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Extraction of volatiles. Lunar soil heated to 1300 K releases 0.1% by weight of the following trapped volatiles: CO, CO2, N2, H2, H2O, SO2, H2S, CH4, and inert gases (He, Ar, Ne, Kr, Xe). As much as 0.5-1.5% by weight may be released upon heating to 1700 K (Phinney et al., 1977).
This is from NASA's 1980 Advanced Automation for Space Missions study, which proposes self-replicating robot factories for Luna development.
How much energy does it take to heat 1 kg of dirt to 1700 K?
If you do it with sunlight the exact amounts needed are not relevant because the equipment is very cheap and the heating occurs essentially for free.
On Earth, low cost mirrors can achieve 2000 F pretty easily. Remove the atmosphere that diffuses the insolation and higher temperatures are possible.
The Hubble huggers are building a case for STS to fly a repair mission by making Hubble relevant to the VSE.
Not that I have any problem with that.
Several years ago, either at New Mars or its predecessor board we were discussing what skills would be useful for the first long term team to visit Mars (or the moon).
Back then, I insisted we need a chemist. A versatile, broadly experienced chemist.
I stand by that opinion.
Where are you going to get the nitrogen from?
(a) The technology needed to make the alon powder may be beyond lunar application; but
(b) if (a) is solved then note that the chemical formula for alon is something like 23 Al + 32 O + 4 N. By mass, the nitrogen is a tiny, tiny, tiny fraction of the whole thing.
Where do we get the nitrogen? From a tank - shipped from Earth.
Silicon, aluminum, oxygen and nitrogen! Si-Al-O-N Time to google on how to make this stuff. Lunar alon would be way better than fiberglass.
Maybe President Bush was right after all. We can build spaceships on the Moon. 8)
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ALON looks perfect for spacecraft portholes and helmet visors.
Given the amount of methane and the mass of the equipment needed to convert it to plastics, it would be simpler to just skip it and send tanks of two-part epoxy instead. I'd suggest just sending rolls of prefabricated fiberglass cloth at first, too - save the smelters for later. And as for vacuum vapor deposition, I'd skip that, too - it requires a carrier gas, which would also have to be manufactured or shipped in. VVD and fuel-to-epoxy conversion are unnecessary. IMHO, garden variety sintering is just fine for lunar fibrglass.
A Mars mission wouldn't have the same conditions, though, and all the raw materials needed to make epoxy (or some other resin) are already there right along with the silica and magnesium needed to make fiberglass. There, conventional resins make more sense than VVD and sintering.
Sending equipment for ISRU fiberglass production is a workable proposition for both Mars and the moon, as long as we don't send the same equipment to both places.
Do two part expoxies outgas anything useful?
I wouldn't even begin to bother powering Lunar equipment with imported Methane or Hydrogen without recycling every bit of it, its far too precious to just dump.
I agree. Pretty much everything is too precious to just dump.
My argument for imported methane / H2 works only if every drop of exhaust (H2O & CO2) is captured and recycled.
Methane boy wishes to remind everyone that CH4 includes carbon.
Methane / LOX rovers and back up generators allow carbon imports to do double duty since importing inert carbon is simply an expense.
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As for water, one landing of the proposed VSE LSAM cargo version can bring about 20 MT of liquid hydrogen which will yield 180 MT of water if combusted with lunar LOX. In the beginning, why will any base need more than 180 MT of water?
As for carbon, one landing of the proposed VSE LSAM can deliver about 20 MT of CH4 which will yield 15 MT of carbon (& 30 MT of water) which equals 35 MT of CO or 55 MT of CO2. 20 MT of CH4 plus lunar LOX will run rovers and emergency Honda power generators for a long time, and give a small base plenty of carbon.
I assert it will be far cheaper to import methane and extract LOX than dig water out of cold traps and crack into H2 & O2 (let alone process out the impurities)
At $30000/lb? If I can send a 2 ton machine that can extract 1000 tons of water, I've got a pretty big win.
Is the existence of lunar ice confirmed? I thought there was still some controversy.
$30,000/lb? Proton is $1000 per pound to LEO today.
Besides, how do you supply power to that machine?
Is there any lunar hydrogen that is recoverable? As far as I know, it's not confirmed yet.
Cause that will end up being a hell of a lot of methane, repeatedly. Verses a reactor in one shot.
Its interesting that for all the talk of microwave solar power plants, no one has thought to set up a power source on high ground and beam the power down to all the things need it in its line of sight. Might not be all that great for long range explorers early on but it will be great for powering all the rovers bringing regolith to a LOX plant.
Hydrogen is the one missing link. Carbon was found in Apollo samples though in low consetrations, be there are probably denser consentrations.
Methane solves the hydrogen missing link. And the carbon missing link. The Moon lacks both elements.
Once methane is combusted into CO2 and H2O then we can crack the H2O (exactly as is proposed for mining the cold traps for lunar ice) and then we use the Sabatier process to reform methane from the H2 and CO2.
Is it easier to extract water or ship methane? Depends on how much power is needed to dig out the water, purify it of sediments, and crack into H2 & O2 in the first place.
My main point is that the need for a nuclear plant should not be a mission critical FIRST step, necessary before we can do anything else.
Useful? Yes. But not necessary. [Edit to add: This is a big advantage the Moon has over Mars, abundant insolation. Utilize in situ energy as well as materials]
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Methane gives you carbon as well as hydrogen and can be used to store solar energy by converting CO2 and H2 via the Sabatier process, something we need to practice for Mars anyway.
Test your Mars Sabatier gear on the Moon by making fuel for rovers.
One VSE LSAM redesigned to carry cargo only could deliver the hardware and the CO2 can be harvested from the exhaust of a methane / LOX surface rover.
I doubt the rovers will be (any)gas powered. Most likely solar, with precharged batteries.
Why? Especially if a lunar LOX plant has been built.
Import methane and receive a four-fer;
Power
Water
carbon dioxide
cabon monoxide (for Mond process)
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Or, import large numbers of solar cells and/or a nuclear power plant.
Which will be "lighter" and cheaper?
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I assert it will be far cheaper to import methane and extract LOX than dig water out of cold traps and crack into H2 & O2 (let alone process out the impurities)
A Honda power generator (a $1000 item) running methane / LOX will spew what is nearly distilled water from the tailpipe.
Lunar night?
Couldn't you heat rocks with passive solar during the 14 days of sunlight and extract the heat during the lunar night to run your heat engines?
Efficient? No! But how mucn would it cost to send 10 square meters of mylar (or 100 sq meters) and inflatable frame?
If there are going to be vast quantities of solar cells built, it would be awfully hard to import large quantities of dopant economically I mean... nor does the author make too big of effort to explain the dual-layer nature of silicon cells.
Since imported mass is a huge limiting factor, I believe a good solar alternative would be Stirling cycle engines that use supercritical CO2 as the working fluid (Argonne Nat'l Lab has done some work on supercrit CO2 turbines); deploys the "cold end" of the Stirling cycle engine in shaded regolith; and the "hot end" at the focal point of multiple inflatable mirrors.
Austin Stanley has pointed out the amount of solar energy that can be concentrated with a few hundred (or thousand) dollars of very light weight material.
One VSE LSAM redesigned to carry cargo only could deliver the hardware and the CO2 can be harvested from the exhaust of a methane / LOX surface rover.
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Add a "for example" link: supercritical CO2 cycles for advanced nuclear power.
This link is for Brayton cycle but should work with just about any heat engine, the key being 2000 F plus temperatures coming from solar energy concentrated by commerical grade mylar mirrors.
But a power grid of solar panels would solve this problem and work could continue.
Of course.
My question is whether such things (nuclear reactors, Luna circling power grids) are a necessary condition BEFORE we start doing useful (profitable) work on the Moon. Personally, I hope to see lots and lots of nuke plants and a huge power grid sooner rather than later.
But, must we postpone commercial plans until that happens?
And what ahppens when you are in Lunar night (which you will be almost beyond doubt) at your mining site, Bill?
Mining free-floating asteroids that haven't crashed on the Moon is basically impossible thanks to the lack of gravity. It really does make all the diference in the world.
I'm gonna laugh when Roberts' silly rocket peitons bounce off the rock too often to make them reliable.
To be clear, nuclear reactors would be nice. But lacking reactors, nickel can be digested and vapor deposited on a 14 days on and 14 days off schedule.
Rest and perform facility maintenance during the lunar night.
I just want one good nuclear reactor on the moon--and you will have the power for a foundry.
For a foundry you dont need a reactor, sunlight focused through mirrors would be enough but for initial bases then yes a reactor to provide the power to the base is essential when it goes dark.
