Abstract On the basis of numerical experiments, we have shown the principal possibility of long (more than 1 month) and extremely long (more than 1 year) orbit lifetime of technogenic microparticles with radii from 1 to 100 μm injected into the near-Earth space in highly elliptical orbits with low perigee, including the case of an orbit with parameters corresponding to the orbital parameters of the Molniya satellite. Calculations are performed taking into account the perturbing effect on the orbital microparticle motion in the near-Earth space of gravitational perturbation caused by the Earth’s polar oblateness, the solar pressure force (calculated using methods of the Mie theory), and the drag force of neutral component of the background gas under conditions of low, medium, and high levels of solar and geomagnetic activities.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Orbit lifetime for microparticles in highly elliptical orbits with low perigee


    Beteiligte:

    Erschienen in:

    Cosmic Research ; 49 , 4 ; 360-366


    Erscheinungsdatum :

    01.08.2011


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Modeling Catastrophic Decay Orbits Through Perigee

    Fischer, J. D. / Cefola, P. J. / Proulx, R. J. et al. | British Library Conference Proceedings | 1998


    A Perigee Orbit Change Method for Geostationary Satellite

    Zhang, ShuHua / Yao, Heng / Li, JianPing et al. | Springer Verlag | 2023


    LONG-TERM PERIGEE HEIGHT VARIATIONS OF GEO DISPOSAL ORBITS - A REVISIT

    Chao, C.-C. / Campbell, S. | British Library Conference Proceedings | 2005



    Perigee Attitude Maneuvers of Geostationary Satellites During Electric Orbit Raising

    Mostaza-Prieto, David / Roberts, Peter C. E. | AIAA | 2017

    Freier Zugriff