The burning pressure - time diagrams were predicted and measured for spinning solid propellant rocket engines. The propellant was in the internal burning star configuration. To predict pressure histories, the acceleration induced and orientation dependent burning rate augmentation data of a solid propellant from slab motor tests were entered into a grain regression program. Composite propellants were tested at spin rates of 0 to 870 rpm. Additional tests of spinning solid propellant rocket engines were conducted in an altitude simulation facility. The measured time histories were compared with the data obtained in the test situation. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Pressure Histories of Spinning Solid Propellant Rocket Motors


    Beteiligte:
    T. Niioka (Autor:in) / S. Ishii (Autor:in) / T. Mitani (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    25 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    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


    Testing solid-propellant rocket motors

    Klient, R.E. / McCown, R.D. | Engineering Index Backfile | 1960