<?xml version="1.0" encoding="UTF-8"?><rss version="2.0"
	xmlns:content="http://purl.org/rss/1.0/modules/content/"
	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/"
		>
<channel>
	<title>Comments on: Power source</title>
	<atom:link href="http://blog.aopa.org/helicopter/?feed=rss2&#038;p=319" rel="self" type="application/rss+xml" />
	<link>http://blog.aopa.org/helicopter/?p=319</link>
	<description>AOPA's Helicopter Blog</description>
	<lastBuildDate>Tue, 21 May 2013 12:38:25 +0000</lastBuildDate>
	<sy:updatePeriod>hourly</sy:updatePeriod>
	<sy:updateFrequency>1</sy:updateFrequency>
	<generator>http://wordpress.org/?v=3.5.1</generator>
	<item>
		<title>By: Sean C</title>
		<link>http://blog.aopa.org/helicopter/?p=319#comment-1179</link>
		<dc:creator>Sean C</dc:creator>
		<pubDate>Sun, 26 Sep 2010 21:55:08 +0000</pubDate>
		<guid isPermaLink="false">http://blog.aopa.org/helicopter/?p=319#comment-1179</guid>
		<description><![CDATA[Don&#039;t forget the possibility of aviation-designed diesel engines appearing in helicopters. At least one diesel (the DeltaHawk) is close to certification which has been designed with helicopter operation in mind. The challenge for aviation diesels will be to keep the power-to-weight ratio competitive with existing gasoline engines, or at least close enough to allow their lower fuel burn rate to help compensate for the increased empty weight.]]></description>
		<content:encoded><![CDATA[<p>Don&#8217;t forget the possibility of aviation-designed diesel engines appearing in helicopters. At least one diesel (the DeltaHawk) is close to certification which has been designed with helicopter operation in mind. The challenge for aviation diesels will be to keep the power-to-weight ratio competitive with existing gasoline engines, or at least close enough to allow their lower fuel burn rate to help compensate for the increased empty weight.</p>
]]></content:encoded>
	</item>
	<item>
		<title>By: Alex Kovnat</title>
		<link>http://blog.aopa.org/helicopter/?p=319#comment-1128</link>
		<dc:creator>Alex Kovnat</dc:creator>
		<pubDate>Tue, 24 Aug 2010 17:29:34 +0000</pubDate>
		<guid isPermaLink="false">http://blog.aopa.org/helicopter/?p=319#comment-1128</guid>
		<description><![CDATA[The likely phaseout of 100LL, may well lead to more turbine-powered helicopters. Unless of course a not-too-costly 100 octane lead-free avgas proves possible.]]></description>
		<content:encoded><![CDATA[<p>The likely phaseout of 100LL, may well lead to more turbine-powered helicopters. Unless of course a not-too-costly 100 octane lead-free avgas proves possible.</p>
]]></content:encoded>
	</item>
</channel>
</rss>
