271 comments on Solar Satellite Power with Laser Propulsion and Reusable Launch Vehicle
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"Since you posted this piece, please identify Keith Henson, his background and his affiliations."
http://en.wikipedia.org/wiki/Keith_Henson
Of course lots of people seem to *want* low energy world, including a population die back to one or two billion people. Ran into this the first time clear back in 1975 at a Limits to Growth conference. The just formed L5 Society was promoting power satellite. I as a junior member of the team that included Dr. Peter Vajk. He was talking about how power satellites built from lunar resources could really change their disaster models. We were nearly thrown out.
Keith, I just posted a rather polite comment, then refreshed my browser, saw this, and realized what deep denial you're in.
"realized what deep denial you're in."
Hmm. Can you explain what you mean? It is just an observation as far back as 1975 and as recent as last year when Dr. Robert L. Hirsch like to burned my ear off when I suggested there could be a technical breakthrough that could replace fossil fuels.
Sigh. I probably shouldn't have posted that, I know you mean well.
And now you've asked me to clarify it, which is even more awkward.
I mean it in the same sense as I would apply it to the Jehovah's Witnesses who come to my door. They have a paradigm they want to share, and it's a humdinger in terms of features and payoff, and they mean well. Their worldview just has a very low probability of being correct under reasonable standards of analysis. So I thank them and wish them well, which is what I should have done here.
I mean that people like myself who have concluded that a human dieback is probably inevitable don't WANT a dieback, for the most part they have come to unpleasant conclusions after serious study. Your comment about "wanting dieoff" struck me in the same vein as a Jehovah's witness concluding you must want to go to hell if you don't join them saving souls, and I reacted. (At the link you posted, I see you've also been a proponent of cryonics. I wish you luck with the frozen head thing.)
You should give Hirsch more respect. It isn't necessarily due to a bad attitude (as in a desire for billions of deaths) when someone disagrees with you.
"Your comment about "wanting dieoff" struck me in the same vein as a Jehovah's witness concluding you must want to go to hell if you don't join them saving souls, and I reacted."
Perhaps it is incorrect of me to assume they are in favor of a die off when they reject that there even could be a solution to the carbon/energy problems. Operationally though it's the same thing.
Hirsch, like yourself, has worked through the consequences of the data and concluded that a major die off is inevitable. He is hostile to any possibility that his world view might have a flaw in it. This strikes me as religious-like dogmatic thinking.
I can't fault him though, it's probably a more comforting world view than mine. Like Ray Kurzweil and Vernor Vinge I see the technological singularity as inevitable. Only instead of it being the rapture of the nerds, I see our brains being eaten by friendly AIs.
Still, to enjoy this, we probably have to solve energy problems first.
Far out. On what basis do you predicate a Singularity as inevitable? And why would we need to muck about in LEO if we're due to be uploaded soon?
Forgive me for being skeptical. We have a historical record chock full of collapsed civilizations owing to overshoot, after all; also decades of predictions of inevitable breakthroughs in all manner of tech including Kurzweil's nano-based solar. Prudence is warranted when making decisions as to what directions mankind should head in to secure energy supplies sufficient for people to lead a comfortable lifestyle; should we spend $60 billion on SPS or a program for switching the OECD shipping fleet over to alternate fuels we can secure domestically?
As others have commented at present funding options are limited, and many believe the crude oil price runup/spike was a major factor in the present recession. If they are correct, bets are that, in the short term at the least, money will be thrown at solutions that are literally more mundane than SPS.
Where is Hirsch saying that he foresees dieoff? All I've ever heard him predict is that peak oil will lead to extreme hardship, economically and socially. This doesn't equate with mass starvation at all.
"On what basis do you predicate a Singularity as inevitable?"
I don't see any way to avoid it. Singularity is AI and molecular nanotechnology. If we got AI one of the first things to do with it would be to develop nanotechnology. If we got nanotech, one of the things we could do is brute force AI by scanning brains. I knew Eric Drexler from the mid 70s on, been thinking about this for 30 years.
But an energy induced fall in the population looks like it will start decades sooner than mid 2040s--which is where Kurzweil (who has studied it more than anyone) thinks it will happen.
"And why would we need to muck about in LEO if we're due to be uploaded soon?"
It's GEO that's interesting, not LEO. And if I could be certain the singularity would happen before mass starvation and wars start taking the population down I wouldn't bother to think about energy.
The only page I know about that touches on both issues is here: http://www.drmillslmu.com/peakoil.htm
"Which will arrive first? Ecological overshoot and collapse (Malthus), or
a "techno-fix" (Kurzweil)?
No one knows.
But, we probably won't have to wait long to find out. One of these two scenarios will likely
occur within the next several decades. But, which one?
Generally it is healthy to be optimistic.
But optimism can be deadly if it produces a Pollyannaish denial of real problems.
We should not ignore problems by assuming "someone else" will take care
of it, or that "the market" or "technological breakthroughs" will always come
to the rescue in time.
Solutions may not come in time, and we may get a quite rude Malthusian
smack down later. (In my opinion, should the internet go down due to
energy shortages, the Mathusian writing will be on the wall... )
To avoid this, we must solve the transition from our finite, depleting oil resources
to renewable energy.
Technological civilization runs on energy.
****************(end of quote)
". . . should we spend $60 billion on SPS or a program for switching the OECD shipping fleet over to alternate fuels we can secure domestically?"
This *is* a program for alternate fuels. Power at a penny a kWh (what else can you do with off peak power?) can be used to make hydrogen. Hydrogen and C02 reacts just fine to make synthetic oil. True, you only get 56% of the energy in the liquid fuels, but at a dollar a gallon who cares?
Going for SBSP is unlikely to be our decision. (as in the US)
I see no evidence the US could go back to the moon, much less cope with something of this scale.
"extreme hardship, economically and socially"
Is a euphemism for mass death due to wars, famines, epidemics due to weakened immune systems and freezing in the dark. Consider figure 14 here: http://www.theoildrum.com/node/3091 I am sure Hirsch is familiar with it. Hirsch may not be willing to consider a ray of energy hope (for emotional reasons tied to his commitment to this grim future) but he is nobody's fool. When he talks about coming out on the far side in better shape, he is talking about a world with far fewer people.
In some ways that might be a better world. It also might be rather radioactive. In any case, it's going to be a bad time I had rather avoid if possible.
From a strategic point of view this would appear to be an easy system to knock out. In a war situation a belligerant could launch debris or individual satellite killing devices. Anyone dependent on such power sources would immediately be in the dark. In an instant all of that investment could be wiped out. Any proposed energy system should have source diversity (lack of a single kill switch) as one of its requirements.
"From a strategic point of view this would appear to be an easy system to knock out. In a war situation a belligerant could launch debris or individual satellite killing devices."
I am a bit curious as to why someone with the capacity to do it would do it. In a very short time I expect every advanced country would have hundreds of power sats.
One point of this project is to reduce resource competition and therefor the basic reason for wars.
Energy is not the only cause of war or scarce resource in the world. What about ideology - the cause of most wars?
The threat of war will never be eliminated. The only way the threat can be reduced is to have diversity in power sources. If a single madman can wipe out the world then it would have been done many times already. The reason it has not occurred is that we have had diverse ideologies and power sources. Making people dependent on a single kill switch solution (such as your satellites) renders everyone easily vulnerable to such a madman scenario.
"Energy is not the only cause of war or scarce resource in the world. What about ideology (cause of most wars)"
I make the case in "Evolutionary Psychology, Memes and the Origin of War" that ideology is the result of anticipated resource shortages rather than a cause.
"and access to metals?"
With loads of energy you can make metals out of country rock.
North Korea (if it wished) has the same access to scarce resources (including energy) as South Korea. Ideology is the only difference between North and South. Extremist ideology has minimal relationship to energy resources. North Korea could easily wipe out your suggested satellite system many times over with their existing technology.
Assuming they could (a stretch) and they wiped out a Chinese power sat, how long do you think they would last?
The Chinese would be in cahoots and would have the North Koreans knock out US and European satellites on their behalf. Proxy wars are old.
I suppose that's possible. Remind me to have my power sat insured by a Chinese company.
If you want diversity of power sources, which I agree with, then introducing SSP is certainly a good thing. SSP certainly has no single "kill switch". For starters the rectenna on the ground is owned and defended by the local utility and nation receiving the power. The satellite in space would be defended even better by various national military, even better than the growing fleet of communications and other satellites. The increased defense of national and global interests in near space is necessary as our global economic infrastructure increases its presence in cis-lunar space. We must reduce our environmental footprint on earth. I don't think you understand how difficult it would be to "kill" an SSP. It would be sort of like attempting to destroy the interstate highway system with a bomb placed anywhere you like. We may have difficulty preventing that bomb, but violators will be swiftly located and introduced to corrective measures. Everyone that has reliable electric power wants to see their electric power continue.
What about ideology - the cause of most wars?
Are you sure that Ideology is not being used to 'sell' the war VS being the cause?
Back in 1908 - 1912, the dominant meme in the west was that the Great Powers were too interdependent (financially and in trade) for a major war to be possible. There was no "reason for war."
Every technology since steam has been promoted as "reducing the reason for war." Notably, nuclear fission proponents pushed this long and hard. Strangely, despite all these wonderful technologies (that we already have), we still seem to need to "reduce the reason for war."
War does not need reasons.
Two questions:
The problem I have with your argument is the same one I have with Kurzweil's, namely that having the physical capabilities to do something (simulate brains, scan brains) doesn't imply the knowledge or skills needed to exploit that (create strong AI). A scanned brain is just a big pile of data; using that data to create a super-human intelligence is by no means a trivial feat.
This appears to be why Kurzweil's predictions for AI were so off the mark - he's fixating on hardware and ignoring knowledge, which based on my experience is the harder part of solving most problems. (FWIW, his first book is online at his website, and it's interesting to look at his predictions for AI and compare them to what actually happened. With one exception - chess - he was uniformly and wildly over-optimistic.)
Do you have a link to a detailed analysis showing 56% efficiency for electricity-to-oil? I've been trying to find empirical evidence for the efficiency of synthetic oil, but there doesn't seem to be data for an actual implementation of the hydrogen-to-oil leg. There is such data for electrolysis, but all industrial-scale installations I've seen data for were under 50% efficiency.
"Why would nanotech necessarily allow brute-force scanning of brains? "
Molecular disassemblers, an obvious product.
"Why would being able to scan brains necessarily lead to AI? "
Simulation.
Finely infiltrating a brain with enough sensors to tell what the cells were doing would probably work as well.
"Do you have a link to a detailed analysis showing 56% efficiency for electricity-to-oil?"
I worked out the mass and power budget for a 1000 bbl/day forward fuel synthesis plant for the military. It ran on ~100 MW input. I worked the efficiency just before a talk and seem to have got it wrong. I can't get as that low an efficiency now. A bbl of oil is about 1.7MWh. 1000 bbls would be 1700 MWh. 24 hrs x 100 MW is 2400 MWh. 17/24 is 71%. 98% of the energy is for making hydrogen. That could range up to 120 MW which would lower the efficiency to 59%. Some of this could be recovered making steam while cooling the Fischer-Tropsch reactors.
How would that help?
We have no lack of human-level intelligences already - they're called "humans". Why would simulating a few more let us do something new? If the already-existing human intelligences couldn't come up with a supra-human intelligence, why do you so blithely assume the addition of simulated human intelligences would change that?
This isn't a board full of people already convinced of the inevitability of a technological singularity; you can't just wave your hands and say "magic happens" and expect people to believe you.
You're making an enormous assumption about what nanotech can and cannot do. Your argument seems to boil down to:
That's not a persuasive argument. It's more like a statement of faith.
Where is your evidence that a 1000 bbl/day plant runs on 100MW? You can't just arbitrarily choose both input and output volumes, otherwise you've chosen the conversion efficiency, which is exactly what you're trying to calculate!
If this is an example of your calculations, no wonder they don't make sense - you're just making shit up.
Garbage in, garbage out - if there's no evidence behind the numbers you put into your calculations, there's no point in doing the calculations. Industrial electrolysis is 50-70% efficient, meaning that if you seriously believe creation of synthetic diesel from electricity is going to be 70% efficient, you very clearly have no idea what you're talking about.
This is simply embarrassing; are you trying to make renewable energy people look unrealistic and out of touch? That is what you're doing, and right now that's more harm than help.
"Where is your evidence that a 1000 bbl/day plant runs on 100MW?"
Basic chemistry
Liquid fuels can be made out of carbon dioxide by n(CO2) + n(3H2) --> (CH2)n + 2n H2O. (It's exothermic.)
120t C, 60t H2 makes 140t synthetic oil, which is about 1000 bbls
Recipe for 140t of synthetic oil per day
Carbon 120t (5t /hr)
Hydrogen 60t (2.5t/hr)
(40t of Hydrogen combines with the oxygen and is recycled.)
It takes about 100kWh/t to remove carbon dioxide from the air. See http://www.eurekalert.org/pub_releases/2008-09/uoc-cd092908.php (This is equal to 360 kWh/t of carbon.)
Experimentally these researchers have removed CO2 from air at a rate of 20 tons per year with a square meter of scrubber
20 t/year/square meter
20t/year/365/year/m2 x 12/44 = 0.0149 t/d/m2 (C)
120t/d/0.0149 t/d/m2
= 8000m2
100kWh/ton of CO2
366kWh/t of carbon.
5t/hr / .36 MWh/t = 1.8MW
Sanity check, 120t of carbon per day is 5 t/hr Air is 350 ppm CO2 or 95 ppm carbon
1,000,000t of air has 95t of carbon in it
Tonne of air has a volume of about 800 m3
About 1.2 billion m3 of air per day.
Or 1.2Bm3/8000m2, 150 km/day or about 6 km/h. (Half the average wind speed and not as big as the rectenna.)
Electrolytic hydrogen requires 48 MWh/t currently. Recent results from MIT make it possible the energy might get down to 33MWh/t. The chemical equation above requires sixty t of H2 to 120t of carbon.
2.5t/h x 48MWh/ton = 120MW (Theory is 33MWh/t, 83 MW)
For rough numbers, ignore the small energy cost of carbon and use the average of the above line.
"Molecular disassemblers, an obvious product."
Tea. Earl Gray. Hot.
Sorry, Keith. I like graph paper a lot, too. But your overconfidence in the predictive abilities of calculation are like expecting a man who is the same weight and height of Shakespeare to arrive at the same products as long as you give him enough paper..
.. I'm going to my shop, where I can spill some more coffee on that graph paper that earnestly tries to tell me how to connect Post A to Gimbal B ..
Bob
Thanks Pitt. Once again you've said it for me.
The fact that somebody has been thinking about it for decades does not mean didley squat. Brilliant mathematicians spent centuries thinking about how to eliminate Euclid's postulate about parallel lines because their intuition told them that it was not necessary. Guess what? They were all wrong.
Hi Greenish,
Does he mean well? Or is he just caught up in his own technological delusion?
What a depressing post - like the Hydraulic Fracturing essay the other day. I really don't fault Gail for bringing up these technologies - this is our reality - she is more than justifed in bringing them to light. Just as in the other post, I'm sure that Rockman is extremely knowledgeable. And, I'm sure this fellow knows his stuff.
The problem is one of perspective. This post and the one on fracturing seem to imply that human population growth is a given and the only problem is how to accomodate that fact. The really simple solution to all of our problems is to get back into balance with the ecosphere. Basic math tells us that simple family planning measures could accomplish that by the end of the century. This obvious solution here is not to expend enormous amounts of natural resources to put gadgets in orbit, but to design better condums and birth control stuff.
To survive to the end of the century, we don't need to gamble on laser propulsion, we need to convince huge masses of people that bicycles are way more cool than cars.
I could go on - as I'm sure you could - but, is there really much hope when laser propulsion and fracturing is a lot more sexy than bikes and thinner condums.
Hi BikeDave.
I have utterly no doubt he means well; most religious proselytizers do within their self-referential worldview. And I don't begrudge any of them their visions of paradise. One person's rapture is another person's laser ablation, space fleet, frozen head, and robotic upload.
