Rocket ignition demonstration tests using silane were performed at the Penn State Combustion Research Laboratory. A heat sink combustor with one injection element was used with gaseous propellants. Mixtures of silane and hydrogen were used as fuel, and oxygen was used as oxidizer. Reliable ignition was demonstrated using fuel lead and and a swirl injection element.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Rocket Ignition Demonstrations Using Silane


    Beteiligte:
    Pal, Sibtosh (Autor:in) / Santoro, Robert (Autor:in) / Watkins, William B. (Autor:in) / Kincaid, Kevin (Autor:in)

    Kongress:

    Propulsion Symposium ; 1998 ; Huntsville, AL, United States


    Erscheinungsdatum :

    14.10.1998


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    System Design and Technical Demonstrations for Reusable Sounding Rocket

    Nonaka, S. / Ogawa, H. / Naruo, Y. et al. | British Library Conference Proceedings | 2011



    Rocket Experiments and Demonstrations for Microwave Power Transmission (MPT)

    Kaya, N. / American Society for Civil Engineers; Aerospace Division | British Library Conference Proceedings | 1996


    Ignition mechanism of scram jet fuel using silane

    HAYASHI, A. / FUJIWARA, TOSHI | AIAA | 1988


    Technical Demonstrations for Reusable Sounding Rocket System (AAS 12-580)

    Nonaka, S. / Ogawa, H. / Naruo, Y. et al. | British Library Conference Proceedings | 2013