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	Comments on: Air Force requests info for new engine	</title>
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		<title>
		By: Pzatchok		</title>
		<link>https://behindtheblack.com/behind-the-black/points-of-information/air-force-requests-info-for-new-engine/#comment-249941</link>

		<dc:creator><![CDATA[Pzatchok]]></dc:creator>
		<pubDate>Sun, 24 Aug 2014 02:48:08 +0000</pubDate>
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					<description><![CDATA[In reply to &lt;a href=&quot;https://behindtheblack.com/behind-the-black/points-of-information/air-force-requests-info-for-new-engine/#comment-246799&quot;&gt;fred k&lt;/a&gt;.

Not if they design it to match very closely the engines they are already using.


They even have examples to reverse engineer from if they want to go that way.]]></description>
			<content:encoded><![CDATA[<p>In reply to <a href="https://behindtheblack.com/behind-the-black/points-of-information/air-force-requests-info-for-new-engine/#comment-246799">fred k</a>.</p>
<p>Not if they design it to match very closely the engines they are already using.</p>
<p>They even have examples to reverse engineer from if they want to go that way.</p>
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		<title>
		By: Tom Billings		</title>
		<link>https://behindtheblack.com/behind-the-black/points-of-information/air-force-requests-info-for-new-engine/#comment-246809</link>

		<dc:creator><![CDATA[Tom Billings]]></dc:creator>
		<pubDate>Fri, 22 Aug 2014 18:09:18 +0000</pubDate>
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					<description><![CDATA[The F-1 cannot be throttled, IIRC. Thus, the MaxQ would be hugely greater than with the RD-180. 

The rational thing would be to throttle down the SpaceX Raptor engine, and use that to replace the RD-180. LockMart and Boeing would both rather fall on their slide rules than do that, however. Oh yeah, ... the managers never heard of slide rules, ...but they still wouldna&#039; do it.]]></description>
			<content:encoded><![CDATA[<p>The F-1 cannot be throttled, IIRC. Thus, the MaxQ would be hugely greater than with the RD-180. </p>
<p>The rational thing would be to throttle down the SpaceX Raptor engine, and use that to replace the RD-180. LockMart and Boeing would both rather fall on their slide rules than do that, however. Oh yeah, &#8230; the managers never heard of slide rules, &#8230;but they still wouldna&#8217; do it.</p>
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		<title>
		By: fred k		</title>
		<link>https://behindtheblack.com/behind-the-black/points-of-information/air-force-requests-info-for-new-engine/#comment-246799</link>

		<dc:creator><![CDATA[fred k]]></dc:creator>
		<pubDate>Fri, 22 Aug 2014 18:06:57 +0000</pubDate>
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					<description><![CDATA[It is important to note that *any* engine replacement represents a new rocket.   The new engine will have different mass distribution, different aerodynamics, etc, etc.   Attaching a new engine to the same tanks will require the same amount of testing as designing a &quot;new rocket&quot; consisting of new tanks and a new engine.

I suspect ULA would like to have confusion on this subject because is sounds better to have a new engine (and implicitly continue to use them as the provider) rather than switch providers.

In fact, it may be much, much simpler and much, much cheaper to move the payload to another launcher.]]></description>
			<content:encoded><![CDATA[<p>It is important to note that *any* engine replacement represents a new rocket.   The new engine will have different mass distribution, different aerodynamics, etc, etc.   Attaching a new engine to the same tanks will require the same amount of testing as designing a &#8220;new rocket&#8221; consisting of new tanks and a new engine.</p>
<p>I suspect ULA would like to have confusion on this subject because is sounds better to have a new engine (and implicitly continue to use them as the provider) rather than switch providers.</p>
<p>In fact, it may be much, much simpler and much, much cheaper to move the payload to another launcher.</p>
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		<title>
		By: geoffc		</title>
		<link>https://behindtheblack.com/behind-the-black/points-of-information/air-force-requests-info-for-new-engine/#comment-246735</link>

		<dc:creator><![CDATA[geoffc]]></dc:creator>
		<pubDate>Fri, 22 Aug 2014 17:29:22 +0000</pubDate>
		<guid isPermaLink="false">http://behindtheblack.com/?p=30355#comment-246735</guid>

					<description><![CDATA[How about resurect the F-1?  1.5 Million lbs thrust is a bit higher than the 933Klbs of the RD-180 and lower ISP (328 for RD-180, 263s for F-1).  

But you ought to be able to get bigger payloads to orbit this way!  :)]]></description>
			<content:encoded><![CDATA[<p>How about resurect the F-1?  1.5 Million lbs thrust is a bit higher than the 933Klbs of the RD-180 and lower ISP (328 for RD-180, 263s for F-1).  </p>
<p>But you ought to be able to get bigger payloads to orbit this way!  :)</p>
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		<title>
		By: Juan in TN		</title>
		<link>https://behindtheblack.com/behind-the-black/points-of-information/air-force-requests-info-for-new-engine/#comment-246677</link>

		<dc:creator><![CDATA[Juan in TN]]></dc:creator>
		<pubDate>Fri, 22 Aug 2014 16:59:29 +0000</pubDate>
		<guid isPermaLink="false">http://behindtheblack.com/?p=30355#comment-246677</guid>

					<description><![CDATA[Well, it appears they are deadset on going this route so why don&#039;t they dig up a design that is already well along in development.  I am specifically thinking of the RS-84.  I am not a rocket scientist but wasn&#039;t it pretty much completed before it was cancelled?  Even if it wasn&#039;t why can&#039;t it be completed?  It would have to be cheaper than a clean sheet.]]></description>
			<content:encoded><![CDATA[<p>Well, it appears they are deadset on going this route so why don&#8217;t they dig up a design that is already well along in development.  I am specifically thinking of the RS-84.  I am not a rocket scientist but wasn&#8217;t it pretty much completed before it was cancelled?  Even if it wasn&#8217;t why can&#8217;t it be completed?  It would have to be cheaper than a clean sheet.</p>
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