<?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/"
	xmlns:media="http://search.yahoo.com/mrss/"
		>
<channel>
	<title>Comments for Space-Based Solar Power</title>
	<atom:link href="http://spacesolarpower.wordpress.com/comments/feed/" rel="self" type="application/rss+xml" />
	<link>http://spacesolarpower.wordpress.com</link>
	<description>a public discussion sponsored by the Space Frontier Foundation</description>
	<lastBuildDate>Thu, 02 Jul 2009 02:45:40 +0000</lastBuildDate>
	<generator>http://wordpress.com/</generator>
	<sy:updatePeriod>hourly</sy:updatePeriod>
	<sy:updateFrequency>1</sy:updateFrequency>
		<item>
		<title>Comment on Time to Build!  A First Look at &#8220;The Initial Plan&#8221; by Alternative Energy</title>
		<link>http://spacesolarpower.wordpress.com/2008/10/13/time-to-build-a-first-look-at-the-initial-plan/#comment-3139</link>
		<dc:creator>Alternative Energy</dc:creator>
		<pubDate>Thu, 02 Jul 2009 02:45:40 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/?p=178#comment-3139</guid>
		<description>Good idea, but I would probably suggest what Geoff had to say about the high-altitude balloon to lower the cost at least until the idea is profected!</description>
		<content:encoded><![CDATA[<p>Good idea, but I would probably suggest what Geoff had to say about the high-altitude balloon to lower the cost at least until the idea is profected!</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on Wireless Power Broadcast for Computers and Phones Anticipated! by Solar Power for Homes</title>
		<link>http://spacesolarpower.wordpress.com/2008/08/23/wireless-power-beaming-for-computers-and-phones-anticipated/#comment-3137</link>
		<dc:creator>Solar Power for Homes</dc:creator>
		<pubDate>Tue, 23 Jun 2009 16:32:15 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/?p=137#comment-3137</guid>
		<description>I am new to your site and the topic, but does it mean that we will have free power for computers in near future?

Anyway, your site is good.
Thank you!</description>
		<content:encoded><![CDATA[<p>I am new to your site and the topic, but does it mean that we will have free power for computers in near future?</p>
<p>Anyway, your site is good.<br />
Thank you!</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on &#8220;How to Build a Space Solar Power System&#8221; by Neil Cox</title>
		<link>http://spacesolarpower.wordpress.com/2007/07/22/how-to-build-a-space-solar-power-system/#comment-3136</link>
		<dc:creator>Neil Cox</dc:creator>
		<pubDate>Tue, 23 Jun 2009 02:10:51 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/2007/07/22/how-to-build-a-space-solar-power-system/#comment-3136</guid>
		<description>~The following is my comment on the  June 26, 2009 Wall Street Journal article.~ The 2500 megawatts mentioned in the article is enough for one very large city. The receiving site occupies several square miles to be completely safe.  Several good things happen if we do this, large scale: Reduced water, coal, nuclear and oil use. Reduced polution and carbon dioxide emissions even compared to the best renewable energy methods, on Earth&#039;s surface. Occupies less land area even at extreme amounts of energy.
At 2500 megawatts, delivered to one square mile, you would want to remove your winter coat after a few minutes exposure, so you are in trouble if it is a hot summer day. From 22,000 miles = GEO altitude, several square miles is the minimum size spot the beam illuminates, unless we go to a shorter wave length such as millimeter waves. With lasers, minimum spot size is perhaps 100 feet and it is deadly in seconds, even on very cold days. Aluminum foil or other metal does give some protection, but it needs to be grounded. Present lasers have low efficiency, and high cost, but lasers may be practical by 2016, as the technology is still advancing rapidly. Thick clouds are a problem for laser wavelengths.
The solar panels can be deployed in LEO = low Earth orbit and can likely power the assembly to GEO altitude = 22,000 miles, but we have not done this even small scale, so some surprises are likely.   Neil</description>
		<content:encoded><![CDATA[<p>~The following is my comment on the  June 26, 2009 Wall Street Journal article.~ The 2500 megawatts mentioned in the article is enough for one very large city. The receiving site occupies several square miles to be completely safe.  Several good things happen if we do this, large scale: Reduced water, coal, nuclear and oil use. Reduced polution and carbon dioxide emissions even compared to the best renewable energy methods, on Earth&#8217;s surface. Occupies less land area even at extreme amounts of energy.<br />
At 2500 megawatts, delivered to one square mile, you would want to remove your winter coat after a few minutes exposure, so you are in trouble if it is a hot summer day. From 22,000 miles = GEO altitude, several square miles is the minimum size spot the beam illuminates, unless we go to a shorter wave length such as millimeter waves. With lasers, minimum spot size is perhaps 100 feet and it is deadly in seconds, even on very cold days. Aluminum foil or other metal does give some protection, but it needs to be grounded. Present lasers have low efficiency, and high cost, but lasers may be practical by 2016, as the technology is still advancing rapidly. Thick clouds are a problem for laser wavelengths.<br />
The solar panels can be deployed in LEO = low Earth orbit and can likely power the assembly to GEO altitude = 22,000 miles, but we have not done this even small scale, so some surprises are likely.   Neil</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on Technical Discussion On Power Beaming: Engineers Take Note! by Andrew Bloss</title>
		<link>http://spacesolarpower.wordpress.com/2007/08/10/technical-discussion-on-power-beaming-engineers-take-note/#comment-3135</link>
		<dc:creator>Andrew Bloss</dc:creator>
		<pubDate>Mon, 15 Jun 2009 02:22:03 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/2007/08/10/technical-discussion-on-power-beaming-engineers-take-note/#comment-3135</guid>
		<description>Hi Coyote,

I think the Dark Sky balloons go well with SBSP.  The balloon based power stations can also be receivers at night for space based powers.  So there is no land footprint, apart from the tether, and the power supply is not interrupted by night.

