Просмотр по теме "sa tellite disposal"

Отображаемые элементы 1-7 из 7

    • Devising a deorbitation strategy for Kazakhstani’s KazEOSat-1 spacecraft 

      Zhumazhanov, B.; Kulakayeva, A.; Ashurov, A.; Baktybekov, K.; Zhetpisbayeva, A.; Uskenbaev, D.; Zhumazhanov, B.; Zylgara, A.; Kargulova, A. (Eastern-European Journal of Enterprise Technologies, 2024)
      The object of this study is the process of deorbiting the KazEOSat-1 spacecraft, which has completed its active service life in low Earth orbit. The main problem is the lack of an effective technique to deorbit KazEOSat-1, taking into account its technical characteristics, orbital parameters, and the need to minimize risks to the environment and other objects in orbit. As ...
      2026-02-23

    • Devising a deorbitation strategy for Kazakhstani’s KazEOSat-1 spacecraft 

      Zhumazhanov, B.; Kulakayeva, A.; Ashurov, A.; Baktybekov, K.; Zhetpisbayeva, A.; Uskenbaev, D.; Zhumazhanov, B.; Zylgara, A.; Kargulova, A. (Eastern-European Journal of Enterprise Technologies, 2024)
      The object of this study is the process of deorbiting the KazEOSat-1 spacecraft, which has completed its active service life in low Earth orbit. The main problem is the lack of an effective technique to deorbit KazEOSat-1, taking into account its technical characteristics, orbital parameters, and the need to minimize risks to the environment and other objects in orbit. As ...
      2026-03-19

    • Devising a deorbitation strategy for Kazakhstani’s KazEOSat-1 spacecraft 

      Zhumazhanov, B.; Kulakayeva, A.; Ashurov, A.; Baktybekov, K.; Zhetpisbayeva, A.; Uskenbaev, D.; Zhumazhanov, B.; Zylgara, A.; Kargulova, A. (Eastern-European Journal of Enterprise Technologies, 2024)
      The object of this study is the process of deorbiting the KazEOSat-1 spacecraft, which has completed its active service life in low Earth orbit. The main problem is the lack of an effective technique to deorbit KazEOSat-1, taking into account its technical characteristics, orbital parameters, and the need to minimize risks to the environment and other objects in orbit. As ...
      2026-03-05

    • DEVISING A DEORBITATION STRATEGY FOR KAZAKHSTANI’S KazEOSat-1 SPACECRAFT 

      Zhumazhanov, B.; Kulakayeva, A.; Ashurov, A.; Baktybekov, K.; Zhetpisbayeva, A.; Uskenbaev, D.; Zhumazhanov, B.; Zylgara, A.; Kargulova, A. (Eastern-European Journal of Enterprise Technologies, 2024)
      The object of this study is the process of deorbiting the KazEOSat-1 spacecraft, which has completed its active service life in low Earth orbit. The main problem is the lack of an effective technique to deorbit KazEOSat-1, taking into account its technical characteristics, orbital parameters, and the need to minimize risks to the environment and other objects in orbit. As ...
      2026-03-17

    • DEVISING A DEORBITATION STRATEGY FOR KAZAKHSTANI’S KazEOSat-1 SPACECRAFT 

      Zhumazhanov, B.; Kulakayeva, A.; Ashurov, A.; Baktybekov, K.; Zhetpisbayeva, A.; Uskenbaev, D.; Zhumazhanov, B.; Zylgara, A.; Kargulova, A. (Eastern-European Journal of Enterprise Technologies, 2024)
      The object of this study is the process of deorbiting the KazEOSat-1 spacecraft, which has completed its active service life in low Earth orbit. The main problem is the lack of an effective technique to deorbit KazEOSat-1, taking into account its technical characteristics, orbital parameters, and the need to minimize risks to the environment and other objects in orbit. As ...
      2026-03-11

    • DEVISING A DEORBITATION STRATEGY FOR KAZAKHSTANI’S KazEOSat-1 SPACECRAFT 

      Zhumazhanov, B.; Kulakayeva, A.; Ashurov, A.; Baktybekov, K.; Zhetpisbayeva, A.; Uskenbaev, D.; Zhumazhanov, B.; Zylgara, A.; Kargulova, A (Eastern-European Journal of Enterprise Technologies, 2024)
      The object of this study is the process of deorbiting the KazEOSat-1 spacecraft, which has completed its active service life in low Earth orbit. The main problem is the lack of an effective technique to deorbit KazEOSat-1, taking into account its technical characteristics, orbital parameters, and the need to minimize risks to the environment and other objects in orbit. As ...
      2026-03-26

    • DEVISING A DEORBITATION STRATEGY FOR KAZAKHSTANI’S KazEOSat-1 SPACECRAFT 

      Zhumazhanov, B.; Kulakayeva, A.; Ashurov, A.; Baktybekov, K.; Zhetpisbayeva, A.; Uskenbaev, D.; Zhumazhanov, B.; Zylgara, A.; Kargulova, A. (Eastern-European Journal of Enterprise Technologies, 2024)
      The object of this study is the process of deorbiting the KazEOSat-1 spacecraft, which has completed its active service life in low Earth orbit. The main problem is the lack of an effective technique to deorbit KazEOSat-1, taking into account its technical characteristics, orbital parameters, and the need to minimize risks to the environment and other objects in orbit. As ...
      2026-01-06