By means of 3 magnetic aspect sensors, aspect of rocket can be computed for whole flight; as example, computation is exposed for Veronique rocket V 27; comparison of results with data given by instruments on board of V 27 shows excellent agreement; rocket remained nose up during all flight, until re-entry in dense layers (45 km); after some wavering, axis is placed on its precession cone; roll is about 55 rpm.


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    Title :

    Results of measurements of attitude of rocket "Veronique" by magnetic means


    Additional title:

    Resultats concernant l'attitude d'une fusee Veronique obtenus au moyen de capteurs magnetiques


    Contributors:
    Israel, G. (author) / Vassy, A. (author)

    Published in:

    Publication date :

    1962


    Size :

    14 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    French







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