As an aside, could the balloons themselves store power for the night?  Split water during the day and store the hydrogen in the balloons and burn it at night.  

And finally, perhaps you can reduce launch costs by building an electric space plane with power cells on the wings.</description>
		<content:encoded><![CDATA[<p>Hi Coyote,</p>
<p>I think the Dark Sky balloons go well with SBSP.  The balloon based power stations can also be receivers at night for space based powers.  So there is no land footprint, apart from the tether, and the power supply is not interrupted by night.</p>
<p>As an aside, could the balloons themselves store power for the night?  Split water during the day and store the hydrogen in the balloons and burn it at night.  </p>
<p>And finally, perhaps you can reduce launch costs by building an electric space plane with power cells on the wings.</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on Technical Discussion On Power Beaming: Engineers Take Note! by Raymond N. Cox</title>
		<link>http://spacesolarpower.wordpress.com/2007/08/10/technical-discussion-on-power-beaming-engineers-take-note/#comment-3132</link>
		<dc:creator>Raymond N. Cox</dc:creator>
		<pubDate>Sun, 07 Jun 2009 22:15:59 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/2007/08/10/technical-discussion-on-power-beaming-engineers-take-note/#comment-3132</guid>
		<description>~Following is a condensed version of a forum discussion in Space business at www.space.com  ~ http://www.thespacereview.com/article/1383/1

SSP: a spherical architecture
by Trevor Brown
Monday, June 1, 2009

Space solar power (SSP) is gradually beginning to look practical. Enterprising SSP ventures, such as Solaren Corp. and Space Energy, Inc., are in the midst of developing initial projects to supply energy from space. Solaren Corp. of California has recently reached an agreement with Pacific Gas and Electric, a California utility, to supply 200 megawatts of energy beginning in 2016, while Space Energy, Inc., a Swiss based company, is producing a prototype demonstration satellite that will help it close purchase power agreements with entities it is currently in discussions with.
As SSP advocates are painfully aware, the high expense of launching numerous payloads into space for the assembly of satellites large enough to transmit meaningful amounts of energy to Earth is cost prohibitive. While very large structures in space are theoretically within the realm of the technically possible for legitimate SSP interests, the launch costs associated with the construction of a satellite a few kilometers in length, as would be necessary for large scale energy transmission, are exorbitant. Additionally, the expense of space systems and operations—robotic technologies and the supporting space and Earth-based infrastructure—are extremely high and must be dramatically reduced. While proponents hope that large-scale space infrastructure projects will achieve certain economies of scale that will bring down the cost of each individual launch, component, and support system, the prevailing price tag for the whole of such a project would doubtless be enormous, making it very difficult to compete in the broader energy marketplace.
As such is the case, a critically sought after breakthrough may not be in space construction techniques or in PV performance, but rather in the nature of the physical composition of photovoltaic cells. If photovoltaic cells were produced with elastic properties affording them the capability of expanding, then a significant opportunity would arise for a novel new architecture for SSP: an inflatable sphere.

Scientists at the Technion - Israel Institute of Technology have already made certain strides in spherical photovoltaic technology with the development of photovoltaic balloons. While the Israeli development is of terrestrial photovoltaic balloon technology, the basic premise of crafting an inflatable sphere with elastic photovoltaic cells capable of expanding in reaction to the pressure of gases is a novel approach that could be a game-changing solution for cost-to-orbit factors and issues of on-orbit assembly that are necessary to resolve before establishing SSP architectures in space.

Indeed, the concept of an inflatable photovoltaic sphere is a simple idea that could possibly overcome many of the obstacles that SSP faces. As basic math bears out, such a design would enable extremely large satellites to be lofted into space with substantially increased surface areas. For example, whereas a satellite 5 kilometers in length and 2 kilometers in width would provide a surface area of only 10 square kilometers and would have to maneuver so that its photovoltaic cells could remain in the Sun, a sphere inflated to a diameter of 5 kilometers would provide an illuminated surface area of over 39 square kilometers with no orbital maneuvers necessary. Such architecture would be a far more ideal for damming the nearly 1.4 gigawatts of solar energy continuously pouring through every square kilometer of space in Earth orbit.

The key to the concept’s feasibility is the ability to inflate the sphere rather than painstakingly assemble it in orbit. The sphere could of course be condensed into a very small package for transport into space and would then expand once it achieved orbit. The use of gases would be critical in this regard—large amounts would be compressed very tightly, would weigh virtually nothing, would cost very little. Such a system would still face major technical challenges, including maintaining integrity in a space environment filled with micrometeorites and space debris.

According to the 2007 National Security Space Office (NSSO) study on SSP the United States has limited capabilities to build large structures in space and cannot at present move large amounts of mass into orbit. The United States correspondingly has extremely limited capabilities for in-space manufacturing and construction or in situ space resource utilization. By crafting a balloon-like satellite the amount of on orbit construction for SSP infrastructure would at once be drastically reduced in tandem with the amount of launches necessary for establishing this architecture in space. In wholesale fashion the inflatable sphere would eliminate the many structural components that conventional SSP spacecraft possess, mooting many questions of modularity maximization in the process.

