It was found that reduction in thermal radiation from an oxygen-hydrocarbon rocket exhaust flame of 50% or greater might be achieved with the addition of approximately 10% water, by weight, to propellants, with an attendant performance loss on the order of only 2%. (Author)


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    Titel :

    The Effect of Water Injection on the Thermal Radiation from Oxygen-Hydrocarbon Rocket Exhaust Flames


    Beteiligte:
    J. F. Brown (Autor:in)

    Erscheinungsdatum :

    1959


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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