Following the establishment of the overall transport concept, a study of all of the life limiting constraints associated with the transport were analyzed using modeling techniques. These design techniques included: (1) a response analysis from which the performance of the transport could be determined under operating conditions for a variety of conceptual variations both in a new and aged condition; (2) an analysis of a double cone guidance technique which yielded an optimum design for maximum guidance with minimum tape degradation; (3) an analysis of the tape pack design to eliminate spoking caused by negative tangential stress within the pack; (4) an evaluation of the stress levels experienced by the magnetic tape throughout the system; (5) a general review of the bearing and lubrication technology as applied to satellite recorders and hence the recommendation for using standard load carrying antifriction ball bearings; and (6) a kinetic analysis to determine the change in kinetic properties of the transport during operation.


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    Titel :

    Design study for a high reliability five-year spacecraft tape transport


    Beteiligte:
    Benn, G. S. L. (Autor:in) / Eshleman, R. L. (Autor:in)

    Erscheinungsdatum :

    01.11.1971


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Feasibility model of a high reliability five-year tape transport, Volume 1

    Eshleman, R. L. / Meyers, A. P. / Davidson, W. A. et al. | NTRS | 1973


    Feasibility model of a high reliability five-year tape transport. Volume 3: Appendices

    Meyers, A. P. / Davidson, W. A. / Gortowski, R. C. | NTRS | 1973


    Spacecraft tape recorders

    Heinzmann, J.D. | Engineering Index Backfile | 1966



    Reliability Design of Spacecraft Antenna

    You, Rui / Gao, Wenjun / Wu, Chunbang et al. | Springer Verlag | 2020