The spherical concept would enable cost-to-orbit factors to be lowered considerably as the platform would weigh much less than conventional models and would require far fewer launches to be brought online. Whereas other SSP plans call for slashing the cost per pound to orbit with substantial increases in launches, the inflatable sphere would slash the overall launch costs by lessening the amount of launches required while still producing a massive surface area for the production of solar energy.

While it would be highly desirable to possess the capabilities discussed in the 2007 NSSO study, an inflatable sphere would be a design that could by-pass the necessity of their development in the short term, making SSP technically and financially practical in the immediate future. Perhaps the resources engendered from the success of spherical SSP could then in turn be utilized to advance the aforementioned capabilities for other commercial, scientific, or military endeavors in the medium of space.

However, for large systems, pieces of the sphere would have to be sewn together in orbit before it can be inflated. If this were the case, larger spheres would doubtless face similar technical obstacles as the smaller conventional SSP platforms in that a significant amount of launches and on orbit assembly would be required for both. It would therefore be necessary to develop the capabilities previously mentioned in the 2007 NSSO SSP study before the project could be undertaken.

Nonetheless, the spherical design would nevertheless continue to afford a satellite with a far larger surface area producing far more solar energy for the amount of resources that were invested. Once an extremely large sphere—100 kilometers in diameter—had been crafted in space, it could be inflated to its full size and would then have the potential of producing tens or hundreds of terawatts of energy from an illuminated area in excess of 15,700 square kilometers. By comparison, the alternative designs, which would also require numerous launches and on orbit assembly, would only produce gigawatts. With the ability to produce such vast amounts of energy, large-scale spheres would surely overcome the manifold economic barriers that have thus far thwarted SSP endeavors, justifying the incursion of the full spectrum of costs—launch, in space assembly, supporting space systems, and supporting terrestrial infrastructure.

Indeed, inflatable space-based spheres with elastic photovoltaic cells could be the energy technology breakthrough that much of the world has been waiting for. Should a space-faring nation with the requisite resources proceed to ring the Earth in GEO with relatively small photovoltaic spheres, or if it should fashion giant photovoltaic spheres, or if it should proceed to do both, the energy resources that the nation in question will have availed itself would be more than considerable. A nation such as the United States would have developed enough clean and renewable solar energy to become one of the world’s foremost energy exporters.

If solar power satellites such as these did come into being, they would very likely necessitate the overhaul of the entire global economy to achieve broad compatibility with the new energy technology. The resultant economic transformation would be incredible, creating many new high technology jobs in industries across the world, but especially in the nation that was at the epicenter of the SSP breakthrough. In fact, of greatest economic impact may not be the new energy technology itself, but rather the wave of innovation arising in complement to the new energy technology.

And yet the tremendous symbolic power that these satellites could possess may have a profound impact far beyond the realm of economics and the environment. Due to their photovoltaic properties, large enough spheres could have a crystalline appearance in space visible from the Earth with the naked eye, giving them the appearance of diamonds in the sky. If this were the case, these satellites would not only drastically reduce carbon emissions and provide a plentiful source of renewable energy, but there physical beauty across the backdrop of both day and night skies could be surreal for onlookers, causing many around the world to become enamored with the entrepreneurial verve of a nation that developed them as well as with the culture that created them. A nation that owned and operated what appeared to be diamonds in the sky producing abundant clean energy would surely be at the forefront of global leadership, attracting the sentiments of much of the world’s population into its socio-political camp.

Of even greater socio-cultural impact could be their effect on the technological aptitude of a nation, as the case may very well be that crystalline discs shining like diamonds in the sky could inspire an entire generation of young Americans to excel in math and science like never before. With the tangible, ever present symbol of mathematical excellence glimmering in the sky by day and by night, kids could very likely develop a whole new appreciation for the “coolness” of science.

Trevor Brown is an author focused on political, economic, and military strategy for the medium of space. He holds a BA from Indiana University and an MSc from Nanyang Technological University.pmn1 e » Fri Jun 05, 2009 5:41 pm 

Interesting concept...but instead of pressurizing the balloons, why not use electric charge to &quot;inflate&quot; the balloons? There are several advantages to this:

1.) In the event of a micrometeorite impact, it would simply pass straight through the balloon while perhaps knocking out a small, insignificant piece of the balloon without causing a violent depressurization which would cause significantly more damage.

2.) In the event of a tear due to an impact, a similar charging mechanism could be used to bring adjacent cells together and some static bond could &quot;re-seal&quot; the structure...however, this may not even be necessary; consider Christmas tree lights which are connected in parallel, if one light goes out the rest function fine, unlike series connected lights.