That said, it does seem to evince a rather grotesque perspective on systems thinkers. A quote from the keyposter directly above says:
So Hirsch is the one being religious, and - ipso facto - his conclusions about an inevitable dieoff must be "comforting" to him, which explains why he's "hostile" to those who realize the technological singularity (another non-falsifiable afterlife claim) is inevitable.
By any reasonable criteria, this was a religion key post. "Not that there's anything wrong with it," as Seinfeld would say.
Thanks Dave but I actually just know folks who know a lot about fracing. But I agree with your point to a degree. Fracing gas shales isn't a solution to anything....it's just a way to get more NG out Of the ground. The only potential long term benefit is if we use NG as a buffer while we move onto real solutions. IMO we don't need new tech to save us. We have all the tech now to ease the problem significantly and allow us a more peaceful transition to a low use FF world.
But we won't IMO. And I see the single biggest obstacle is the focus on short term issues. Society is dominated by the 24 hour news cycle. Folks won't tolerate a discussion today about making choices that will affect us 10 or 15 years down the road. They want solutions to finding a job, paying the mortgage, filling up the car with gasoline, etc, etc, NEXT month. The solutions to our future are in the hands of the politicians...not the scientists, not the engineers, not the geologists, not the environmentalists. and certainly not the folks who participate at TOD. And the politicians are ruled by the average citizen. I know it’s old and worn out but it still fits well: “We have met the enemy and he is US.”
Rockman wrote:
While I agree that we are our own worst enemy in many ways, I think that you miss the main point about politics as it's practiced today in the U.S. To get elected requires a massive amount of money. Much of that money comes from corporate sources and the politicians tend to satisfy the needs of those who pay their bills. To be sure, the political game involves attempting to satisfy as many voters as possible while alienating the fewest. But, there's so much corporate propaganda out there that the voters are easily influenced to demand actions which are favorable to the corporations. Besides, without a job, most of us are screwed. Still, for the politicians, the game is about power and they would not do what the corporate bosses wanted if the voters really wanted a different path.
Having worked on several presidential campaigns, I've seen how they are run from the inside. I even tried to get a (future) President interested in solar power back when, only to run into a wall put up by the nuclear power guys. That wall crumbled after TMI, but now it's being rebuilt, IMHO...
E. Swanson
I am in complete agreement with you as far as attacking the overpop problem from the side of managing reduction (through family planning, of course and not forced attrition) and not assuming a growing head count. If for no other reason than to buy time for the more exotic and ego satisfying solutions to come to fruition, if at all.........
Now, as far as how to get people to be more conservative etc. All organisisms will always take "the path of least resistance". This observation is axiomatic and immutable so we must assume it will always hold in any new arrangements.
Our current spacial order is designed around a mode of transportation that allowed for a much more sprawled geography than transportation based on human power alone can provide. Don't expect anyone to be "talked into" using a bike to travel 5 miles to procure a gallon of milk when they can just hop into the family truckster and be back in a flash without even breaking a sweat.
No, this is about the patterns that people will establish based on the environment they live in and that environment is too spread out to do much more than improve the efficiency of the current transportation modes.
There is a lot of room to trim the fat for sure but I just don't see a replacing of fuel powered transportation until a more compact geography makes it feasible.
So I guess we need to plan our cities and towns differently or more like the good old days.
In the mean time keep working on those better condoms!
I really think you're ignoring the fact that very rarely, if ever, do humans voluntarily limit their birth rate.
And I pose the question, if we have the energy and resources to grow in balance, why not? Why degenerate into an eventually doomed race limiting itself to one planet, if we can build cities in Langrange points, moon bases, terraform Mars, Niven rings, and eventually Dyson Spheres.
Sure there will be mistakes, but to do it long term, we will have to learn and incorporate deeper knowledge of ecological systems, and perhaps adapt somewhat to meet the large goals. But the future is NOT entirely calculated out, as Malthus proved, and no models have incorporated all the (currently unknownw) new ideas and new technologies into their calculations.
Might as well give up using fire.
Huh? What are you talking about? What do mean, "deep denial?" Mr. Henson's achievements and accomplishments are applauded around the world, and what have you done to improve the human condition?
|Don't complain about your intellectual and moral superiors just because you're jealous or have some other emotional or ideological issues. Mr. Henson's insites are considered by science and technology advocates around the world as roughly equal to the likes of A. C. Clarke and Azimov, so you'll have to explain what your difficulty is with Mr. Henson's achievments.
Would only be fair. }:-}
As it stands, let's hope thyat such technologies become a reality, a means of restoring some ecological infrastructure while retaining the world's admittedly shakey quality of life.
Thanks for posting this link to your background. Looking thru it, I'm certainly impressed by your experience, however, what you write does not prove the feasibility of the SBSP as you have described them. BTW, my first job after college involved working with analog computers on some satellite attitude control problems...
E. Swanson
"what you write does not prove the feasibility of the SBSP as you have described them."
I hardly described them at all. SBSP is an obvious winner *if* you can get the cost to GEO down low enough. That's what I have been trying to do. In retrospect, it involves matching the exhaust velocity to the mission velocity to get the mass ratio down. I.e., two stage to GEO with most of the delta V in the second stage using 10,000 m/sec exhaust velocity.
