Four-stage solid propellant missile may be used as 3-stage missile by omitting first stage and adding fins to second stage flare; study made to determine effect of fin area and second stage flare angle on static longitudinal stability; results obtained.


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    Title :

    Investigation of static longitudinal stability characteristics of 0. 067-scale of model of four-stage configuration of scout research vehicle at mach numbers of 2.29, 2.96, 3.96, and 4.65


    Additional title:

    NASA -- Tech Note


    Contributors:
    Jernell, L.S. (author) / Wong, N. (author)


    Publication date :

    1960


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English