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        <title>Rolls Royce Goshawk engine </title>
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        <![CDATA[ From what i&#39;ve read on this, it was hoped that steam cooling would offer weight saving over water cooling, what kind of weight saving was there for the
vulnerabilities of the system to be accepted?
 ]]>
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		<item>
			<title><![CDATA[ Re: Rolls Royce Goshawk engine  ]]></title>
			<link>http://warships1discussionboards.yuku.com/reply/75161/t/Rolls-Royce-Goshawk-engine.html#reply-75161</link>
			<description><![CDATA[ <blockquote>
  <strong class="quote-title">NewGolconda wrote:</strong>
  <hr>
  Wieght saving? I read drag savings.
  <br>
  <br>
  Around 1930, cooling drag was a major draw back of the in line watercooled engine. RR hoped that steam cooling, with its condensor, would elliminate pr
  significantly reduce coolling drag.
  <br>
  <br>
  As it turns out, advances in radiator design, flowing through from the auto makers, presserised glycol cooling, and the design of adjustable, and later low... ]]></description>

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			<pubDate>Mon, 31 Mar 2008 19:19:45 GMT</pubDate>
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		<item>
			<title><![CDATA[ Re: Rolls Royce Goshawk engine  ]]></title>
			<link>http://warships1discussionboards.yuku.com/reply/75075/t/Rolls-Royce-Goshawk-engine.html#reply-75075</link>
			<description><![CDATA[ Wieght saving? I read drag savings.
<br>
<br>
Around 1930, cooling drag was a major draw back of the in line watercooled engine. RR hoped that steam cooling, with its condensor, would elliminate pr
significantly reduce coolling drag.
<br>
<br>
As it turns out, advances in radiator design, flowing through from the auto makers, presserised glycol cooling, and the design of adjustable, and later low
drag radiator mountings that actually generated thrust from the flow of waste heat were designed,... ]]></description>

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			<author>feeds@yuku.com (NewGolconda)</author>
			<guid isPermaLink="true">http://warships1discussionboards.yuku.com/sreply/75075</guid>
			<pubDate>Sun, 30 Mar 2008 22:07:37 GMT</pubDate>
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		<item>
			<title><![CDATA[ Re: Rolls Royce Goshawk engine  ]]></title>
			<link>http://warships1discussionboards.yuku.com/reply/75058/t/Rolls-Royce-Goshawk-engine.html#reply-75058</link>
			<description><![CDATA[ Ahh, I meant the 1920&#39;s Goshawk engine.
<br> ]]></description>

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			<pubDate>Sun, 30 Mar 2008 19:11:19 GMT</pubDate>
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		<item>
			<title><![CDATA[ Re: Rolls Royce Goshawk engine  ]]></title>
			<link>http://warships1discussionboards.yuku.com/reply/75057/t/Rolls-Royce-Goshawk-engine.html#reply-75057</link>
			<description><![CDATA[ The lightest Adour is the mk 861, at 1,282 lb (second-lightest is the mk 151 at 1,299 lb), and the heaviest are the mk 851 &amp; 106 at 1,360 lb.
<br>
<br>
The F405 (both -400 &amp; -401) is 1,306 lb.
<br>
<br>
At least according to Jane&#39;s and this site: <font size="2"><span style="font-size: 12pt;"><a target="_blank" href="http://www.jet-engine.net/miltfspec.html">http://www.jet-engine.net/miltfspec.html</a></span></font> ]]></description>

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			<author>feeds@yuku.com (bager1968)</author>
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			<pubDate>Sun, 30 Mar 2008 19:06:53 GMT</pubDate>
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		<item>
			<title><![CDATA[ Re: Rolls Royce Goshawk engine  ]]></title>
			<link>http://warships1discussionboards.yuku.com/reply/75050/t/Rolls-Royce-Goshawk-engine.html#reply-75050</link>
			<description><![CDATA[ I can&#39;t see any difference in weight between 100 series Adour and the 800/F405 series ]]></description>

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			<author>feeds@yuku.com (BenRoethig)</author>
			<guid isPermaLink="true">http://warships1discussionboards.yuku.com/sreply/75050</guid>
			<pubDate>Sun, 30 Mar 2008 18:17:44 GMT</pubDate>
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		<item>
			<title><![CDATA[ Rolls Royce Goshawk engine  ]]></title>
			<link>http://warships1discussionboards.yuku.com/topic/5866/t/Rolls-Royce-Goshawk-engine.html</link>
			<description><![CDATA[ From what i&#39;ve read on this, it was hoped that steam cooling would offer weight saving over water cooling, what kind of weight saving was there for the
vulnerabilities of the system to be accepted?
<br> ]]></description>

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			<pubDate>Sun, 30 Mar 2008 17:37:13 GMT</pubDate>
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