Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Liquid Metal Heat Pipes for Cooling Rocket Nozzle Walls


    Contributors:

    Conference:

    39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit



    Publication date :

    2003-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





    Liquid propellant rocket engine nozzle with passive condensate cooling

    PATEL JITEN R / CLARK JIM A / WHIPPLE IV CHARLES | European Patent Office | 2021

    Free access

    Analysis of nuclear-rocket nozzle cooling

    Robbins, W.H. / Bachkin, D. / Medeiros, A.A. | Engineering Index Backfile | 1960


    Vaporization Experiment of Liquid Oxygen Cooling Nozzle for Hybrid Rocket Engine

    Mitsutani, T. / Kitagawa, K. / Makita, M. et al. | British Library Conference Proceedings | 2005