3.) To state the obvious, you wouldn&#039;t need to pay for gas  
  
» Fri Jun 05, 2009 5:43 pm 

In fact...you may not even need to repair any missing parts unless the part knocked out was sufficiently large enough to cause a huge drop in power...after all, what are a few solar wind particles going to do to it if they get inside 
e
~by neilsox » Sun Jun 07, 2009 8:45 pm PDT
The electric charge to inflate the balloon in orbit (after or instead of inflating with hydrogen) may make the idea doable. If the balloon has a total surface area of 10 square kilometers and a total mass of one million kilograms = 100,000 kilograms per square kilometer = 100 grams per square meter. Much of that mass would need to be the electrical conductors that connect the flexible PV in series parallel, otherwise resistance losses will be excessive. Possible as the balloon needs very little strength in LEO = low Earth orbit and in theory the stretchable PV cells can be extremely thin. You may have a winner. Proven in LEO, similar balloons may be practical at GEO altitude = 36,000 kilometers.   Neil~</description>
		<content:encoded><![CDATA[<p>~Following is a condensed version of a forum discussion in Space business at <a href="http://www.space.com" rel="nofollow">http://www.space.com</a>  ~ <a href="http://www.thespacereview.com/article/1383/1" rel="nofollow">http://www.thespacereview.com/article/1383/1</a></p>
<p>SSP: a spherical architecture<br />
by Trevor Brown<br />
Monday, June 1, 2009</p>
<p>Space solar power (SSP) is gradually beginning to look practical. Enterprising SSP ventures, such as Solaren Corp. and Space Energy, Inc., are in the midst of developing initial projects to supply energy from space. Solaren Corp. of California has recently reached an agreement with Pacific Gas and Electric, a California utility, to supply 200 megawatts of energy beginning in 2016, while Space Energy, Inc., a Swiss based company, is producing a prototype demonstration satellite that will help it close purchase power agreements with entities it is currently in discussions with.<br />
As SSP advocates are painfully aware, the high expense of launching numerous payloads into space for the assembly of satellites large enough to transmit meaningful amounts of energy to Earth is cost prohibitive. While very large structures in space are theoretically within the realm of the technically possible for legitimate SSP interests, the launch costs associated with the construction of a satellite a few kilometers in length, as would be necessary for large scale energy transmission, are exorbitant. Additionally, the expense of space systems and operations—robotic technologies and the supporting space and Earth-based infrastructure—are extremely high and must be dramatically reduced. While proponents hope that large-scale space infrastructure projects will achieve certain economies of scale that will bring down the cost of each individual launch, component, and support system, the prevailing price tag for the whole of such a project would doubtless be enormous, making it very difficult to compete in the broader energy marketplace.<br />
As such is the case, a critically sought after breakthrough may not be in space construction techniques or in PV performance, but rather in the nature of the physical composition of photovoltaic cells. If photovoltaic cells were produced with elastic properties affording them the capability of expanding, then a significant opportunity would arise for a novel new architecture for SSP: an inflatable sphere.</p>
<p>Scientists at the Technion &#8211; Israel Institute of Technology have already made certain strides in spherical photovoltaic technology with the development of photovoltaic balloons. While the Israeli development is of terrestrial photovoltaic balloon technology, the basic premise of crafting an inflatable sphere with elastic photovoltaic cells capable of expanding in reaction to the pressure of gases is a novel approach that could be a game-changing solution for cost-to-orbit factors and issues of on-orbit assembly that are necessary to resolve before establishing SSP architectures in space.</p>
<p>Indeed, the concept of an inflatable photovoltaic sphere is a simple idea that could possibly overcome many of the obstacles that SSP faces. As basic math bears out, such a design would enable extremely large satellites to be lofted into space with substantially increased surface areas. For example, whereas a satellite 5 kilometers in length and 2 kilometers in width would provide a surface area of only 10 square kilometers and would have to maneuver so that its photovoltaic cells could remain in the Sun, a sphere inflated to a diameter of 5 kilometers would provide an illuminated surface area of over 39 square kilometers with no orbital maneuvers necessary. Such architecture would be a far more ideal for damming the nearly 1.4 gigawatts of solar energy continuously pouring through every square kilometer of space in Earth orbit.</p>
<p>The key to the concept’s feasibility is the ability to inflate the sphere rather than painstakingly assemble it in orbit. The sphere could of course be condensed into a very small package for transport into space and would then expand once it achieved orbit. The use of gases would be critical in this regard—large amounts would be compressed very tightly, would weigh virtually nothing, would cost very little. Such a system would still face major technical challenges, including maintaining integrity in a space environment filled with micrometeorites and space debris.</p>
<p>According to the 2007 National Security Space Office (NSSO) study on SSP the United States has limited capabilities to build large structures in space and cannot at present move large amounts of mass into orbit. The United States correspondingly has extremely limited capabilities for in-space manufacturing and construction or in situ space resource utilization. By crafting a balloon-like satellite the amount of on orbit construction for SSP infrastructure would at once be drastically reduced in tandem with the amount of launches necessary for establishing this architecture in space. In wholesale fashion the inflatable sphere would eliminate the many structural components that conventional SSP spacecraft possess, mooting many questions of modularity maximization in the process.</p>
<p>The spherical concept would enable cost-to-orbit factors to be lowered considerably as the platform would weigh much less than conventional models and would require far fewer launches to be brought online. Whereas other SSP plans call for slashing the cost per pound to orbit with substantial increases in launches, the inflatable sphere would slash the overall launch costs by lessening the amount of launches required while still producing a massive surface area for the production of solar energy.</p>
