Tests of a 1/15-scale model of the TALOS 6cl missile were performed in the TMB 7- by 10-Foot Transonic Wind Tunnel for a Mach number range of 0.7 to 1.17, at angles of attack of -4 to 10, and roll angles of 0 and -45. The investigation included evaluation of the effects of ram-air bleed at the base of the second stage and the longitudinal stability and control effectiveness of the missile. The data are presented without analysis. (Author)


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    Titel :

    Transonic Wind-Tunnel Tests of A 1/15-Scale Model of the TALOS 6cl Missile


    Beteiligte:
    M. E. McDonald (Autor:in)

    Erscheinungsdatum :

    1961


    Format / Umfang :

    196 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch