Tests were conducted in Langley Unitary Plan wind tunnel to determine stability characteristics of 0.10-scale model of second and third stages of 3-stage rocket vehicle; 2 fin sizes and planforms, delta and clipped delta, were tested at Mach 3.96 and 4.65 at about 10× 106 Re based on model length; test results are compared with calculated data.


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    Title :

    Static longitudinal stability of rocket vehicle having rear-facing step ahead of stabilizing fins


    Additional title:

    NASA -- Tech Notes


    Contributors:


    Publication date :

    1961


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English





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