<?xml version="1.0" encoding="UTF-8"?>
<rss version="2.0"
	xmlns:content="http://purl.org/rss/1.0/modules/content/"
	xmlns:wfw="http://wellformedweb.org/CommentAPI/"
	xmlns:dc="http://purl.org/dc/elements/1.1/"
	xmlns:atom="http://www.w3.org/2005/Atom"
	xmlns:sy="http://purl.org/rss/1.0/modules/syndication/"
	xmlns:slash="http://purl.org/rss/1.0/modules/slash/"
	>

<channel>
	<title>Электронный научно-практический журнал «Современные научные исследования и инновации» &#187; космический аппарат</title>
	<atom:link href="http://web.snauka.ru/issues/tag/kosmicheskiy-apparat/feed" rel="self" type="application/rss+xml" />
	<link>https://web.snauka.ru</link>
	<description></description>
	<lastBuildDate>Sat, 18 Apr 2026 09:41:14 +0000</lastBuildDate>
	<language>en</language>
	<sy:updatePeriod>hourly</sy:updatePeriod>
	<sy:updateFrequency>1</sy:updateFrequency>
	<generator>http://wordpress.org/?v=3.2.1</generator>
		<item>
		<title>Evaluation of mass characteristics of the system for moving nuclear power plant from the electric propulsion thruster of interorbital space tug</title>
		<link>https://web.snauka.ru/en/issues/2015/11/59126</link>
		<comments>https://web.snauka.ru/en/issues/2015/11/59126#comments</comments>
		<pubDate>Wed, 11 Nov 2015 12:36:44 +0000</pubDate>
		<dc:creator>Косенко Александр Борисович</dc:creator>
				<category><![CDATA[05.00.00 Technical sciences]]></category>
		<category><![CDATA[convertible truss]]></category>
		<category><![CDATA[electric propulsion tug]]></category>
		<category><![CDATA[interorbital space tug]]></category>
		<category><![CDATA[Moon]]></category>
		<category><![CDATA[nuclear power plant]]></category>
		<category><![CDATA[space]]></category>
		<category><![CDATA[spacecraft]]></category>
		<category><![CDATA[космический аппарат]]></category>
		<category><![CDATA[космос]]></category>
		<category><![CDATA[Луна]]></category>
		<category><![CDATA[межорбитальный буксир]]></category>
		<category><![CDATA[трансформируемая ферменная конструкция]]></category>
		<category><![CDATA[электроракетный буксир]]></category>
		<category><![CDATA[ядерная энергетическая установка]]></category>

		<guid isPermaLink="false">https://web.snauka.ru/issues/2015/11/59126</guid>
		<description><![CDATA[Sorry, this article is only available in Русский.]]></description>
			<content:encoded><![CDATA[<p>Sorry, this article is only available in <a href="https://web.snauka.ru/issues/tag/kosmicheskiy-apparat/feed">Русский</a>.</p>
]]></content:encoded>
			<wfw:commentRss>https://web.snauka.ru/en/issues/2015/11/59126/feed</wfw:commentRss>
		<slash:comments>0</slash:comments>
		</item>
		<item>
		<title>Desaturation method for accumulated actuator momentum of the spacecraft on high-elliptic orbit in roll and yaw channels</title>
		<link>https://web.snauka.ru/en/issues/2015/11/59141</link>
		<comments>https://web.snauka.ru/en/issues/2015/11/59141#comments</comments>
		<pubDate>Thu, 12 Nov 2015 13:42:18 +0000</pubDate>
		<dc:creator>Екатерина Воробьева</dc:creator>
				<category><![CDATA[05.00.00 Technical sciences]]></category>
		<category><![CDATA[gravity gradient forces]]></category>
		<category><![CDATA[high-elliptic orbit]]></category>
		<category><![CDATA[inertial actuator]]></category>
		<category><![CDATA[MIMO-system? инерционные исполнительные органы]]></category>
		<category><![CDATA[spacecraft]]></category>
		<category><![CDATA[высокоэллиптическая орбита]]></category>
		<category><![CDATA[гравитационный момент]]></category>
		<category><![CDATA[космический аппарат]]></category>
		<category><![CDATA[МИМО-система]]></category>

		<guid isPermaLink="false">https://web.snauka.ru/issues/2015/11/59141</guid>
		<description><![CDATA[Sorry, this article is only available in Русский.]]></description>
			<content:encoded><![CDATA[<p>Sorry, this article is only available in <a href="https://web.snauka.ru/issues/tag/kosmicheskiy-apparat/feed">Русский</a>.</p>
]]></content:encoded>
			<wfw:commentRss>https://web.snauka.ru/en/issues/2015/11/59141/feed</wfw:commentRss>
		<slash:comments>0</slash:comments>
		</item>
		<item>
		<title>Mathematical modeling of movement small spacecraft around the mass center in the composition of orbital deploy tether system</title>
		<link>https://web.snauka.ru/en/issues/2016/04/67340</link>
		<comments>https://web.snauka.ru/en/issues/2016/04/67340#comments</comments>
		<pubDate>Sat, 30 Apr 2016 11:18:29 +0000</pubDate>
		<dc:creator>Ульянов Никита Владимирович</dc:creator>
				<category><![CDATA[01.00.00 Physics and mathematics]]></category>
		<category><![CDATA[inertia tensor]]></category>
		<category><![CDATA[mathematical modeling]]></category>
		<category><![CDATA[orbital tether system]]></category>
		<category><![CDATA[spacecraft]]></category>
		<category><![CDATA[the equations of motion]]></category>
		<category><![CDATA[космический аппарат]]></category>
		<category><![CDATA[математическое моделирование]]></category>
		<category><![CDATA[орбитальная тросовая система]]></category>
		<category><![CDATA[тензор инерции]]></category>
		<category><![CDATA[уравнения движения]]></category>

		<guid isPermaLink="false">https://web.snauka.ru/issues/2016/04/67340</guid>
		<description><![CDATA[Sorry, this article is only available in Русский.]]></description>
			<content:encoded><![CDATA[<p>Sorry, this article is only available in <a href="https://web.snauka.ru/issues/tag/kosmicheskiy-apparat/feed">Русский</a>.</p>
]]></content:encoded>
			<wfw:commentRss>https://web.snauka.ru/en/issues/2016/04/67340/feed</wfw:commentRss>
		<slash:comments>0</slash:comments>
		</item>
	</channel>
</rss>
