human space exploration . Astronomy applications (e.g., large aperture telescopes), . Deep space missions, DoD applications, Other applications.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Ares V: Overview and Status


    Beteiligte:
    Creech, Steve (Autor:in) / Sumrall, Phil (Autor:in) / Cockrell, Charles E. (Autor:in) / Burris, Mike (Autor:in)

    Erscheinungsdatum :

    2009-10-12


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Ares V: Overview and Status

    S. Creech / P. Sumrall / C. E. Cockrell et al. | NTIS | 2009


    Ares V Overview and Status

    Creech, Steve / Sumrall, Phil / Cockrell, Charles E., Jr. et al. | NTRS | 2009


    Ares I Ares V Overview

    P. Sumrall | NTIS | 2009


    Ares I Ares V Overview

    Sumrall, Phil | NTRS | 2009


    Ares Launch Vehicles Overview

    T. Vanhooser | NTIS | 2009