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	<title>Comments on: The Mars Landing Approach: Getting Large Payloads to the Surface of the Red Planet</title>
	<atom:link href="http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/feed/" rel="self" type="application/rss+xml" />
	<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/</link>
	<description>Space and astronomy news</description>
	<lastBuildDate>Sun,  8 Nov 2009 10:14:11 -0600</lastBuildDate>
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		<title>By: Martin Doherty</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-64686</link>
		<dc:creator>Martin Doherty</dc:creator>
		<pubDate>Wed, 22 Apr 2009 20:29:32 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-64686</guid>
		<description>I&#039;m surprised that the article made no reference to the detailed humans-to-Mars ideas contained in the book &quot;The Case For Mars&quot; by Robert Zubrin.</description>
		<content:encoded><![CDATA[<p>I&#039;m surprised that the article made no reference to the detailed humans-to-Mars ideas contained in the book &#034;The Case For Mars&#034; by Robert Zubrin.</p>
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		<title>By: Zlaya_sonichka</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-62341</link>
		<dc:creator>Zlaya_sonichka</dc:creator>
		<pubDate>Wed, 08 Apr 2009 19:26:53 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-62341</guid>
		<description>?????????? ????. 
????? ??? ???????? ???????? ? ?????? ??????. ??? ??? ????? ???????? ?? ?????????? ?????????.
? ???? ???? ????? ? ????? ?????? ??? ? ????. ??????, ? ??????? ??? ? ??. ?????????? ??? ???? ))

????? ???? ?????????? ???????. ??? ????????.</description>
		<content:encoded><![CDATA[<p>?????????? ????.<br />
????? ??? ???????? ???????? ? ?????? ??????. ??? ??? ????? ???????? ?? ?????????? ?????????.<br />
? ???? ???? ????? ? ????? ?????? ??? ? ????. ??????, ? ??????? ??? ? ??. ?????????? ??? ???? ))</p>
<p>????? ???? ?????????? ???????. ??? ????????.</p>
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		<title>By: Trevor Davis</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-61003</link>
		<dc:creator>Trevor Davis</dc:creator>
		<pubDate>Tue, 31 Mar 2009 10:57:24 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-61003</guid>
		<description>As much as I would like to see men on Mars, it&#039;s clear we will have to start with the Moon as a means of gaining experience. As for Mars, it might be feasible to use Phobos or Deimos as natural &quot;space stations&quot; to serve as staging points to prepare to land on Mars using smaller vehicles which can utilize present  methods to reach the surface, and then put together the units like &quot;Lego&quot; blocks for the various requirements. All we need are lots of time and $$$$$.</description>
		<content:encoded><![CDATA[<p>As much as I would like to see men on Mars, it&#039;s clear we will have to start with the Moon as a means of gaining experience. As for Mars, it might be feasible to use Phobos or Deimos as natural &#034;space stations&#034; to serve as staging points to prepare to land on Mars using smaller vehicles which can utilize present  methods to reach the surface, and then put together the units like &#034;Lego&#034; blocks for the various requirements. All we need are lots of time and $$$$$.</p>
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		<title>By: Mark</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-54631</link>
		<dc:creator>Mark</dc:creator>
		<pubDate>Thu, 19 Feb 2009 10:42:14 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-54631</guid>
		<description>Real science doesn&#039;t need humans in Earth orbit much less on Mars. The ISS is a $100 billion waste of money. Sending people to Mars would simply be folly.

