The use of well understood, legacy elements of the Space Shuttle system could yield a near-term, high-confidence Heavy Lift Launch Vehicle that offers significant performance, reliability, schedule, risk, cost, and work force transition benefits. This side-mount Shuttle-Derived Vehicle (SDV) concept has major improvements over previous “Shuttle-C” concepts delivering 78 mt to LEO at an estimated recurring cost of $5,000 per kg. This paper provides the latest data and estimates on the configurations, performance, concept of operations, reliability and safety, development schedule, risks, costs, and work force transition opportunities for this optimized side-mount SDV concept. As shown in this paper the SDV is capable of launching large demonstration and initial operational capability Solar Power Satellite missions.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Applying Proven technologies for a near term, high confidence heavy lift launch vehicle


    Contributors:


    Publication date :

    2009-03-01


    Size :

    3210628 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    A Near Term, High Confidence Heavy Lift Launch Vehicle

    Rothschild, W. / Talay, T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009


    A Near-Term, High-Confidence Heavy Lift Launch Vehicle

    Rothschild, William J. / Talay, Theodore A. | NTRS | 2009


    A Near Term, High Confidence Heavy Lift Launch Vehicle

    Rothschild, William / Talay, Theodore | AIAA | 2009


    APPLICATION OF THE NATIONAL LAUNCH SYSTEM PROVEN TECHNOLOGIES TO NASA'S HEAVY LIFT LAUNCH VEHICLE

    Strobl, W.C. / Hora, R. / Mildice, J. et al. | British Library Conference Proceedings | 2012


    A High Confidence Heavy Lift Launch Vehicle

    Rothschild, William / Talay, Theodore / Henderson, Edward | AIAA | 2010