Test firing of 100-lb thrust ablatively cooled rocket chambers


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    An experimental evaluation of 100-lb-thrust ablatively cooled rocket engines


    Contributors:

    Publication date :

    1966-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Ablatively cooled pulse rocket engine design

    FIO RITO / R. J. | AIAA | 1965


    Preliminary Performance Data of an 18kN Ablatively Cooled, Blowdown Liquid Rocket Engine.

    Martin, Duran J. / Cooper, Ryan W. / Wunderlin, Nino et al. | AIAA | 2024


    Transpiration Cooled Ceramic Thrust Chamber Applicability for High-Thrust Rocket Engines

    Herbertz, Armin / Ortelt, Markus / Müller, Ilja et al. | AIAA | 2012