The solid propellant rocket motor is so constructed and arranged that the propellant grain burns through to the case over its entire inner surface at the instant of complete burnout. Thus, during the burning period of the rocket motor, the propellant itself serves as thermal insulation for the case, shielding the latter against the high temperature combustion gases, and at the moment any of the case is first exposed to the hot gases, the combustion process ceases, due to exhaustion of the propellant.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Propellant Grain for Rocket Motors


    Beteiligte:
    R. M. Pierce (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Multiple Propellant Grain for Rocket Motors

    J. V. Braun / W. S. Bacon | NTIS | 1965


    Liquid propellant rocket motors

    Diplock, B.R. / Lofts, D.L. / Grimston, R.A. | Engineering Index Backfile | 1953


    Solid-Propellant Rocket Motors

    Greatrix, David R. | Springer Verlag | 2012


    Solid propellant rocket motors

    Maxwell, W.R. / Young, G.H.S. | Engineering Index Backfile | 1961