NASA s Space Launch Vehicle (SLS) program has chosen the Reusable Solid Rocket Motor V (RSRMV) as the booster system for initial flights. Lift off acoustics continue to be a consideration in overall vehicle vibroacoustic evaluations and launch pad modifications. Work started with the Ares program to understand solid rocket noise mechanisms is continuing through SLS program in conjunction with BYU/Blue Ridge Research Consulting.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Analyses of Noise from Reusable Solid Rocket Motor (RSRM) Firings


    Contributors:
    K. L. Gee (author) / R. J. Kenny (author) / T. W. Jerome (author) / T. B. Neilsen (author) / C. M. Hobbs (author)

    Publication date :

    2012


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Analyses of Noise from Reusable Solid Rocket Motor (RSRM) Firings

    Gee, Kent L. / Kenny, R. Jeremy / Jerome, Trevor W. et al. | NTRS | 2012



    Overview of CFD Analyses Supporting the Reusable Solid Rocket Motor (RSRM) Program at MSFC

    Stewart, Eric / McConnaughey, P. / Lin, J. et al. | NTRS | 1996


    Overview of CFD Analyses Supporting the Reusable Solid Rocket Motor (RSRM) Program at MSFC

    Stewart, E. / McConnaughey, P. / Lin, J. et al. | British Library Conference Proceedings | 1996