The Upper Stage Element of NASA's Ares I Crew Launch Vehicle (CLV) is a 'clean-sheet' approach that is being designed and developed in-house, with Element management at MSFC. The USE concept is a self-supporting cylindrical structure, approximately 115 long and 216' in diameter. While the Reusable Solid Rocket Booster (RSRB) design has changed since the CLV inception, the Upper Stage Element design has remained essentially a clean-sheet approach. Although a clean-sheet upper stage design inherently carries more risk than a modified design, it does offer many advantages: a design for increased reliability; built-in extensibility to allow for commonality/growth without major redesign; and incorporation of state-of-the-art materials, hardware, and design, fabrication, and test techniques and processes to facilitate a potentially better, more reliable system.


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    Titel :

    NASA Ares 1 Crew Launch Vehicle Upper Stage Configuration Selection Process


    Beteiligte:
    J. R. Cook (Autor:in)

    Erscheinungsdatum :

    2006


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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