The feasibility of influencing the reentry point of the Skylab space station is being evaluated. The concept involves modulation of the drag near the reentry point to induce or delay reentry enough to shift the debris footprint away from a land mass, should its natural trajectory indicate this to be the case. Technologies and strategies are presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Skylab orbit decay update and the eleventh hour contingency plan


    Beteiligte:
    Kaplan, M. H. (Autor:in) / Alexander, S. G. (Autor:in)

    Kongress:

    American Astronautical Society, Annual Rocky Mountain Guidance and Control Conference ; 1979 ; Keystone, CO


    Erscheinungsdatum :

    1979-02-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Simulation of Skylab Orbit Decay and Attitude Dynamics

    Marshall H. Kaplan / David J. Cwynar / Stephen G. Alexander | AIAA | 1979


    Simulation of Skylab orbit decay and attitude dynamics

    KAPLAN, M. / CWYNAR, D. / ALEXANDER, S. | AIAA | 1978


    Skylab flight plan development

    Anderson, W. M. / Holloway, T. W. | NTRS | 1974


    On-Orbit Contingency Plan for the Mars 2020 Mission

    Kruizinga, Gerhard / Jesick, Mark / McCandless, Sarah Elizabeth | NTRS | 2021


    On-Orbit Contingency Plan for the Mars 2020 Mission

    Kruizinga, Gerhard / Jesick, Mark / McCandless, Sarah Elizabeth | NTRS | 2021