Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Design of Injectors and Ablative Thrust Chambers for a Flox-Propane Rocket Engine with a 1.2-Inch Throat Diameter


    Contributors:
    A. J. Pavli (author) / D. A. Peterson (author) / J. M. Winter (author)

    Publication date :

    1969


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    Improved Throat Inserts for Ablative Thrust Chambers

    D. N. Crump / H. H. Henderson / K. J. Smith | NTIS | 1967


    Improved throat inserts for ablative thrust chambers

    Crump, D. N. / Henderson, H. H. / Smith, K. J. | NTRS | 1967