A twelve-month program was conducted to develop and demonstrate an advanced injector to be used with the propellants N2O4/N2H4 at a thrust level of 3000 lbf. Five injectors were tested in 13 unique configurations to establish the parameters necessary to the optimization of performance, dynamic stability, chamber cooling capability, and injector/chamber compatibility. Once established, the optimized parameters were incorporated into a final injector. This last unit was employed in performance and stability demonstration tests and in long-duration durability tests. All contract design goals were met or exceeded by the final optimized injector. (Author)


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    Titel :

    Development and Demonstration of a N2O4/N2H4 Injector


    Beteiligte:
    J. O. Hartsell (Autor:in)

    Erscheinungsdatum :

    1969


    Format / Umfang :

    226 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    MIYAJIMA, H. / KURODA, Y. / NAGASHIMA, R. et al. | AIAA | 1986



    Cleaning of Liquid N2O4

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    High performance N2O4/amine elements

    Falk, A. Y. | NTRS | 1976