Studies of separation dynamics of spin-stabilized satellites and probes indicate possibility of unbalanced moment disturbances during separation process that result in excessively large nutation or coning motions of body in its free flight; paper shows linear acceleration at point away from center of mass on spinning body may be used as driving force for damper system; spinning vehicle equations of motion, including motion of sliding mass, are derived; solutions of resulting fourth-order differential equations for angular rates, and numerical results are presented; approximate design formulas and test program used to verify damper action.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Spinning vehicle nutation damper


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Wadleigh, K.H. (Autor:in) / Galloway, A.J. (Autor:in) / Mathur, P.N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Spinning vehicle nutation damper

    GALLOWAY, A. J. / MATHUR, P. N. / WADLEIGH, K. H. | AIAA | 1964


    Comment on Spinning Vehicle Nutation Damper

    E. J. SLACHMUYLDERS | AIAA | 1965



    CIRCULAR CONSTRAINT NUTATION DAMPER

    CARTWRIGHT, W. F. / MASSINGILL, E. C. / TRUEBLOOD, R. D. | AIAA | 1963


    Eldo-Pas Nutation Damper

    W. H. De Leeuw | NTIS | 1968