Find a large enough chunk of nickel-iron asteroid and you don't really need a foundry. Digest the metallic nickel with CO (carbonyl) and deposit it via nickel vapor deposition. Heat the mandrels with sunlight to induce the nickel carbonyl gas to let go of the nickel and you can make pretty much anything out of pure metallic nickel.
No nuclear plant necessary.
As for platinum revenue, nope its not enough to sustain a cis-lunar economy. Not even close.
In 2004, the entire world produced about $6 billion worth of platinum, half of that imported by China which has ZERO native platinum reserves.
Now, if China wanted to leverage lunar platinum to assist with the prestige of a lunar base, they begin with a $3 billion platinum import defict which can be used to partially offset a space program.
Anyway, my plan is for TV rights to pay for the EML-1 station and development of a re-useable EML-1 to Luna landing module. Then follow on mission are paid for with TV rights for the 1st Japanese, 1st Indonesian, 1st Mexican etc. . plus alumni donations for the 1st grad of Middle State Poly-Tech to walk on the Moon.
At Proton / Soyuz prices ($100 million per Soyuz + Proton) plus shipping some methane/kerosene and LOX, even places like Singapore might be able to sell TV rights for $200-$300 million for coverage of a native son or daughter walking on the Moon. Tourism offers more revenue.
Next, mint lunar platinum coins. The very first coins ever made with metals mined off of the Earth. 500 years from now, those will be extraordinarily valuable. Sell them today at a premium to artificially inflate the price of the first lunar platinum returned to the Earth.
Okay, that will run out before too long.
Harley Davidson makes more money on merchandize than they do selling motorcycles. So, as you are mining platinum (maybe at a loss) market the heck out of your company and brand consumer goods.
Buy our shoes, shirts and show your support for opening the lunar frontier. Can't be done? Study Nike. They spend $2 billion per year on endorsement contracts. If my company has begun mining lunar platinum, I can sell shirts, shoes, pants, whatever.
Genuine lunar nickel bathroom fixtures? The nickel is "free" since I cannot completely refine out the platinum on the Moon and the nickel needs to come back to Earth anyway.
Now by doing this in a fictional context, perhaps I can create a basis for discussion and provoke some "out of the box" thinking.
Looking for a lunar landing using as much off the shelf stuff as possible. If Russia had an HLLV, then no need for so much on orbit assembly. A plan based on re-starting Energia lines is an option, of course but then its less off the shelf. if we are talking about re-opening production lines. Rather like modular EELV versus shuttle derived HLLV.
Well, that's why I never liked O'Keefe's plan with the EELVs. It would have been tremendously expensive and risky. Griffin is right with the Shuttle derived HLLV.
Uh oh!
First time ever I accidentally abused my moderator super powers. I hit edit not quote.
Sorry. :oops:
Anyway, I agree about EELV.
Is this the whole thing except for the movie?
Brazilian Astronaut, Marcus Pontes To Travel To ISS In March 2006
Yes, and the Indonesian government has recently signed a deal for the delivery of Russian made Suchoi jet fighters. This includes a trip for that country's first astronaut to the ISS.
Three Blocks D should do the trick, alright. But, wow, that's an awful lot of automatic docking. Pretty risky stuff! None of this has ever been tested. Your plan sounds extremely complicated.
By the way, why do you insist on Methane LOX. NASA will use it for their CEV, because they have plans for insitu propellent production on Mars. The Russians have a lot of experience with Kerosine which has almost the same isp as cryogenic methane and it's much easier to store. And don't forget, your LEM will have to be replaced regularly, especially if you plan to use LOX tanks.
Just some thoughts
Looking for a lunar landing using as much off the shelf stuff as possible. If Russia had an HLLV, then no need for so much on orbit assembly. A plan based on re-starting Energia lines is an option, of course but then its less off the shelf. if we are talking about re-opening production lines. Rather like modular EELV versus shuttle derived HLLV.
Gateway is all that needs multiple Block D assembly. Thereafter its one Soyuz / Shenzou (or Kliper or t/Space CVX or CEV) and a propulsion stage to get to L1.
Kerosene is an excellent point. Thanks.
As for the lander, the idea is to swap out the LOX tanks with new ones filled on the lunar surface. Robotic LOX plants are dropped using the same chassis and engines as the new landing module.
RL-10s are good for a great many firings, my google reading suggests. Besides sending new engines to EML-1 isn't a huge deal if the landing module is designed to allow engine removal and replacement using the Canadarm and Dextre at EML-1.
