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	<title>Comments on: Speculating on SpaceShipTwo&#8217;s design</title>
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	<link>http://www.newspacejournal.com/2006/07/11/speculating-on-spaceshiptwos-design/</link>
	<description>Tracking the entrepreneurial space industry</description>
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		<title>By: Jim Howard</title>
		<link>http://www.newspacejournal.com/2006/07/11/speculating-on-spaceshiptwos-design/comment-page-1/#comment-5350</link>
		<dc:creator><![CDATA[Jim Howard]]></dc:creator>
		<pubDate>Wed, 19 Jul 2006 22:43:13 +0000</pubDate>
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		<description><![CDATA[I find the single engine design a little iffy also. I&#039;m hoping for four J79&#039;s with afterburners.

I expect that Burt will tell us a bit more about the SS2 program at Oshkosh next week. For the first time in five years, I can&#039;t go.  grrrrrrrr]]></description>
		<content:encoded><![CDATA[<p>I find the single engine design a little iffy also. I&#8217;m hoping for four J79&#8217;s with afterburners.</p>
<p>I expect that Burt will tell us a bit more about the SS2 program at Oshkosh next week. For the first time in five years, I can&#8217;t go.  grrrrrrrr</p>
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		<title>By: Chance</title>
		<link>http://www.newspacejournal.com/2006/07/11/speculating-on-spaceshiptwos-design/comment-page-1/#comment-4965</link>
		<dc:creator><![CDATA[Chance]]></dc:creator>
		<pubDate>Thu, 13 Jul 2006 16:43:25 +0000</pubDate>
		<guid isPermaLink="false">http://www.personalspaceflight.info/2006/07/11/speculating-on-spaceshiptwos-design/#comment-4965</guid>
		<description><![CDATA[I don&#039;t see a post yet about Bigelow&#039;s test habitat module getting launched.  According to the Space.com article, they intend to send up several more for testing and proof of concept.

Even though it is 99.999999999% certain I will never be able to afford to visit one of his orbital hotels, I am still excited that that percentage will no loger be 100%.  My hats off to Mr. Bigelow for the achievement]]></description>
		<content:encoded><![CDATA[<p>I don&#8217;t see a post yet about Bigelow&#8217;s test habitat module getting launched.  According to the Space.com article, they intend to send up several more for testing and proof of concept.</p>
<p>Even though it is 99.999999999% certain I will never be able to afford to visit one of his orbital hotels, I am still excited that that percentage will no loger be 100%.  My hats off to Mr. Bigelow for the achievement</p>
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		<title>By: Peter</title>
		<link>http://www.newspacejournal.com/2006/07/11/speculating-on-spaceshiptwos-design/comment-page-1/#comment-4910</link>
		<dc:creator><![CDATA[Peter]]></dc:creator>
		<pubDate>Thu, 13 Jul 2006 06:32:07 +0000</pubDate>
		<guid isPermaLink="false">http://www.personalspaceflight.info/2006/07/11/speculating-on-spaceshiptwos-design/#comment-4910</guid>
		<description><![CDATA[Don&#039;t expect it to be too differant.  The cabin will be differant but that won&#039;t really affect flight performance.  The description is good but don&#039;t buy into that drawing much.  When up in the sky the pair won&#039;t look too much differant other then the paintjob.
   As for the single turbine theory...  Due to the high altitude and the fact that the turbines aren&#039;t designed to operate that high there is a inherant risk of flame-out due to low oxygen.  On a recent flight of White Knight taking the X-37 up to altitude one of the turbines flamed out after releasing the x-37.  WK2 will certaintly have two (or more) turbines as a safety precaution for this risk.
  Not to mention the fact that two side mounted turbines will be lower than a single.  You don&#039;t want to have the thrust profile significantly higher then the CG.  With SS1 attached WK1 already had the problem of down-pitch with throttle up and an up-pitch with throttle down.]]></description>
		<content:encoded><![CDATA[<p>Don&#8217;t expect it to be too differant.  The cabin will be differant but that won&#8217;t really affect flight performance.  The description is good but don&#8217;t buy into that drawing much.  When up in the sky the pair won&#8217;t look too much differant other then the paintjob.<br />
   As for the single turbine theory&#8230;  Due to the high altitude and the fact that the turbines aren&#8217;t designed to operate that high there is a inherant risk of flame-out due to low oxygen.  On a recent flight of White Knight taking the X-37 up to altitude one of the turbines flamed out after releasing the x-37.  WK2 will certaintly have two (or more) turbines as a safety precaution for this risk.<br />
  Not to mention the fact that two side mounted turbines will be lower than a single.  You don&#8217;t want to have the thrust profile significantly higher then the CG.  With SS1 attached WK1 already had the problem of down-pitch with throttle up and an up-pitch with throttle down.</p>
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		<title>By: Chance</title>
		<link>http://www.newspacejournal.com/2006/07/11/speculating-on-spaceshiptwos-design/comment-page-1/#comment-4681</link>
		<dc:creator><![CDATA[Chance]]></dc:creator>
		<pubDate>Tue, 11 Jul 2006 13:38:19 +0000</pubDate>
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		<description><![CDATA[Would it really be that differant?  You have a proven design, so it seems like it would be pretty complicated to change the design very much.]]></description>
		<content:encoded><![CDATA[<p>Would it really be that differant?  You have a proven design, so it seems like it would be pretty complicated to change the design very much.</p>
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