<p>While it would be highly desirable to possess the capabilities discussed in the 2007 NSSO study, an inflatable sphere would be a design that could by-pass the necessity of their development in the short term, making SSP technically and financially practical in the immediate future. Perhaps the resources engendered from the success of spherical SSP could then in turn be utilized to advance the aforementioned capabilities for other commercial, scientific, or military endeavors in the medium of space.</p>
<p>However, for large systems, pieces of the sphere would have to be sewn together in orbit before it can be inflated. If this were the case, larger spheres would doubtless face similar technical obstacles as the smaller conventional SSP platforms in that a significant amount of launches and on orbit assembly would be required for both. It would therefore be necessary to develop the capabilities previously mentioned in the 2007 NSSO SSP study before the project could be undertaken.</p>
<p>Nonetheless, the spherical design would nevertheless continue to afford a satellite with a far larger surface area producing far more solar energy for the amount of resources that were invested. Once an extremely large sphere—100 kilometers in diameter—had been crafted in space, it could be inflated to its full size and would then have the potential of producing tens or hundreds of terawatts of energy from an illuminated area in excess of 15,700 square kilometers. By comparison, the alternative designs, which would also require numerous launches and on orbit assembly, would only produce gigawatts. With the ability to produce such vast amounts of energy, large-scale spheres would surely overcome the manifold economic barriers that have thus far thwarted SSP endeavors, justifying the incursion of the full spectrum of costs—launch, in space assembly, supporting space systems, and supporting terrestrial infrastructure.</p>
<p>Indeed, inflatable space-based spheres with elastic photovoltaic cells could be the energy technology breakthrough that much of the world has been waiting for. Should a space-faring nation with the requisite resources proceed to ring the Earth in GEO with relatively small photovoltaic spheres, or if it should fashion giant photovoltaic spheres, or if it should proceed to do both, the energy resources that the nation in question will have availed itself would be more than considerable. A nation such as the United States would have developed enough clean and renewable solar energy to become one of the world’s foremost energy exporters.</p>
<p>If solar power satellites such as these did come into being, they would very likely necessitate the overhaul of the entire global economy to achieve broad compatibility with the new energy technology. The resultant economic transformation would be incredible, creating many new high technology jobs in industries across the world, but especially in the nation that was at the epicenter of the SSP breakthrough. In fact, of greatest economic impact may not be the new energy technology itself, but rather the wave of innovation arising in complement to the new energy technology.</p>
<p>And yet the tremendous symbolic power that these satellites could possess may have a profound impact far beyond the realm of economics and the environment. Due to their photovoltaic properties, large enough spheres could have a crystalline appearance in space visible from the Earth with the naked eye, giving them the appearance of diamonds in the sky. If this were the case, these satellites would not only drastically reduce carbon emissions and provide a plentiful source of renewable energy, but there physical beauty across the backdrop of both day and night skies could be surreal for onlookers, causing many around the world to become enamored with the entrepreneurial verve of a nation that developed them as well as with the culture that created them. A nation that owned and operated what appeared to be diamonds in the sky producing abundant clean energy would surely be at the forefront of global leadership, attracting the sentiments of much of the world’s population into its socio-political camp.</p>
<p>Of even greater socio-cultural impact could be their effect on the technological aptitude of a nation, as the case may very well be that crystalline discs shining like diamonds in the sky could inspire an entire generation of young Americans to excel in math and science like never before. With the tangible, ever present symbol of mathematical excellence glimmering in the sky by day and by night, kids could very likely develop a whole new appreciation for the “coolness” of science.</p>
<p>Trevor Brown is an author focused on political, economic, and military strategy for the medium of space. He holds a BA from Indiana University and an MSc from Nanyang Technological University.pmn1 e » Fri Jun 05, 2009 5:41 pm </p>
<p>Interesting concept&#8230;but instead of pressurizing the balloons, why not use electric charge to &#8220;inflate&#8221; the balloons? There are several advantages to this:</p>
<p>1.) In the event of a micrometeorite impact, it would simply pass straight through the balloon while perhaps knocking out a small, insignificant piece of the balloon without causing a violent depressurization which would cause significantly more damage.</p>
<p>2.) In the event of a tear due to an impact, a similar charging mechanism could be used to bring adjacent cells together and some static bond could &#8220;re-seal&#8221; the structure&#8230;however, this may not even be necessary; consider Christmas tree lights which are connected in parallel, if one light goes out the rest function fine, unlike series connected lights.</p>
<p>3.) To state the obvious, you wouldn&#8217;t need to pay for gas  </p>
<p>» Fri Jun 05, 2009 5:43 pm </p>
<p>In fact&#8230;you may not even need to repair any missing parts unless the part knocked out was sufficiently large enough to cause a huge drop in power&#8230;after all, what are a few solar wind particles going to do to it if they get inside<br />
e<br />
~by neilsox » Sun Jun 07, 2009 8:45 pm PDT<br />
The electric charge to inflate the balloon in orbit (after or instead of inflating with hydrogen) may make the idea doable. If the balloon has a total surface area of 10 square kilometers and a total mass of one million kilograms = 100,000 kilograms per square kilometer = 100 grams per square meter. Much of that mass would need to be the electrical conductors that connect the flexible PV in series parallel, otherwise resistance losses will be excessive. Possible as the balloon needs very little strength in LEO = low Earth orbit and in theory the stretchable PV cells can be extremely thin. You may have a winner. Proven in LEO, similar balloons may be practical at GEO altitude = 36,000 kilometers.   Neil~</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on Obama Team Asking for Public Input on Space-Based Solar Power by EcoHearth</title>
		<link>http://spacesolarpower.wordpress.com/2008/12/13/obama-team-asking-for-public-input-on-space-based-solar-power/#comment-3130</link>
		<dc:creator>EcoHearth</dc:creator>
		<pubDate>Tue, 02 Jun 2009 20:44:16 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/2008/12/13/obama-team-asking-for-public-input-on-space-based-solar-power/#comment-3130</guid>
