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	Comments on: Russia looks to reduce Proton launch costs	</title>
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	<lastBuildDate>Fri, 24 Jun 2016 20:10:17 +0000</lastBuildDate>
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		<title>
		By: Alex		</title>
		<link>https://behindtheblack.com/behind-the-black/points-of-information/russia-looks-to-reduce-proton-launch-costs/#comment-904830</link>

		<dc:creator><![CDATA[Alex]]></dc:creator>
		<pubDate>Fri, 24 Jun 2016 20:10:17 +0000</pubDate>
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					<description><![CDATA[Addition to my comment above: It might be even possible that the Russian engineers remove two of the six RD 253/278 engines for the new design, in order to save money, because there is no need for 1,000 tons launch thrust for the lighter rocket.]]></description>
			<content:encoded><![CDATA[<p>Addition to my comment above: It might be even possible that the Russian engineers remove two of the six RD 253/278 engines for the new design, in order to save money, because there is no need for 1,000 tons launch thrust for the lighter rocket.</p>
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		<title>
		By: Alex		</title>
		<link>https://behindtheblack.com/behind-the-black/points-of-information/russia-looks-to-reduce-proton-launch-costs/#comment-904796</link>

		<dc:creator><![CDATA[Alex]]></dc:creator>
		<pubDate>Fri, 24 Jun 2016 18:40:24 +0000</pubDate>
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					<description><![CDATA[Why not to delete second stage from Proton to save money, by streching the 2.stage? BTW, I would also stretch the first stage tankages due to the large initial T/W-ratio of the launcher (six engines RD-253), which would allow it.]]></description>
			<content:encoded><![CDATA[<p>Why not to delete second stage from Proton to save money, by streching the 2.stage? BTW, I would also stretch the first stage tankages due to the large initial T/W-ratio of the launcher (six engines RD-253), which would allow it.</p>
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