A missile piloting system is described, combining a pyrotechnic guidance system creating normal forces near the gravity center and a more classical aerodynamic piloting. The combination is up to 10 times faster than existing systems, and specially adapted for antimissile defense. Studies of the transversal jet devices and of aerodynamic interferences with the main propulsor are also discussed.


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    Titel :

    Pilotage Pif-Paf des Missiles Tactiques (Pif-Paf Piloting of Tactical Missiles)


    Beteiligte:
    B. Lazure (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch