Description of the four-year development of Skylab analytical programs, mathematical model complexity, and vibration and load analyses associated with the docking/latching maneuver. Examples are shown where coarse models produced loads in excess of structural capability. However, subsequent model refinement lowered the loads to the point where redesign was not required. A summary of experience gained over a four-year period is presented in the conclusions.


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    Titel :

    Skylab experience with Apollo docking/latching loads.


    Beteiligte:
    Heath, R. A. (Autor:in) / Holland, W. B. (Autor:in)

    Kongress:

    Joint Space Mission Planning and Execution Meeting ; 1973 ; Denver, CO


    Erscheinungsdatum :

    01.07.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Skylab experience with Apollo docking/latching loads

    HEATH, R. / HOLLAND, W. | AIAA | 1973


    Skylab Experience with Apollo Docking/Latching Loads

    R. A. HEATH AND W. B. HOLLAND | AIAA | 1974


    MSFC Skylab Apollo Telescope Mount

    Morse, A. R. | NTRS | 1974


    Apollo-Skylab contamination photography (S226)

    Craven, P. D. / Gary, G. A. | NTRS | 1974


    Msfc Skylab APOLLO Telescope Mount

    A. R. Morse | NTIS | 1974