Means for generating an inert enveloping gas for surrounding the exhaust plume of a rocket motor are disclosed along with how the enveloping gas serves to prevent the adverse interaction between the rocket motor exhaust plume and the on-board sensors when the rocket motor is operating in exoatmospheric environments. Means for generating an inert enveloping gas utilizes a combination of a T-tube rocket motor and a donut of a chemical which is a gas generant selected from hydrazine bisborane, covalent azides, tetracene, or fluorocarbon-nitroamine. (Author)


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    Titel :

    Inert Gas Generants for Utilization with Rocket Motors


    Beteiligte:
    D. C. Sayles (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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