Criteria of choice for an engine capable of performing a transfer orbit and a de-orbiting of a launcher’s orbital stage and gasification of the unspent propella

Trushlyakov V. I., Emanuelli M., Tintori C.

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Full metadata record

DC Field	Value	Language
dc.coverage.spatial	деорбитация
dc.coverage.spatial	выбор двигательной установки
dc.coverage.spatial	газификация неизрасходованного топлива
dc.coverage.spatial	удаление с орбиты
dc.coverage.spatial	остаточное ракетное топливо
dc.coverage.spatial	отделяемые ступени
dc.coverage.spatial	ракеты-носители
dc.coverage.spatial	космический мусор
dc.creator	Trushlyakov V. I., Emanuelli M., Tintori C.
dc.date	2011
dc.date.accessioned	2025-08-22T12:21:10Z	-
dc.date.available	2025-08-22T12:21:10Z	-
dc.date.issued	2011
dc.identifier.identifier	RU\НТБ СГАУ\488170
dc.identifier.citation	Trushlyakov, V. I. Criteria of choice for an engine capable of performing a transfer orbit and a de-orbiting of a launcher’s orbital stage and gasification of the unspent propellant of the stage / V. I. Trushlyakov, M. Emanuelli, C. Tintori // Проблемы и перспективы развития двигателестроения : междунар. науч.-техн. конф. : материалы докл., 28-30 июня 2011 г. / Самар. гос. аэрокосм. ун-т им. С. П. Королева (нац. исслед. ун-т) ; редкол.: Е. В. Шахматов, А. И. Ермаков, Ф. В. Паровай. - Самара : СГАУ, 2011Ч. 1. - 2011. - С. 245.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/14299	-
dc.language	eng
dc.relation.ispartof	Проблемы и перспективы развития двигателестроения : междунар. науч.-техн. конф. : материалы докл., 28-30 июня 2011 г. - Текст : электронный
dc.source	Проблемы и перспективы развития двигателестроения. - Ч. 1
dc.subject	деорбитация
dc.subject	выбор двигательной установки
dc.subject	газификация неизрасходованного топлива
dc.subject	удаление с орбиты
dc.subject	остаточное ракетное топливо
dc.subject	отделяемые ступени
dc.subject	ракеты-носители
dc.subject	космический мусор
dc.title	Criteria of choice for an engine capable of performing a transfer orbit and a de-orbiting of a launcher’s orbital stage and gasification of the unspent propella
dc.type	Text
dc.citation.spage	245
local.contributor.author	Trushlyakov V. I.
local.contributor.author	Emanuelli M.
local.contributor.author	Tintori C.
local.identifier.olduri	http://repo.ssau.ru/handle/Probl-i-persp-razvitiya-dvigatelestroeniya/Criteria-of-choice-for-an-engine-capable-of-performing-a-transfer-orbit-and-a-deorbiting-of-a-launcher’s-orbital-stage-and-gasification-of-the-unspent-propellant-of-the-stage-99481
Appears in Collections:	Проблемы и перспективы развития двигателестроения

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