REPOSITORY.ENU

Просмотр по теме "sa tellite disposal"

Просмотр по теме "sa tellite disposal"

Отсортировать по:Порядку:Результатам:

  • 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 ...
  • 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 ...
  • 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 ...
  • 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 ...