		<description>Check this out: http://ecohearth.com/eco-news/eco-op-ed/593-space-based-solar-power-the-time-has-come.html, a very simple but comprehensive summery of the space based solar issue.</description>
		<content:encoded><![CDATA[<p>Check this out: <a href="http://ecohearth.com/eco-news/eco-op-ed/593-space-based-solar-power-the-time-has-come.html" rel="nofollow">http://ecohearth.com/eco-news/eco-op-ed/593-space-based-solar-power-the-time-has-come.html</a>, a very simple but comprehensive summery of the space based solar issue.</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on Time to Build!  A First Look at &#8220;The Initial Plan&#8221; by Raymond N. Cox</title>
		<link>http://spacesolarpower.wordpress.com/2008/10/13/time-to-build-a-first-look-at-the-initial-plan/#comment-3125</link>
		<dc:creator>Raymond N. Cox</dc:creator>
		<pubDate>Mon, 25 May 2009 17:33:40 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/?p=178#comment-3125</guid>
		<description>Unless Solaran knows something unknown to most of the SSP experts, they will not supply even one megawatt-hour to PG&amp;E by 2017. Getting solar panels to orbit costs way too much with current technology, and slight possibilities such as the space elevator will be available after 2017, if ever.
The study in the 1980s proposed a 5 kilometer antenna at an altitude of 23,000 miles, to send energy to a rectenna that covers about ten square miles. Can you imagine the cost of ten square miles near Fresno, California? One trillion dollars perhaps. If we figure there is no upper limit on radio frequencies, same as the color green perhaps? Then the antenna and the rectenna can be much smaller: Perhaps 2000 square meters. That would be 1/10 th megawatt per square meter, which is a death ray, if you can&#039;t escape in seconds. Exposure feels like a raging fever. At the much higher frequency about a trillion rectenna elements are needed. The rectenna diodes may not rectify at less than ten watts per square centimeter = 100 kilowatts per square meter = 1/10 th megawatt per square meter, unless many elements can be series connected to each diode. As far as I know, rectennas have not been designed for frequencies above about 30 gigahertz There are lots of details at &lt;a href=&quot;http://www.spacesolarpower.com&quot; rel=&quot;nofollow&quot;&gt;www.spacesolarpower.com&lt;/a&gt; which has a great forum.
Death ray is not a problem with present technology which likely cannot illuminate a spot smaller than 300,000 square meters from a distance of 23,000 kilometers. That is 1/10 watt per square centimeter = the allowable leakage from microwave ovens = not dangerous. To put 200 megawatts on the grid the beam needs to have about 300 megawatts. There are some losses in the rectenna, the inverters and the step up transformers.  Neil</description>
		<content:encoded><![CDATA[<p>Unless Solaran knows something unknown to most of the SSP experts, they will not supply even one megawatt-hour to PG&amp;E by 2017. Getting solar panels to orbit costs way too much with current technology, and slight possibilities such as the space elevator will be available after 2017, if ever.<br />
The study in the 1980s proposed a 5 kilometer antenna at an altitude of 23,000 miles, to send energy to a rectenna that covers about ten square miles. Can you imagine the cost of ten square miles near Fresno, California? One trillion dollars perhaps. If we figure there is no upper limit on radio frequencies, same as the color green perhaps? Then the antenna and the rectenna can be much smaller: Perhaps 2000 square meters. That would be 1/10 th megawatt per square meter, which is a death ray, if you can&#8217;t escape in seconds. Exposure feels like a raging fever. At the much higher frequency about a trillion rectenna elements are needed. The rectenna diodes may not rectify at less than ten watts per square centimeter = 100 kilowatts per square meter = 1/10 th megawatt per square meter, unless many elements can be series connected to each diode. As far as I know, rectennas have not been designed for frequencies above about 30 gigahertz There are lots of details at <a href="http://www.spacesolarpower.com" rel="nofollow">http://www.spacesolarpower.com</a> which has a great forum.<br />
Death ray is not a problem with present technology which likely cannot illuminate a spot smaller than 300,000 square meters from a distance of 23,000 kilometers. That is 1/10 watt per square centimeter = the allowable leakage from microwave ovens = not dangerous. To put 200 megawatts on the grid the beam needs to have about 300 megawatts. There are some losses in the rectenna, the inverters and the step up transformers.  Neil</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on Obama Team Asking for Public Input on Space-Based Solar Power by Raymond N. Cox</title>
		<link>http://spacesolarpower.wordpress.com/2008/12/13/obama-team-asking-for-public-input-on-space-based-solar-power/#comment-3120</link>
		<dc:creator>Raymond N. Cox</dc:creator>
		<pubDate>Sat, 23 May 2009 15:15:28 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/2008/12/13/obama-team-asking-for-public-input-on-space-based-solar-power/#comment-3120</guid>
		<description>Most of change.org is no longer accepting comments, but I just successfully submitted two suggestions at  http://change.gov/page/s/ecconomy  Most any suggestion can be related to the ecconomy so this should be a good choice.   Neil</description>
		<content:encoded><![CDATA[<p>Most of change.org is no longer accepting comments, but I just successfully submitted two suggestions at  <a href="http://change.gov/page/s/ecconomy" rel="nofollow">http://change.gov/page/s/ecconomy</a>  Most any suggestion can be related to the ecconomy so this should be a good choice.   Neil</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on Obama Team Asking for Public Input on Space-Based Solar Power by Raymond N. Cox</title>
		<link>http://spacesolarpower.wordpress.com/2008/12/13/obama-team-asking-for-public-input-on-space-based-solar-power/#comment-3119</link>
		<dc:creator>Raymond N. Cox</dc:creator>
		<pubDate>Sat, 23 May 2009 11:36:38 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/2008/12/13/obama-team-asking-for-public-input-on-space-based-solar-power/#comment-3119</guid>
		<description>Low cost delivery to GEO orbit. How about an orbiting tether about 628 kilometers long? It rotates once per hour, so the end passes within about 50 kilometers of the ground while the other end is at an altitude of 678 kilometers. A hypersonic airplane attaches the payload at an altitude of about 51 kilometers, 30 minutes later the pay load is released at an altitude of about 678 kilometers. The circumference of the tip travel is 2000 kilometers, so the speed of the tip is 2000 kilometers per hour, add the speed of rotation of Earth&#039;s equator = about 1600 kilometers per hour subtract the orbital speed of about 28,000 kilometers per hour = -24,400 kilometers per hour = the required speed of the hypersonic airplane. The minus sign has little or no meaning. The release speed is the sum = 31,600 kilometers per hour, so the pay load can go anywhere in the inner solar system, except Mercury and the Sun with a minor mid course correction. So a sling shot maneuver around Jupiter is possible, allowing anywhere in the solar system.