"involved working with analog computers on some satellite attitude control problems"
Cool! My first patent (long expired) was the log-antilog four quadrant multiplier. I have recently proposed using tethers for attitude control of power satellites. That's probably too technical to discuss here, but ask (hkhenson@rogers.com) and I will send you what I have. It needs more thinking, especially what happens when a fast moving rock cuts a bridal line on the transmitter disk and how to keep the whole thing from turning over around the axis of the tether.
SBSP is an obvious winner *if* you can get the cost to GEO down low enough.
Magically free? Come now - the last times the Space Power has come up I've pointed out how present land based PV cells are almost as good at getting the energy of photons to elecromotive force as the photons in space -> downshifted to Earth -> converted to electomotive force.
And on earth - repairs can get made.
Another claims 1/6 the energy of PV
http://www.vnunet.com/business-green/analysis/2202907/space-solar-power-...
http://www.theoildrum.com/node/5306#comment-494573
I asked for someone to offer up a refudiation of the 1/6 to 2x power claims. Perhaps you can?
It depends on a lot of other factors.
Roughly speaking, a system in GEO is about 4-5x more power per GWp than that system on earth (3x longer exposure + 1.5x higher energy density). Transmission efficiency is a huge unknown, but let's optimistically estimate 67%, for a total "orbital improvement factor" of 3x: the same system will generate 3x as much power in orbit as on earth, so an earth-based system that generated as much power would cost 3x as much.
If a 1kW satellite costs $600, then, a 1kW ground-based system would cost at most $1800, and probably a significant amount less (as it would likely have simpler requirements than a satellite). So the question becomes what the launch, construction, maintenance, and rectenna costs are; if they're anywhere near $1200/kW, the ground-based system is cheaper.
You're assuming 5kg/kW, or 1/200 tons; with 12 tons per flight and 200 flights per $450m ship, that's $450M / 200 flights = $2.25M/flight / 12 tons = $188,000 per ton / 200 = $938 per 5kg kW in ship costs without even considering fuel, operations, or maintenance. Your cost is already up to 85% of a ground-based system without considering more than two aspects of the space-based installation!
***
Basically, the key to your system is assuming super-cheap solar power; $600/kW from space is ~$1,800/kW on the ground, which is roughly the cost of a coal-fired system but without fuel or maintenance. That's about $600/kWp, which is roughly 5-10x cheaper than current solar power systems. Given your assumptions, the launch system is irrelevant - you could just take exactly the same technology and make a ground-based system that did the same thing but cost less.
"You're assuming 5kg/kW, or 1/200 tons; with 12 tons per flight and 200 flights per $450m ship, that's $450M / 200 flights = $2.25M/flight / 12 tons = $188,000 per ton / 200 = $938 per 5kg kW in ship costs without even considering fuel, operations, or maintenance. Your cost is already up to 85% of a ground-based system without considering more than two aspects of the space-based installation!"
You missed the main point. The first kg up cost ~$750/kg. But the cost of the Skylons comes down by 2/3rd, the life goes up reducing the cost by 2/5th and the amount go GEO goes up from 6 tons to 25 as more lasers take over more of the delta V.
The net effect is 1/15, which lowers the cost to $50/kg.
Power sat energy is fed into making fuel, so the only cost is the capital equipment.
I thought the point of the exercise was to find a way for renewable energy to cost-effectively replace fossil fuels? Given that, why insist on a demonstrably-more-expensive approach?
Given your assumptions, a ground-based system is cheaper; why insist on the space-based one, with all its unknowns and critical assumptions, unless your intent is "cool stuff in space" rather than "affordable renewable energy"?
The basic fact that you have to contend with is that you're proposing something enormously more complex than a ground-based installation, yet you're making the assumption that solar generation is extremely cheap. That means you have a fairly narrow range from which to pay for this additional complexity before simply installing solar generators on the ground is cheaper, and once all the costs you're ignoring are taken into account, your proposal does not appear to be in that range.
That's an enormous chain of advances that have to go according to plan in order for your system to work. What if there are cost over-runs on building the spacecraft? What if costs don't fall as much as you hope? What if lifetime extension requires extensive maintenance? What if these things actually cost money to maintain and operate?
Moreover, you're ignoring an enormous number of details - practically all of them, in fact. Enough that it's not really possible to evaluate your proposal, unfortunately. How can we take seriously a proposal that has spacecraft flying twice daily but doesn't allocate a penny towards operating or maintaining those spacecraft? Or towards acquiring/creating fuel? Or towards ground station costs?
Of course your proposal looks cheap - you're ignoring almost all of the costs!
Then why is there no capital cost entry for fuel synthesis plants? High-temperature electrolysis and LOH/LOX storage aren't free.
Moreover, ignoring operations and maintenance expenses for fuel synthesis, not to mention spacecraft that fly twice a day, seems...unrealistically optimistic. Suggesting that the only costs in existence are fuel and capital doesn't engender confidence in the thoroughness of the analysis.
There are too many details and too many numbers missing from your analysis. All we can conclude from it is (a) you're making a huge number of assumptions, and (b) ground-based installations would probably be cheaper and certainly have vastly lower startup costs.
The launch system Keith describes is well beyond what could be proposed and built in an SSP business case today. Skylon's SABRE engine and push-pull lasers are over the edge of feasibility. Lasers, for example, are blocked by clouds. Another major reason is that no mass market exists to support the existence of such launch to orbit vehicles. That is why Keith's budget numbers are somewhat incoherent. As another student of SSP (I contend there are no SSP experts,.. yet), I would disagree with Keith's massive use of astronauts to bolt these together - telerobotics are a thousand times more cost effective for any task stream - since they can be operated from the ground.
