An artificial gravity experiment which is tethered to a Delta second stage and which uses the Small Expendable Deployer System is proposed. Following tether deployment, the Delta vehicle performs the required spin-up maneuver and can then be passivated. A surplus reentry vehicle houses the artificial gravity life science experiments. When the experiments are completed, the reentry phase of the experiment is initiated by synchronizing the spin of the configuration with the required deorbit impulse.


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    Titel :

    An artificial gravity demonstration experiment


    Beteiligte:
    Rupp, C. (Autor:in) / Lemke, L. (Autor:in) / Penzo, P. (Autor:in)

    Kongress:

    International Conference on Tethers in Space - Toward Flight ; 1989 ; San Francisco, CA, United States


    Erscheinungsdatum :

    1989-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    An artificial gravity demonstration experiment

    RUPP, C. / LEMKE, L. / PENZO, P. | AIAA | 1989


    An artificial gravity performance assessment experiment

    Allen, R. E. / Brown, N. E. / Mallory, K. M., Jr. | NTRS | 1971


    An earth orbital artificial gravity experiment

    GANOUNG, J. / SENATOR, F. | AIAA | 1971