(Heh! Then ask Bigelow for an inflatable space garage.)
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Disclosure time. This is the backbone of an almost finished novel.
I hope to provide scenarios or a platform to discuss lunar development issues in a concrete if fictional setting.
After the initial tourism thing dies down, hunting lunar platinum (Dennis Wingo's theory) is the next item on the explorers' agenda.
Sorry, I forgot your Gateway construction questions.
Budget 1 Proton to lift the FGB-2 & budget 2 more to push to EML-1. That's why I specify 9 Proton.
If I need 3 Block D, no big deal, right? One Block D might be enough for a docking module to connect to the FGB-2 and TransHab.
Radiation protection? The Transhab can be made with boron doped polyethylene (& Kevlar) with a central core storm shelter and methane tanks can be stockpiled around the facility.
Standardized tanks are new. No question. But it is either that or cryogenic fuel pumping. I prefer to design a standardized tank.
That re-useable landing module is the biggest new piece of hardware. I envision an oversized LEM with landing legs that do not come off. Methane / LOX is better than the Apollo hypergolics and methane stores way better than LH2. Same engines (RL-10 class) perform the descent and ascent functions.
Has the patent expired on the original basic RL-10 yet?
More fuel will be needed to return to EML-1 bringing the whole vessel but once lunar LOX comes on-line the long term savings will be enormous.
But up to now they haven't even got a single space tourist for the circumlunar trip with Space Adventures.
They are selling to the wrong market. Few will care about a billionaire joyrider.
But, how much would the Brazilian television networks pay (collectively) to broadcast live coverage of the first Brazilian to set foot on the Moon?
India?
Japan?
Korea?
U.K.?
Germany?
Canada?
Once Brazil does it, challenge Argentina to raise the television money to send one of their citizens. Incremental cost is a Soyuz + Block D plus some LOX / methane delivered to EML-1. $500 million covers the incremental costs easily. Japanese TV could recoup $500 million quite handily by selling advertising during the coverage of the 1st Japanese citizen to set foot on the Moon. More people would watch that than the Olympics, IMHO.
Then what?
Well, why are we going to the Moon in the first place?
More answers:
FGB-1 was launched via Proton and is now part of ISS.
Re-fueling? I'd suggest standardized tanks of LOX and methane for the re-useable lander. Use a plug-n-play format. No zero gee fuel transfers.
Soyuz + Block DM can do a lunar fly-by from EML-1 or fly direct to Earth. Depends on the math. The upper stage will needs a few weeks (a month?) deep space shelf life.
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Once there were vague plans to build a Proton pad in equatorial Brazil.
And what's the business model supposed to be? How do you want to make money? ... have space tourists pay 10 billion per launch?
Ten billion (back of envelope) deploys an EML-1 station and a re-useable lander to shuttle between EML-1 and the Moon.
Soyuz plus Proton Block DM gets 3 crew to EML-1 (variant of Space Adventures fly-by architecture) where they change trains to the re-useable lander. Sortie to Moon. Return to EML-1. Fly home on Soyuz.
Repeat as desired.
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Incremental costs per mission are
Soyuz + Proton
As many Proton as needed to get methane / LOX to EML1 to fuel the lander. If / when lunar LOX comes on-line use that.
Flight Control services
Let Elon Musk or whoever bid to deliver methane to EML-1 using Belbruno trajectories.
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Business model? Fly the first Brazilian to the moon. The first Indian. The first Japanese. The first Korean. The first Australian. etc. . .
Six day round trips will only be for the initial cable Bill, that additional cable would be layed to permit two simultainious transits (one up, one down) and support the mass of multiple elevator cars. Then, considering a dozen cars and three-day transits, that would give you a lift opportunity every twelve hours, round' the clock. The "six day" cable will only be the dirt construction path, the twin-rail cable will be the highway. Once the initial cable is in place, it will be quite easy to add additional cables, so the elevator will have the bennefit of radically decreasing the cost of bigger or even subsequent elevators... but a tether will not.
This is a good answer.
12 hour payload cycles probably can recoup the investment at $100/lb. But again, this also requires potentially staggering levels of demand. 30,000 pounds going up every 12 hours.
2 million pounds of mass per month, per elevator, with multiple elevators likely needed to fully achieve the economies of scale to get to $100/lb.
But yes this will change everything.
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Rather than flying tethers as an intermediate step, a lunar to EML-1 elevator would appear to be a good intermediate step.
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Next up, the geo-politics of all this.