Влияние тягоозброености космического аппарата на продолжительность перехода с околоземной на окололунную орбиту

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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