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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    Title :

    Development and Demonstration of a N2O4/N2H4 Injector


    Contributors:

    Publication date :

    1969


    Size :

    226 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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