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 Upper Stage Element concept is a self-supporting cylindrical structure, approximately 84' long and 18' in diameter. While the First Stage Solid Rocket Booster (SRB) design has changed since the CLV inception, the Upper Stage Element design has remained essentially a clean-sheet design approach. A clean-sheet upper stage design does offer many advantages: a design for increased reliability; built-in evolvability to allow for commonality/growth without major redesign; incorporation of state-of-the-art materials and hardware; and incorporation of design, fabrication, and test techniques and processes to facilitate a more operable system.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Ares I Upper Stage Overview


    Contributors:

    Conference:

    AIAA Space 2007 Conference ; 2007 ; Long Beach, CA, United States


    Publication date :

    2007-09-18


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English