We have great machines called computers that are already doing a brilliant job of Martian exploration. Let&#039;s stick with what works and leave the childish fantasies of &#039;Wagon Train to the Stars&#039; to Hollywood.</description>
		<content:encoded><![CDATA[<p>Real science doesn&#039;t need humans in Earth orbit much less on Mars. The ISS is a $100 billion waste of money. Sending people to Mars would simply be folly.</p>
<p>We have great machines called computers that are already doing a brilliant job of Martian exploration. Let&#039;s stick with what works and leave the childish fantasies of &#039;Wagon Train to the Stars&#039; to Hollywood.</p>
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		<title>By: mike</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-48264</link>
		<dc:creator>mike</dc:creator>
		<pubDate>Fri, 02 Jan 2009 17:08:31 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-48264</guid>
		<description>oh my god i got an idea,what if first they send an unmanned spacecraft to mars that contains a giant bouncy castle(landing site)
and pump air through it  and when the crew come they would bash into it .but before that they could try to slow dow with parachutes and thrusters. oh and 1 question out of the topic,how long would it take to get to mars by using antimatter rockets?</description>
		<content:encoded><![CDATA[<p>oh my god i got an idea,what if first they send an unmanned spacecraft to mars that contains a giant bouncy castle(landing site)<br />
and pump air through it  and when the crew come they would bash into it .but before that they could try to slow dow with parachutes and thrusters. oh and 1 question out of the topic,how long would it take to get to mars by using antimatter rockets?</p>
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		<title>By: Conic</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-47927</link>
		<dc:creator>Conic</dc:creator>
		<pubDate>Mon, 29 Dec 2008 17:56:49 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-47927</guid>
		<description>&quot;1. A 3 year round trip - no mechanical system ever designed is this reliable. The ISS crew couldn&#039;t fix the toilet without a repair kit from earth.

2. Radiation would kill the crew - if not during the mission anyone going would know that they would probably die prematurely afterwards.

3. The crew would be multinational and politics would play a large part in selection. Would such a crew really be able to remain sane, healthy and effective - or would cabin fever set in ?&quot;

A perfect sample of the kind of misconceptions found among armchair novices.  

1.)  No mechanical devices made that reliable?  How about the Voyager spacecraft?  Made decades ago, and it has lasted decades.  Any mission would have triple redundancy anyway.

2.) Radiation would not kill the crew.  You are simply wrong here.  But even if we want to reduce radiation, we could simply provide an inner room surrounded by the several tons of water needed for the mission.

3.)  The crew would probably be all American.  Or all Russian, or all Chinese.  No nation is going to pay for this project then not send their own people.  And the ISS demonstrated that cooperation is more expensive than taking a project on your own.

We have had people stay in space for over a year, working well with others.  Sure it isnt the most fun thing ever.  But getting to go to mars is a good incentive.

I agree with you on one point: we are unlikely to go to mars any time soon.  But not because the challenges are all too great, rather it is because even people with a basic understanding of space exploration, have huge misconceptions.  Read a book some time.  I suggest &quot;The Case for Mars.&quot;

The greatest barrier to manned exploration to mars is the lack of effort, lack of motivation, and the misconceptions.  Lousy articles like this one certainly dont help.</description>
		<content:encoded><![CDATA[<p>&#034;1. A 3 year round trip &#8211; no mechanical system ever designed is this reliable. The ISS crew couldn&#039;t fix the toilet without a repair kit from earth.</p>
<p>2. Radiation would kill the crew &#8211; if not during the mission anyone going would know that they would probably die prematurely afterwards.</p>
<p>3. The crew would be multinational and politics would play a large part in selection. Would such a crew really be able to remain sane, healthy and effective &#8211; or would cabin fever set in ?&#034;</p>
<p>A perfect sample of the kind of misconceptions found among armchair novices.  </p>
<p>1.)  No mechanical devices made that reliable?  How about the Voyager spacecraft?  Made decades ago, and it has lasted decades.  Any mission would have triple redundancy anyway.</p>
<p>2.) Radiation would not kill the crew.  You are simply wrong here.  But even if we want to reduce radiation, we could simply provide an inner room surrounded by the several tons of water needed for the mission.</p>
<p>3.)  The crew would probably be all American.  Or all Russian, or all Chinese.  No nation is going to pay for this project then not send their own people.  And the ISS demonstrated that cooperation is more expensive than taking a project on your own.</p>
<p>We have had people stay in space for over a year, working well with others.  Sure it isnt the most fun thing ever.  But getting to go to mars is a good incentive.</p>
<p>I agree with you on one point: we are unlikely to go to mars any time soon.  But not because the challenges are all too great, rather it is because even people with a basic understanding of space exploration, have huge misconceptions.  Read a book some time.  I suggest &#034;The Case for Mars.&#034;</p>
<p>The greatest barrier to manned exploration to mars is the lack of effort, lack of motivation, and the misconceptions.  Lousy articles like this one certainly dont help.</p>
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		<title>By: Luis</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-47575</link>
		<dc:creator>Luis</dc:creator>
		<pubDate>Thu, 25 Dec 2008 00:35:22 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-47575</guid>
		<description>Very nice article!</description>
		<content:encoded><![CDATA[<p>Very nice article!</p>
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		<title>By: tsciru324</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-42852</link>
		<dc:creator>tsciru324</dc:creator>
		<pubDate>Tue, 25 Nov 2008 12:42:57 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-42852</guid>
		<description>[b]Ñïóòíèêîâîå òåëåâèäåíèå ïî÷òè äà?îì.[/b] 
 
