Инд. авторы: Trushlyakov V.I., Kudentsov V.Yu., Lesnyak I.Yu., Lempert D.B., Zarko V.E.
Заглавие: The modeling of unused propellant residues processes from a tank of rocket stage
Библ. ссылка: Trushlyakov V.I., Kudentsov V.Yu., Lesnyak I.Yu., Lempert D.B., Zarko V.E. The modeling of unused propellant residues processes from a tank of rocket stage // 56th Israel Annual Conference on Aerospace Sciences. - 2016.
Внешние системы: SCOPUS: 2-s2.0-84983188003;
Реферат: eng: In this article the physical modeling of processes related to the functioning of the active deorbiting systems of the rocket stage separating parts with liquid propulsion engine (LPE) after completing their mission from orbits and deorbit trajectories is described. The technology of energy resources evaparation from liquid rocket propellant components in the tanks based on the supply of hot gases and their subsequent utilization. The organization of the modeling process on the basis process separation into three stages, the use of model products (obtaining of heat carriers, evaporation, utilization) is proposed. © 2016, Israel Annual Conference on Aerospace Sciences. All rights reserved.
Ключевые слова: Modeling process; Liquid rockets; Liquid propulsion; Hot gas; Heat carriers; Deorbits; Rockets; Tanks (containers); Propellants; Liquid propellants; Energy resources; Aerospace engineering; De-orbiting systems; Physical model;
Издано: 2016
Конференция: Название: 56th Israel Annual Conference on Aerospace Sciences
Аббревиатура: IACAS 2016
Город: Tel-Aviv and Haifa
Страна: Israel
Даты проведения: 2016-03-09 - 2016-03-10