In my humble opinion we desperately need to have Congress charter an SSP company - just as they chartered Comsat - and see what the companies propose. There would likely be a dozen serious bidders and none of the bids need be accepted, and we would certainly learn a great deal about what in fact could be done.
"Lasers, for example, are blocked by clouds."
Beyond the first few years you don't have to have the lasers on the ground. Putting them in GEO complicates the military problem though.
"Another major reason is that no mass market exists to support the existence of such launch to orbit vehicles."
Well, duh. This *is* the mass market.
"budget numbers are somewhat incoherent"
The Skylon/laser combination came together May 17, which is less than a month ago. If anyone wants to work on the spread sheet, just ask for a copy.
"disagree with Keith's massive use of astronauts"
They wouldn't be astronauts. Iron workers maybe or whatever the Chinese term is. I am not opposed to telerobotics. If it works better, use it. I just can't get a dollar number on it, and I can on workers.
"have Congress charter an SSP company"
Darel and I have discussed this quite a bit. As someone else said in these comments, a lawsuit would stop the whole thing if it were done in the US.
"Then why is there no capital cost entry for fuel synthesis plants? High-temperature electrolysis and LOH/LOX storage aren't free."
Give me a number and I will put it in. I venture to say in the context of something this large the number will be small.
"not to mention spacecraft that fly twice a day, seems...unrealistically optimistic."
These things take off and land on runways. So do aircraft. Can you come up with a reason you can't fly one twice a day that doesn't also apply to aircraft?
"ground-based installations would probably be cheaper and certainly have vastly lower startup costs."
Ok. I have a startup cost of ~$60 billion and it replaces all the fossil fuel use in the world after a few decades. To get the US alone off fossil fuel and on solar would need ~2.5 TW. How much will that cost?
Want a reason? How about the fact that the Skylon vehicle must go thru reentry at the end of it's orbital flight. With the Space Shuttle, the heat shielding tiles must be carefully checked after each flight. What about the active heat shield which Skylon use to brake the craft during reentry? How long does that part of the vehicle last between overhauls? There are lots of unknowns in the design, the failure to solve any one of which would kill the concept.
The U.S. had a program to replace the shuttle using air breathing engines. The program was killed, last I heard, perhaps for good technical (not budgetary) reasons.
E. Swanson
Good links you found, but they don't support your argument that the craft would take more than a day or two to service and turn around. And even if it did, so what? All that does in increase the number of vehicles in inventory. The capital charges for keeping more in inventory are ~6 % of the value of one per year. If you fly one 100 times a year and they are good for 500 flights, that's 20% per year for wearing them out.
Years ago, when the company I worked with had a contract to work on the Boeing proposal for the ISS, we looked at automated detection of system failures. Along the way, we learned about the NASA Failure Mode and Effects Analysis efforts. The name rather describes the process, which was to sit around and try and think up what failures might occur during a mission and what the effects would be. In case of the Skylon system, what would be the effect of a loss of coolant in the Thermal Protection System? During the launch phase, a loss of coolant would result in a loss of the wing and a crash. Once in orbit, the craft could not be expected to survive reentry without that system, so the result of a loss of coolant would also likely be catastrophic (assuming the cooling were employed on reentry). The actual probability of such an event would not be known until a few vehicles had been lost.
Wanna bet that this system alone would be able to pass your rapid turnaround requirement?
E. Swanson
Sorry, I am the wrong person to get into the details of Skylon failures.
Reaction Engines makes a point of the vehicle having a viable abort mode throughout the flight. And to boot, cargo flights don't have to be human rated because they don't use pilots.
I just don't know enough detail about the Skylons to debate you on the topic. Maybe we could get someone from Reaction Engines to comment.
Loss of either wing (or both) with the engine(s) attached to the end would not present a "viable abort mode". I suspect that the Skylon vehicle would not return to land with one engine out, whatever the cause. It's that old stability in flight problem, you know. Haven't you learned to fly an aircraft?
E. Swanson
"would not return to land with one engine out"
"Abort capability: The vehicle is capable of flying
to and landing safely at strategically placed abort
sites with up to half its engines shutdown in a
similar manner to aircraft."
http://www.reactionengines.co.uk/downloads/JBIS_v57_22-32.pdf
"Haven't you learned to fly an aircraft?"
When I was 13.
As one with direct experience with aircraft, you probably understand lift-to-drag ratio and how that is related to aspect ratio. To achieve the greatest lift-to-drag ratio, the designer of a subsonic aircraft usually opts for long narrow wings, as seen in a typical glider. Commercial aircraft have such wings, which means that the lift to keep the craft aloft can be provided with minimum drag and thus minimum thrust. The wings on Skylon appear to be intended for supersonic speeds, being relatively short and wide. At subsonic speeds and low altitudes, the craft would require quite a bit of power to remain aloft, especially given that the full load of fuel and oxygen to power the craft during the rocket phase would still be aboard. The lack of sufficient power to overcome the drag would make level flight very difficult, if not impossible. Care to guess what the stall speed would be?
Also, the outboard position of the engines would result in a major yaw torque with either engine out and the vertical tail would need to be large enough to produce a torque at least as large in the opposite direction. Yes, I know that commercial transport craft with 2 engines are designed to fly with one engine out, but these designs have the engines located nearer the center of the craft, so the torque from drag on one dead engine and the torque from the still operating engine can be countered by the force of the vertical tail. I think the Skylon tail is too small to achieve this, especially at landing speeds where aerodynamic forces are at a minimum.
While the detailed description you presented speaks to pitch stability and the position of the wing CP and CG, there's no mention of yaw stability, which is most influenced by the fuselage and the tail. If the CG is near the front of the wing and the CP for the fuselage is at the usual quarter chord of an airfoil, the CP would be ahead of the CG, thus the vehicle would likely be unstable in yaw, even with both engines running. Again, the tail looks too small, IMHO...
E. Swanson
"Care to guess what the stall speed would be?"
No, because I don't like to guess and can't find it in the literature.
The takeoff speed is 155 m/sec, 347 mph. They have an interesting time stopping in the event of a rejected takeoff just short of rotation. To get rid of the heat without having many tons of brakes, they carry 1200 l of water. They do say that stopping one on landing is only 3.5% of an aborted takeoff. So it is going a lot slower than take off as well as being much lighter. I presume they land it under power, but probably not much power.
Although it doesn't have a lot of wing area, when empty, it's only about 50 t. Re the size of the tail, if you think it is too small, why don't you write them and ask? The contact email is on their web page.
That's rich. Most of the content of your original posting is based on unproven assumptions and other guestimates. Aren't you just being evasive to try to slide past a killer problem?
As for the potential to recover the Skylon craft after an engine failure during atmospheric boost, it's clear that the result could be a shutdown of the other engine and glide back to a landing. Since the fuel load for the rocket phase would still be on board, the mass at landing would be quite large, thus the stall speed would also be rather high, perhaps exceeding 275 mph, based on the speed you gave for takeoff. The result would not be the easy glide as seen in Shuttle landings and there would be no second chance...
E. Swanson
"unproven assumptions and other guestimates. Aren't you just being evasive to try to slide past a killer problem?"
No, the stall speed of a Skylon for various loadings is surely *known* from design calculations. I just could not find it. I don't mind estimating from physics when there has been little work on something, but I don't like stating something known when I can't back it up with a reference.
"Since the fuel load for the rocket phase would still be on board, the mass at landing would be quite large"
The brakes don't permit a full fuel load landing, it has to be dumped. A discussion of this is on the Reaction Engines web site. http://www.reactionengines.co.uk/downloads/JBIS_v57_22-32.pdf page 29.
I can't imagine that your concerns about asymmetric thrust from an engine being shut down have not been considered in great detail by the designers. The wings are short so the lever arm to an engine is not great, in fact, it looks to be less than you see on 2 engine passenger jets.
Henson wrote:
The quote you reference says this:
That quote says nothing about recovery from a catastrophic engine failure in the troposphere. At lower elevations, it's claimed that:
At lower altitudes, after a single engine failure or shutdown, it may not be possible to develop enough yaw torque with the vertical tail as shown in the graphic. Therefore, a tail the size of that on a 787 would be more appropriate, IMHO...
E. Swanson
"it may not be possible to develop enough yaw torque with the vertical tail as shown in the graphic. Therefore, a tail the size of that on a 787"
You may be right, though Reaction Engines' response indicates they have enough tail for yaw authority at low speeds. One thing that might make the difference is that it is going like a bat out of hell right off the runway. An engine failure short of rotation recovers using brakes.
I presume you are an AE. I am an EE and while I have wide experience outside that field, I don't know enough about aircraft control to argue the point.
"Maybe we could get someone from Reaction Engines to comment."
Mark Hempsell of Reaction Engines did. Here it is:
Skylon is the result of 25 years of work, dating back to the BAe HOTOL project. There is nothing in the baseline vehicle below TRL3 although there are a few "nice to have" like Expansion Deflection nozzles which we are working on that are below that. The current funded programme is aimed at taking everything on the engine to TRL 4-5 of which the ESA 1 million Euros is only a small part, most of the investment to date has been from private funding; in current dollars the total investment is approaching $100 million. The important point about the ESA money is that, although managed by ESA, it is UK Government money knowingly given, and there will be more.
It follows the development work we are currently doing is not laboratory scale proof of principle The main activity is the productionizing of the heat exchanger modules so we can make a full heat exchanger with frost control to test on our B9 facility. Our current plan (which will need some additional funding) is that within 3 years all the necessary technologies for the whole vehicle will be at, or very near, TRL5 and thus ready to make a decision on full development. I feel 2015 might be a little optimistic for start operations, our current programme says 2020 but I believe a couple of years might be able to taken out of that programme say 2018.
Abort Options: Skylon has the ability to abort the mission throughout the whole of the flight regime including one engine loss abort (depending on the nature of the engine loss). There are a few special tricks that increase the resiliency such as using the spill duct burners alone in a supersonic cruise, it is also worth remembering that the remaining working engine has considerable control authority in pitch and yaw we are not relying on the aerodynamic surfaces alone. Aborts have been looked at independently by two teams and the only point of contention is whether there is a gap between "turn and return" options and "once round" options which might introduce a requirement for a downrange landing site.
Reliability: There is no compromise on the reliability in automated flights partly because of the value of the Skylon vehicle and partly because the automatic flights are part of the on going certification of the crewed flights. It should also be noted we have assumed a certification route to safety and not a man rating route (the difference being in one you certify the vehicle in the other you certify the crew). On entry into service the mission loss rate will be better than 1/1,000 and vehicle loss 1/10,000, but as with most parameters if it were being run in an operation as large as SPS these figured would be much better (simple Weibull).
Wing and Control surface sizing: The C1 configuration has under gone wind tunnel testing up to Mach 12 and some basic CFD over the entire flight regime. We are confident it has lift and control over all flight regimes. It helps to remember on the way back that the main fuselage is basically a hydrogen airship which means our instincts, based on normal aircraft, as to what looks right is wrong.
Thermal control: the lower ballistic coefficient means the temperatures during re-entry are much lower than the Shuttle and we do not need ceramic tiles (and the original Shuttle concept with integral propellants tanks also did not have the tiles they were a result of the move to an external drop tank). The Skylon aeroshell is a proven and available reinforced glass ceramic material (which is why Skylon is black). There are two areas of active thermal control, one around the canard root and the other on the wing where the shock/shock interaction occurs and, yes, if they fail during re-entry we will loose the vehicle.
Flight Rate: if the space port is equatorial then launch windows to any LEO facility occur roughly once every 90 minutes and a single runway spaceport could easily launch a Skylon at every opportunity. Any particular Skylon vehicle could manage a flight every 2 days but it might be possible to bring that down. The development test programme for the Skylon proves the vehicle for a 200 flight lifetime but in mature operation that could probably be extended.
Atmospheric Pollution. There is a few small amount of nitrous oxides produced during the airbreathing stage and some damage to the ozone layer as Skylon flies through it (mostly from the exhaust water). But Skylon is though the layer in a matter of a few seconds if a problem can be minimized by altering the trajectory with some loss of payload. These would need to be assessed in any environmental impact analysis but even with the flight levels needed for an SPS programme it is low compared with current civil aviation.
Passenger Capability: A passenger module that can carry between 20-30 passengers would be a part of the Skylon development programme and would cost around $150 million each. The average cost per passenger we estimate to be around $1 million but with the traffic levels needed by an SPS programme the cost would be much lower – maybe as low as $100,000 per person.
"if the space port is equatorial then launch windows to any LEO facility occur roughly once every 90 minutes and a single runway spaceport could easily launch a Skylon at every opportunity."
Adding a bit, for the geometry in Figure 5, where the goal is to reach a GEO production facility instead of LEO, the launch window is away open. Eight takeoffs and landing an hour is far below the flight rate of major airports and would support a cargo rate of 100 t/hr. Without more lasers in space or on the ground at a different location, the laser stage has to go around the transfer orbit 1 and 1/2 times. With 1.6/14 x 8 GW in space, a laser stage can be circularized on the first opportunity. Between that and draining the Van Allen belt, passenger traffic to GEO would be safe and fast (5 hrs).
Wait, you're making cost claims on the basis that anything you can't find a number for is free? How is that even remotely reasonable?
Your proposal only looks cheap because you're ignoring almost all cost sources.
Are you serious? How about the obvious: exceeding Mach 5.5 en route to rocket-assisted orbit.
If you insist on comparing to airplanes, the closes comparison is high-speed, high-altitude spy planes. From what I've heard, the Blackbird required much more maintenance than the lower-speed, lower-altitude 747; why do you suggest that a vehicle which goes faster and higher than a Blackbird would have maintenance requirements more similar to a slow and low commercial aircraft?
This craft is going to have far higher thermal and atmospheric stresses than a commercial aircraft, and that's not even considering the stresses associated with the rocket engine (hydrogen embrittlement, etc.). If you're assuming the craft will require no more maintenance than a commercial aircraft, your assumptions are not reasonable.
Sometimes as here Pitt gets to the pith and more than compensates for the muddles he manages in some of his other posts.
Since the late 1950's, following encounters with writers such as N. J Berrill and Charles Galton Darwin -and later Garrett Hardin - I have suspected that there might be a population overshoot followed by a dieoff. This prompted me to become active in organizations such as The Population Reference Bureau, Planned Parenthood and eventually Zero Population Growth. At no time did I WANT to see a dieoff. The following is an excerpt from The Tragedy of the Commons,
"A finite world can support only a finite population; therefore, population growth must eventually equal zero. (The case of perpetual wide fluctuations above and below zero is a trivial variant that need not be discussed.) When this condition is met, what will be the situation of mankind? Specifically, can Bentham's goal of "the greatest good for the greatest number" be realized?"
Did Garrett Hardin want a dieoff? Did Georgescu-Roegen, L.F. Ivanhoe and most of the other other authors cited at http://www.dieoff.org want a dieoff. Granted you can probably find someone somewhere who wants a dieoff. Nevertheless I believe that the following claim is disgusting and warrants modification - perhaps even an apology.
"Of course lots of people seem to *want* low energy world, including a population die back to one or two billion people."
At no time did I WANT to see a dieoff.
And there is a difference between "wanting" and pointing out this is the most likely fate of Man.
If anyone WANTS a population reduction they can take something like UG99 and go from cropland to cropland in the various nations spreading it. A more expensive and higher level of training would be buying the DNA 'printers' and making (or remaking) a virus. Posting on the Internet "I want a population reduction" isn't really effective for the reduction action plan.
Hiding behind the distinction between wanting die-off versus expecting die-off, there's a more important point failing to be mentioned.
Supposing Keith gets this vast energy supply fully working. Result paradise? I doubt it. More likely people dump their Hummers for personal heli-Hummers, and the world population jerks up to 12bn. And the ecosphere gets utterly trashed in consequence. If there are any survivors they survive on a planet devoid of trees and fish, let alone happiness. So, near-term die-off is probably the least worst option anyway.