The study objective is to characterize the performance capabilities of an inline, shuttle-derived launch vehicle using two design strategies: the first as an early program demonstrator utilizing high structural margins, maximum shuttle assets, and minimal pad impact, the later having undergone structural optimization, flying operational mission GR&A and serving as a baseline for evolutionary upgrades.


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    Title :

    Launch Vehicle Demonstrator Using Shuttle Assets


    Contributors:
    D. M. Creech (author) / G. E. Threet (author) / E. D. Waters (author)

    Publication date :

    2011


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Launch Vehicle Demonstrator Using Shuttle Assets

    D. M. Creech / G. E. Threet / A. D. Philips et al. | NTIS | 2011


    Launch Vehicle Demonstrator Using Shuttle Assets

    Creech, Dennis M. / Threet, Grady E., Jr. / Philips, Alan D. et al. | NTRS | 2011


    Launch Vehicle Demonstrator Using Shuttle Assets

    Threet, Ed / Creech, Dennis / Philips, Alan et al. | AIAA | 2011


    Launch Vehicle Demonstrator Using Shuttle Assets

    Creech, Dennis M. / Threet, Grady E., Jr. / Waters, Eric D. | NTRS | 2011


    Launch Vehicle Demonstrator Using Shuttle Assets

    Creech, D. / Threet, G. / Philips, A. et al. | British Library Conference Proceedings | 2011