This report contains a description, results and conclusions of flight tests conducted on a fluidic-generator system to environmentally control the firing of aircraft rockets. A spurious-noise acoustic test conducted on the fluidic-generator system is also discussed. Test results are considered successful. Also included are graphs, illustrations of components, and testing configurations. (Author)


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    Fluidic Generator System to Fire Aircraft Rockets Environmentally

    C. J. Campagnuolo / C. J. Sewell / C. D. McKindra | NTIS | 1971



    Aircraft and rockets

    Maezawa, J. / Kobayashi, M. | Tema Archive | 2003


    Rockets for aircraft

    Bruchiss, L. | Engineering Index Backfile | 1945


    Aircraft Rockets

    B. T. Surikov | NTIS | 1981