×òî òàêîå öèô?îâîå òåëåâèäåíèå? ?òî ïå?åäà÷à ñèãíàëà íåïîñ?åäñòâåííî îò òåëåâèçèîííîé àíòåííû â òåëåöåíò?å ê òåëåâèçî?ó ïîñ?åäñòâîì ñïóòíèêà. Óñòàíîâêà ñïóòíèêîâîãî òåëåâèäåíèÿ ïîëüçóåòñÿ ñåãîäíÿ áîëüøîé ïîïóëÿ?íîñòü?, â ñèëó ñâîåé àêòóàëüíîñòè. Óñòàíîâêà ñïóòíèêîâûõ àíòåíí îò íàøåé êîìïàíèè äàåò Âàì âîçìîæíîñòü ï?îñìîò?à áîëüøîãî êîëè÷åñòâà êàíàëîâ, à òàêæå ÍÒÂ ïë?ñ è Ò?èêîëî? ÒÂ. 
 
Ï?è çàêàçå óñòàíîâêè êîìïëåêòà Ò?èêîëî? ÒÂ - êà?òà èç ïàêåòà Ò?èêîëî? &quot;Îïòèìóì&quot; â ïîäà?îê! 
äî 31 äåêàá?ÿ 2008 ãîäà 
 
âñå íà ñàéòå [b]http://www.tsc-i.ru[/b]</description>
		<content:encoded><![CDATA[<p>[b]Ñïóòíèêîâîå òåëåâèäåíèå ïî÷òè äà?îì.[/b] </p>
<p>×òî òàêîå öèô?îâîå òåëåâèäåíèå? ?òî ïå?åäà÷à ñèãíàëà íåïîñ?åäñòâåííî îò òåëåâèçèîííîé àíòåííû â òåëåöåíò?å ê òåëåâèçî?ó ïîñ?åäñòâîì ñïóòíèêà. Óñòàíîâêà ñïóòíèêîâîãî òåëåâèäåíèÿ ïîëüçóåòñÿ ñåãîäíÿ áîëüøîé ïîïóëÿ?íîñòü?, â ñèëó ñâîåé àêòóàëüíîñòè. Óñòàíîâêà ñïóòíèêîâûõ àíòåíí îò íàøåé êîìïàíèè äàåò Âàì âîçìîæíîñòü ï?îñìîò?à áîëüøîãî êîëè÷åñòâà êàíàëîâ, à òàêæå ÍÒÂ ïë?ñ è Ò?èêîëî? ÒÂ. </p>
<p>Ï?è çàêàçå óñòàíîâêè êîìïëåêòà Ò?èêîëî? ÒÂ &#8211; êà?òà èç ïàêåòà Ò?èêîëî? &#034;Îïòèìóì&#034; â ïîäà?îê!<br />
äî 31 äåêàá?ÿ 2008 ãîäà </p>
<p>âñå íà ñàéòå [b]http://www.tsc-i.ru[/b]</p>
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		<title>By: matt</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-39469</link>
		<dc:creator>matt</dc:creator>
		<pubDate>Sun, 09 Nov 2008 22:08:31 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-39469</guid>
		<description>excellent article any thoughts i may have had about using a front mounted rocket system to slow the shuttles speed in the thin martian atmosphere have been put to rest. oh and ivor weener the article was too long for you because you know nothing and are totally ignorant to the point you can&#039;t actually read this from someone who knows exactly what they are talking about!!!

great article once again and keep up the good work

matt</description>
		<content:encoded><![CDATA[<p>excellent article any thoughts i may have had about using a front mounted rocket system to slow the shuttles speed in the thin martian atmosphere have been put to rest. oh and ivor weener the article was too long for you because you know nothing and are totally ignorant to the point you can&#039;t actually read this from someone who knows exactly what they are talking about!!!</p>
<p>great article once again and keep up the good work</p>
<p>matt</p>
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		<title>By: artoftheflatlands</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-37848</link>
		<dc:creator>artoftheflatlands</dc:creator>
		<pubDate>Tue, 28 Oct 2008 07:59:41 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-37848</guid>
		<description>why not a single human, with an oversized thrusterpack, deploying a inflatable nose cone type device then a chute? I think if you played with the numbers it could work good.</description>
		<content:encoded><![CDATA[<p>why not a single human, with an oversized thrusterpack, deploying a inflatable nose cone type device then a chute? I think if you played with the numbers it could work good.</p>
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		<title>By: TomC</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-37135</link>
		<dc:creator>TomC</dc:creator>
		<pubDate>Wed, 22 Oct 2008 03:06:22 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-37135</guid>
		<description>Even at Mars atmospheric density, a 10m heat shield should drop a 5 metric ton craft from Mach 5 in around  a minute, with a peak acceleration briefly on the order of 10G?    

So it sounds like the problem is really just to avoid  &quot;hitting Mars&quot; (falling too fast) during that critical minute or so of aerobraking.   

Instead of using thrusters to brake &quot;horizontal&quot; velocity, why not use them only to slow the rate of descent?  I.e. thrust vertically during aerobraking to maintain altitude and limit vertical velocity - then land with a combination of rocket and parachute for a fast but controlled descent that minimizes rocket fuel.</description>
		<content:encoded><![CDATA[<p>Even at Mars atmospheric density, a 10m heat shield should drop a 5 metric ton craft from Mach 5 in around  a minute, with a peak acceleration briefly on the order of 10G?    </p>
<p>So it sounds like the problem is really just to avoid  &#034;hitting Mars&#034; (falling too fast) during that critical minute or so of aerobraking.   </p>
<p>Instead of using thrusters to brake &#034;horizontal&#034; velocity, why not use them only to slow the rate of descent?  I.e. thrust vertically during aerobraking to maintain altitude and limit vertical velocity &#8211; then land with a combination of rocket and parachute for a fast but controlled descent that minimizes rocket fuel.</p>
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		<title>By: Adiv</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-35797</link>
		<dc:creator>Adiv</dc:creator>
		<pubDate>Fri, 10 Oct 2008 04:21:55 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-35797</guid>
		<description>Why must the transporter enter Mars&#039; orbit at Mach-5? Couldn&#039;t the vehicle slow down sufficiently to get in orbit around the red planet and then a pod vehicle with crew and supplies be released, at a substantially lower speed, thereby ameliorating some of the difficulties associated with deceleration? Alternatively, couldn&#039;t the transport &quot;skim&quot; the atmosphere of Mars, gradually descending and decelerating as it completes a number of orbits?</description>
		<content:encoded><![CDATA[<p>Why must the transporter enter Mars&#039; orbit at Mach-5? Couldn&#039;t the vehicle slow down sufficiently to get in orbit around the red planet and then a pod vehicle with crew and supplies be released, at a substantially lower speed, thereby ameliorating some of the difficulties associated with deceleration? Alternatively, couldn&#039;t the transport &#034;skim&#034; the atmosphere of Mars, gradually descending and decelerating as it completes a number of orbits?</p>
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		<title>By: Refinance and financial crisis</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-35175</link>
		<dc:creator>Refinance and financial crisis</dc:creator>
		<pubDate>Mon, 06 Oct 2008 18:47:15 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-35175</guid>
		<description>To us it is very heavy as well as much in the given situation, and we do not guarantee to you of 100 % the help. We only prompt true decisions on a way of an output from crisis. 
The further depends only on you.</description>
		<content:encoded><![CDATA[<p>To us it is very heavy as well as much in the given situation, and we do not guarantee to you of 100 % the help. We only prompt true decisions on a way of an output from crisis.<br />
The further depends only on you.</p>
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		<title>By: Rick LeBlanc</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-34447</link>
		<dc:creator>Rick LeBlanc</dc:creator>
		<pubDate>Mon, 29 Sep 2008 20:59:32 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-34447</guid>
		<description>Simplest would be to send transport pods to Mars orbit awaiting humans to set up for landing. Fuel, equipment, and the needs for life to be included. No reason a transport pod can&#039;t be assembled in Earth orbit with podlets that would be able to use the airbags and drop greater quantities of small-sized gear from a main frame.  A control pod or a manned orbiting station could be used to gather the pods into a central location. Even a Mars lander and takeoff vehicle could be sent remotely. It take a lot less energy to put a package in Mars orbit than land.</description>
		<content:encoded><![CDATA[<p>Simplest would be to send transport pods to Mars orbit awaiting humans to set up for landing. Fuel, equipment, and the needs for life to be included. No reason a transport pod can&#039;t be assembled in Earth orbit with podlets that would be able to use the airbags and drop greater quantities of small-sized gear from a main frame.  A control pod or a manned orbiting station could be used to gather the pods into a central location. Even a Mars lander and takeoff vehicle could be sent remotely. It take a lot less energy to put a package in Mars orbit than land.</p>
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		<title>By: Omar Sheira</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-32761</link>
		<dc:creator>Omar Sheira</dc:creator>
		<pubDate>Sat, 13 Sep 2008 06:55:02 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-32761</guid>
		<description>&quot;There&#039;s no comfort in the statistics for missions to Mars.&quot;</description>
		<content:encoded><![CDATA[<p>&#034;There&#039;s no comfort in the statistics for missions to Mars.&#034;</p>
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		<title>By: Dan</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-2/#comment-31951</link>
		<dc:creator>Dan</dc:creator>
		<pubDate>Sat, 06 Sep 2008 13:45:25 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-31951</guid>
		<description>I agree with this article - we don&#039;t have the technology to land people on Mars yet. I would actually go further. Manned missions to Mars are complete moonshine at the moment because :

1. A 3 year round trip - no mechanical system ever designed is this reliable. The ISS crew couldn&#039;t fix the toilet without a repair kit from earth. 

2. Radiation would kill the crew - if not during the mission anyone going would know that they would probably die prematurely afterwards. 

3. The crew would be multinational and politics would play a large part in selection. Would such a crew really be able to remain sane, healthy and effective - or would cabin fever set in ?

4. As the article mentions there are serious issues with actually landing on Mars. Neil Armstrong turned off the autopilot and nearly ran out of fuel landing on manual. He was very skilled in bringing Eagle down safely - and lucky. But can we afford to depend on luck ?

People will go to Mars - but probably not for another 50 years. Of I was a politician I would only fund a manned Mars mission (beginning with orbital flight with no landing) if we had the technology to :

(a) Get there in a month, not a year. Advanced nuclear propulsion systems are a necessity, nuclear thermal isn&#039;t good enough. Need exhaust velocities 10 times higher than current chemical rockets. 

(b) Have more than enough ship shielding to protect the crew.

(c) Transport all hardware and living quarters to the surface before the crew get  there - minimises the landing weight problem. 

(d) have completed an unmanned  test flight schedule that demonstrates all this.</description>
		<content:encoded><![CDATA[<p>I agree with this article &#8211; we don&#039;t have the technology to land people on Mars yet. I would actually go further. Manned missions to Mars are complete moonshine at the moment because :</p>
<p>1. A 3 year round trip &#8211; no mechanical system ever designed is this reliable. The ISS crew couldn&#039;t fix the toilet without a repair kit from earth. </p>
<p>2. Radiation would kill the crew &#8211; if not during the mission anyone going would know that they would probably die prematurely afterwards. </p>
<p>3. The crew would be multinational and politics would play a large part in selection. Would such a crew really be able to remain sane, healthy and effective &#8211; or would cabin fever set in ?</p>
<p>4. As the article mentions there are serious issues with actually landing on Mars. Neil Armstrong turned off the autopilot and nearly ran out of fuel landing on manual. He was very skilled in bringing Eagle down safely &#8211; and lucky. But can we afford to depend on luck ?</p>
<p>People will go to Mars &#8211; but probably not for another 50 years. Of I was a politician I would only fund a manned Mars mission (beginning with orbital flight with no landing) if we had the technology to :</p>
<p>(a) Get there in a month, not a year. Advanced nuclear propulsion systems are a necessity, nuclear thermal isn&#039;t good enough. Need exhaust velocities 10 times higher than current chemical rockets. </p>
<p>(b) Have more than enough ship shielding to protect the crew.</p>
<p>(c) Transport all hardware and living quarters to the surface before the crew get  there &#8211; minimises the landing weight problem. </p>
<p>(d) have completed an unmanned  test flight schedule that demonstrates all this.</p>
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		<title>By: dal</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-25923</link>
		<dc:creator>dal</dc:creator>
		<pubDate>Sun, 13 Jul 2008 22:27:24 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-25923</guid>
		<description>Back to the tether concept: more and more elegant

Since exploratory craft would be based in orbit for the tether 
why not tack on a photovoltaic solar array and add a few super-conduction conduits.. to beam down gigawatts of power to the surface which might be used fir chemical conversions.
Another obvious candidate for funding.. since obviously this has great spin-off potential..</description>
		<content:encoded><![CDATA[<p>Back to the tether concept: more and more elegant</p>
<p>Since exploratory craft would be based in orbit for the tether<br />
why not tack on a photovoltaic solar array and add a few super-conduction conduits.. to beam down gigawatts of power to the surface which might be used fir chemical conversions.<br />
Another obvious candidate for funding.. since obviously this has great spin-off potential..</p>
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		<title>By: dal</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-25922</link>
		<dc:creator>dal</dc:creator>
		<pubDate>Sun, 13 Jul 2008 22:19:34 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-25922</guid>
		<description>Cutting the weight of payloads by making components more space efficient might help where every bit helps:

example: using lightweight formwork and CO2 activated foams to build structures and seals by using the locally available materials to build airtight structures.

Another weight saving measure: locate some basecamp near ot at high concentrations of dry ice to facilitate chemical production of rocket fuel.</description>
		<content:encoded><![CDATA[<p>Cutting the weight of payloads by making components more space efficient might help where every bit helps:</p>
<p>example: using lightweight formwork and CO2 activated foams to build structures and seals by using the locally available materials to build airtight structures.</p>
<p>Another weight saving measure: locate some basecamp near ot at high concentrations of dry ice to facilitate chemical production of rocket fuel.</p>
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		<title>By: dal</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-25921</link>
		<dc:creator>dal</dc:creator>
		<pubDate>Sun, 13 Jul 2008 21:51:25 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-25921</guid>
		<description>I agree with tether concept..it&#039;s an elegant solution and material science can help with the cable tech.

As previously said any infrastructure work can/will be done in layers
robotics first since the technicalities needed to land small robotics is well developed.. 

Funding might be easier if  key technologies such as inflatable structures for extreme environments would be obvious candidates for spin-offs applicable for widespread use here on Earth and elsewhere.  High speed Construction technologies would valuable in may places.</description>
		<content:encoded><![CDATA[<p>I agree with tether concept..it&#039;s an elegant solution and material science can help with the cable tech.</p>
<p>As previously said any infrastructure work can/will be done in layers<br />
robotics first since the technicalities needed to land small robotics is well developed.. </p>
<p>Funding might be easier if  key technologies such as inflatable structures for extreme environments would be obvious candidates for spin-offs applicable for widespread use here on Earth and elsewhere.  High speed Construction technologies would valuable in may places.</p>
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		<title>By: grampsderro</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-24499</link>
		<dc:creator>grampsderro</dc:creator>
		<pubDate>Wed, 25 Jun 2008 07:12:20 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-24499</guid>
		<description>Loved the article and rarchimedes&#039; reply. I have always thought that use of the 2 moons should feature in any Mars manned mission, either as a place to park in orbit, or to source some of the materials needed.
I  have also thought that the mission would need several parts landed separately,utilizing relevant and tried landing technologies for the non-human components.</description>
		<content:encoded><![CDATA[<p>Loved the article and rarchimedes&#039; reply. I have always thought that use of the 2 moons should feature in any Mars manned mission, either as a place to park in orbit, or to source some of the materials needed.<br />
I  have also thought that the mission would need several parts landed separately,utilizing relevant and tried landing technologies for the non-human components.</p>
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		<title>By: Sci-Fi Si</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-22983</link>
		<dc:creator>Sci-Fi Si</dc:creator>
		<pubDate>Sun, 08 Jun 2008 11:25:16 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-22983</guid>
		<description>Fab article, many thanks, enjoyed the read.

I agree with many of the comments stating that next generation fuels is the way to go.

The most substantial problem to over come in a Mars landing is deceleration, which requires extra fuel, which means extra weight on launch and thus tending towards prohibitive costs.

However clean nuclear fuels such as the proton/boron11 or even possibly Helium3/Helium3 (If we can ever refine enough) would provide substantially more power/weight ratio.

Focus fusion is a very promissing step towards using these future fuels.

It is a great shame that Â£4 billion has been cut from the UK physics budget this year and the USA is suffering just as badly from funding cuts.

There is also a novel comment by rarchimedes, good stuff.

Keep up the fab work!</description>
		<content:encoded><![CDATA[<p>Fab article, many thanks, enjoyed the read.</p>
<p>I agree with many of the comments stating that next generation fuels is the way to go.</p>
<p>The most substantial problem to over come in a Mars landing is deceleration, which requires extra fuel, which means extra weight on launch and thus tending towards prohibitive costs.</p>
<p>However clean nuclear fuels such as the proton/boron11 or even possibly Helium3/Helium3 (If we can ever refine enough) would provide substantially more power/weight ratio.</p>
<p>Focus fusion is a very promissing step towards using these future fuels.</p>
<p>It is a great shame that Â£4 billion has been cut from the UK physics budget this year and the USA is suffering just as badly from funding cuts.</p>
<p>There is also a novel comment by rarchimedes, good stuff.</p>
<p>Keep up the fab work!</p>
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		<title>By: jaz</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-22041</link>
		<dc:creator>jaz</dc:creator>
		<pubDate>Wed, 28 May 2008 09:23:43 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-22041</guid>
		<description>this was very insteresting and informal to listne to although the other day a space shuttle landed on mars and  needed inforamtion about that please help kind regards jaz</description>
		<content:encoded><![CDATA[<p>this was very insteresting and informal to listne to although the other day a space shuttle landed on mars and  needed inforamtion about that please help kind regards jaz</p>
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		<title>By: tmayes1999</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-20379</link>
		<dc:creator>tmayes1999</dc:creator>
		<pubDate>Wed, 14 May 2008 07:37:25 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-20379</guid>
		<description>chemical rockets are almost totally useless for crewed interplanetary spaceflight . This requires nuclear propulsion, and nuclear power.
tim</description>
		<content:encoded><![CDATA[<p>chemical rockets are almost totally useless for crewed interplanetary spaceflight . This requires nuclear propulsion, and nuclear power.<br />
tim</p>
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		<title>By: tmayes1999</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-20378</link>
		<dc:creator>tmayes1999</dc:creator>
		<pubDate>Wed, 14 May 2008 07:35:34 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-20378</guid>
		<description>mars escape velocity is 11000 mph orbital 
velocity about 70 % of this value,but you need extra fuel for course corrections 
on the way down from orbit.
tim</description>
		<content:encoded><![CDATA[<p>mars escape velocity is 11000 mph orbital<br />
velocity about 70 % of this value,but you need extra fuel for course corrections<br />
on the way down from orbit.<br />
tim</p>
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		<title>By: tmayes1999</title>
		<link>http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/comment-page-1/#comment-20377</link>
		<dc:creator>tmayes1999</dc:creator>
		<pubDate>Wed, 14 May 2008 07:26:33 +0000</pubDate>
		<guid isPermaLink="false">http://www.universetoday.com/2007/07/17/the-mars-landing-approach-getting-large-payloads-to-the-surface-of-the-red-planet/#comment-20377</guid>
		<description>landing on mars requires enough propulsive braking using retro rockets 
to shed 11000 mph starting in mars orbit .
with a chemical rocket burning h2 + 
o2 this requires a 3/1 mass ratio in
a mars landing vehicle. The best solution is use nuclear thermal rocket propulsion
for going to mars.The critics are not objective and they  have a pre ordained conclusion that fits their radical left wing political ideaology against everything nuclear  and against manned space flight .
That is what the truth is.</description>
		<content:encoded><![CDATA[<p>landing on mars requires enough propulsive braking using retro rockets<br />
to shed 11000 mph starting in mars orbit .<br />
with a chemical rocket burning h2 +<br />
o2 this requires a 3/1 mass ratio in<br />
a mars landing vehicle. The best solution is use nuclear thermal rocket propulsion<br />
for going to mars.The critics are not objective and they  have a pre ordained conclusion that fits their radical left wing political ideaology against everything nuclear  and against manned space flight .<br />
That is what the truth is.</p>
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