The document contains inertial load tables and air load tables relative to the development and the results of a study of the feasibility of designing a standard tactical missile launcher which is capable of carrying and launching hypothetical stores, weighing from 500 to 3,000 pounds, from the F100, F101, F104 and F105 aircraft.


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    AIRCRAFT MISSILE LAUNCHER

    POVETKIN OLEG VALENTINOVICH / PROKOP EV ARTEM LEONIDOVICH / BIKMUKHAMETOV IBRAGIM NURSAFOVICH et al. | Europäisches Patentamt | 2015

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    Missile Launcher Assembly

    E. T. Suydam | NTIS | 1964


    Missile Launcher Detent

    R. Cromwell / J. T. Bratton | NTIS | 1965