The tether strength requirements are moderate, unless we increase the rotational speed, which decreases the hypersonic airplane speed. Retiring ICBMs = intercontinental ballistic missiles can be modified to attach small pay loads, so we can test the concept without building the hypersonic airplane. There are some more details: 1 We need to reduce the jerk which occurs shortly after attachment, to avoid breaking the tether 2 The tether will be a lazy S instead of straight due to air resistance at 50 kilometers, but the payload and the air resistance will stretch the tether. These tend to cancel. 3 The lift and air resistance are not free, so we will need to restore the 2000 kilometers per hour and circularize the orbit after a few payload lifts. 4 Up to 48 payloads per day can be lifted. 5 The orbit can be semi-polar allowing easy access by most of the nations of Earth and a wide range of throw directions for the payload. 6 The tether will have stretch transients which can aggravate or help the attachment and the throw accuracy. 7 Making the tether longer reduces air resistance and the speed of the hypersonic airplane, but initial cost rises rapidly with length. 8 This concept was published in an old Analog perhaps 20 years ago. 9 An Edwards type climber should travel the tether to repair damage by space junk, atomic oxygen and micro meteorites. Neil</description>
		<content:encoded><![CDATA[<p>Low cost delivery to GEO orbit. How about an orbiting tether about 628 kilometers long? It rotates once per hour, so the end passes within about 50 kilometers of the ground while the other end is at an altitude of 678 kilometers. A hypersonic airplane attaches the payload at an altitude of about 51 kilometers, 30 minutes later the pay load is released at an altitude of about 678 kilometers. The circumference of the tip travel is 2000 kilometers, so the speed of the tip is 2000 kilometers per hour, add the speed of rotation of Earth&#8217;s equator = about 1600 kilometers per hour subtract the orbital speed of about 28,000 kilometers per hour = -24,400 kilometers per hour = the required speed of the hypersonic airplane. The minus sign has little or no meaning. The release speed is the sum = 31,600 kilometers per hour, so the pay load can go anywhere in the inner solar system, except Mercury and the Sun with a minor mid course correction. So a sling shot maneuver around Jupiter is possible, allowing anywhere in the solar system.<br />
The tether strength requirements are moderate, unless we increase the rotational speed, which decreases the hypersonic airplane speed. Retiring ICBMs = intercontinental ballistic missiles can be modified to attach small pay loads, so we can test the concept without building the hypersonic airplane. There are some more details: 1 We need to reduce the jerk which occurs shortly after attachment, to avoid breaking the tether 2 The tether will be a lazy S instead of straight due to air resistance at 50 kilometers, but the payload and the air resistance will stretch the tether. These tend to cancel. 3 The lift and air resistance are not free, so we will need to restore the 2000 kilometers per hour and circularize the orbit after a few payload lifts. 4 Up to 48 payloads per day can be lifted. 5 The orbit can be semi-polar allowing easy access by most of the nations of Earth and a wide range of throw directions for the payload. 6 The tether will have stretch transients which can aggravate or help the attachment and the throw accuracy. 7 Making the tether longer reduces air resistance and the speed of the hypersonic airplane, but initial cost rises rapidly with length. 8 This concept was published in an old Analog perhaps 20 years ago. 9 An Edwards type climber should travel the tether to repair damage by space junk, atomic oxygen and micro meteorites. Neil</p>
]]></content:encoded>
	</item>
	<item>
		<title>Comment on &#8220;How to Build a Space Solar Power System&#8221; by Jim S</title>
		<link>http://spacesolarpower.wordpress.com/2007/07/22/how-to-build-a-space-solar-power-system/#comment-3114</link>
		<dc:creator>Jim S</dc:creator>
		<pubDate>Mon, 18 May 2009 18:44:40 +0000</pubDate>
		<guid isPermaLink="false">http://spacesolarpower.wordpress.com/2007/07/22/how-to-build-a-space-solar-power-system/#comment-3114</guid>
		<description>I have seen some of the environmental concerns being mentioned, but most concerns are being gleefully pushed aside as optimistic potential is slavishly spread over all. CRap!
The major environmental scientists have much to say against this possible use of solar from space and the proponents are not listening and that will hurt solar power and space exploration in the near run greatly. How can proponents push so blindly when warnings are all about, this is a terrible disaster waiting to happen to science if it is pushed forward.
     The political arguments against this type of project are immense, and they come from the Far Right, as well as the Far Left. Of course if the Far Right had their way the sun would likely be put out so they could sell more coal and oil to heat homes, this would shortly end in O2 depletion, but think of the profits in the mean time, lol.The far left have concerns that while they may seem exagerated, may actually be understatements of what could be fact; due to a missunderstanding of domino principles in environmental equations, equations which really need better understanding and research by the way.It may be possible for humanity to gather enough knowledge in the future to actually KNOW how to control global weather and environment, but we need to survive long enough to do so.
    The simplistic concern is of course about how much external &quot;heat&quot; will be brought into the Earth&#039;s environment from an external source; (Space). Once it is on our side of the greenhouse gases CO2, Methane, etc, then it will need to fight it&#039;s way back out to be radiated into space again. It doesn&#039;t matter what form it is initially brought in as, thermodynamics are quite simple , we may change it&#039;s form but whether used for work or heating etc, it still becomes part of the global warmth factor. It is said that the reduction in CO2 emissions will help make the greenhouse barrior less of a barrior. However, it is now estimated that due to the current projections of global warmth CO2 will be released from the natural environmental sources in greator amounts than what we could change if we stopped all use of CO 2 emissions. Natural sources such as Tundra warming and even warming oceans and increasing acid content that might lead to great releases of methane. The last time this happened, it is said that over half of the species on Earth became extinct!

   In other words we will do vastly more harm to the environment than we have ever done before. We need space exploration and space based technology if we are to control the global environmental issues. We need solar panels on Earth to start using the available warmth that is already here, instead of beaming in more heat. We can&#039;t shade the Earth because we need light for the organisms that absorb CO2 in our oceans to coninue to do so, as well as producing O2.We actually need a period of cooling very soon to prevent the release most importantly of Methane, that would be a far worse Greenhouse barrior gas than CO2, while amounts aren&#039;t that great, we could see a huge release in the next 5-20 years and then we could be in a no win situation. Note that this could happen even before solar power to Earth plans are enacted. At that point we would be in dire staits, and beaming in more heat would be our final coffin nail.</description>
		<content:encoded><![CDATA[<p>I have seen some of the environmental concerns being mentioned, but most concerns are being gleefully pushed aside as optimistic potential is slavishly spread over all. CRap!<br />
The major environmental scientists have much to say against this possible use of solar from space and the proponents are not listening and that will hurt solar power and space exploration in the near run greatly. How can proponents push so blindly when warnings are all about, this is a terrible disaster waiting to happen to science if it is pushed forward.<br />
     The political arguments against this type of project are immense, and they come from the Far Right, as well as the Far Left. Of course if the Far Right had their way the sun would likely be put out so they could sell more coal and oil to heat homes, this would shortly end in O2 depletion, but think of the profits in the mean time, lol.The far left have concerns that while they may seem exagerated, may actually be understatements of what could be fact; due to a missunderstanding of domino principles in environmental equations, equations which really need better understanding and research by the way.It may be possible for humanity to gather enough knowledge in the future to actually KNOW how to control global weather and environment, but we need to survive long enough to do so.<br />
    The simplistic concern is of course about how much external &#8220;heat&#8221; will be brought into the Earth&#8217;s environment from an external source; (Space). Once it is on our side of the greenhouse gases CO2, Methane, etc, then it will need to fight it&#8217;s way back out to be radiated into space again. It doesn&#8217;t matter what form it is initially brought in as, thermodynamics are quite simple , we may change it&#8217;s form but whether used for work or heating etc, it still becomes part of the global warmth factor. It is said that the reduction in CO2 emissions will help make the greenhouse barrior less of a barrior. However, it is now estimated that due to the current projections of global warmth CO2 will be released from the natural environmental sources in greator amounts than what we could change if we stopped all use of CO 2 emissions. Natural sources such as Tundra warming and even warming oceans and increasing acid content that might lead to great releases of methane. The last time this happened, it is said that over half of the species on Earth became extinct!</p>
<p>   In other words we will do vastly more harm to the environment than we have ever done before. We need space exploration and space based technology if we are to control the global environmental issues. We need solar panels on Earth to start using the available warmth that is already here, instead of beaming in more heat. We can&#8217;t shade the Earth because we need light for the organisms that absorb CO2 in our oceans to coninue to do so, as well as producing O2.We actually need a period of cooling very soon to prevent the release most importantly of Methane, that would be a far worse Greenhouse barrior gas than CO2, while amounts aren&#8217;t that great, we could see a huge release in the next 5-20 years and then we could be in a no win situation. Note that this could happen even before solar power to Earth plans are enacted. At that point we would be in dire staits, and beaming in more heat would be our final coffin nail.</p>
]]></content:encoded>
	</item>
</channel>
</rss>
