Experiments were conducted in 100-lb-thrust uncooled rocket chamber firing into vacuum tank; special automatic system was used for precise timing of injection of three components, and reliable and repeatable testing conditions were established; optimum timing was determined, and three different ignition delays could be measured which characterized hypergolic ignition of hydrogen and subsequent ignition of main propellants; ignition proved to be very reliable, and only very small quantities of igniter liquid were required.


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    Titel :

    Ignition of hydrogen-oxygen propellant combination by means of chlorine trifluoride


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Sandri, R. (Autor:in) / Billingam, R. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 4 ; p 770-773


    Erscheinungsdatum :

    1967


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :