REVOLTING EFFECTS IN OWN ROTATION OF HIGH-ORBITAL SATELLITES

Автор(и)

  • V. P. Epishev Laboratory of space researches, Uzhgorod National University, Dalekaja 2a st. Uzhgorod, 88000, Ukraine, Україна
  • I. I. Isak Laboratory of space researches, Uzhgorod National University, Dalekaja 2a st. Uzhgorod, 88000, Ukraine, Україна
  • Y. M. Motrunich Laboratory of space researches, Uzhgorod National University, Dalekaja 2a st. Uzhgorod, 88000, Ukraine, Україна
  • I. I. Motrunich Laboratory of space researches, Uzhgorod National University, Dalekaja 2a st. Uzhgorod, 88000, Ukraine, Україна
  • I. F. Naubauer Laboratory of space researches, Uzhgorod National University, Dalekaja 2a st. Uzhgorod, 88000, Ukraine, Україна
  • S. S. Pop Laboratory of space researches, Uzhgorod National University, Dalekaja 2a st. Uzhgorod, 88000, Ukraine, Україна
  • V. I. Kudak Laboratory of space researches, Uzhgorod National University, Dalekaja 2a st. Uzhgorod, 88000, Ukraine, Україна

DOI:

https://doi.org/10.18524/1810-4215.2007.20.93641

Ключові слова:

high-orbital satellites.

Анотація

Character of own satellites rotation is analysed, depending on the height of their flight. Results of determination of size of indignations which have influence on a rotation of the probed objects are brought. On the basis of the got results the attempt of estimation of relative change of sun permanent on solar period is done.

Посилання

Епишев В.П., Исак И.И., Мотрунич И.И.‚ Новак Э.И.: 2004, Космічна наука і тexнологія, 10, №5 / 6, 152.

Григоревский В.М.: 1969, Бюлл. ст. оптич. наблюдении искусств. спутников Земли, 54, 9.

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Опубліковано

2017-03-15

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