Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Supersonic Flight Separation Simulation for TSTO Launch Vehicles Considering Shock Wave Interaction Reduction


    Contributors:

    Conference:

    50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition



    Publication date :

    2012-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Supersonic Flight Separation Simulation for TSTO Launch Vehicles Considering Shock Wave Interaction Reduction

    Uematsu, T. / Aso, S. / Tani, Y. et al. | British Library Conference Proceedings | 2012


    Cost-Optimized Stage Separation Velocity of Winged TSTO Launch Vehicles

    Koelle, D. E. / International Astronautical Federation | British Library Conference Proceedings | 1994


    TSTO Reusable Launch Vehicles Using Airbreathing Propulsion

    Hank, Joseph / Franke, Milton / Eklund, Dean | AIAA | 2006


    TSTO Reusable Launch Vehicles Using Airbreathing Propulsion

    Hank, J. / Franke, M. / Eklund, D. et al. | British Library Conference Proceedings | 2006


    Stage Separation Wind Tunnel Tests of a Generic TSTO Launch Vehicle

    Bordelon, Wayne / Frost, Alonzo / Reed, Darren | AIAA | 2003