Влияние тягоозброености космического аппарата на продолжительность перехода с околоземной на окололунную орбиту
Рубрика:
| Буланенко, ВЕ, Авдеев, ВВ |
| Косм. наука технол. 2005, 11 ;(Supplement1):018-020 |
| https://doi.org/10.15407/knit2005.01s.018 |
| Язык публикации: Украинский |
Аннотация: Разработана приближенная методика расчета продолжительности перехода и расхода топлива при использовании электроракетного двигателя в квазиимпульсном режиме.
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