This report describes an ignition technique whereby rocket motor propellants may be evaluated for smoke production in a quantitative manner with no deleterious effects attributed by the igniter. This technique is also applicable to areas of rocket signature such as flash, IR, RF, and plume studies. The ignition technique is one in which the same propellant being investigated is ground burned at very high pressure with the resulting gases used to ignite the propellant being measured. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Ignition Techniques for Studying Rocket Signature Effects - Smoke


    Beteiligte:
    R. E. Betts (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Solid-Propellant Rocket Ignition Research

    C. F. Sharn / R. L. Beauregard / J. D. Ferguson et al. | NTIS | 1964


    MK 66 Rocket Signature Reduction

    J. D. Habersat | NTIS | 1982


    ROCKET IGNITION AND RELATED NOMENCLATURE

    SAE Technical Papers | 1994


    Ignition of nonhypergolic rocket fuels.

    MUNJAL, N. L. / PRASAD,J. | AIAA | 1972