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Point withdrawn.
ANTIcarrot.
How much hydrogen would have to be hauled around for that? Granted, hydrogen is useful for radiation shielding, and is an all around a handy element to have around.
Well, that's kinda the point for high ISP engines, you need less fuel for any given deltaV. Say your GCNR engine weighed 100 tons, and you had another hundred tons of fuel, and you wanted to go to mars (4kmps) your ship can weigh up to 1,250tons. Alternatively you could accelerate 200tons to 14kmps or 100 tons to 20kmps.
Such a ship would fulfil the US Air Force's Real World specification for a space-fighter. In other words, it could literally turn around in orbit. A little more than that and you can have proper dog fights in space. ![]()
You just need to overcome all the little technical details first.
ANTIcarrot.
Anyone remember this?

Yes, it's a 1985 vision of the journey to Mars; complete with three venus swing-by landers, two comm sats, two aeroplane probes and an unspecified number of hard-landers and penetrators. All put together at NASA's power-tower space station.
Launched on five Soviet G1s, six ESA Ariane VIIs, and twenty-eight uprated space shuttles; because as we all know, the shuttle turned out to be much cheaper than all the others. ![]()
It's computers incidentally use 64-bit parallel processing with 10MB of ROM, 30Mb of RAM, and, apparently, an early DVD drive. Mission administration provided by the UN Mars Exploration Authority
Why post this here? Why not?
It's all very silly! :laugh:
It's all from a book called the Mars One Crew Manual, which though dated does contain a little useful inforation, as well as a few very nice pullout maps. Also useful as a diplomacy tool. If you ever think another person is proposing a really stupid way to go to mars just remember this post. Whatever method they propose, it can't be worse than this one!
ANTIcarrot.
ISBN: 0-345-31881-1
As I understand it, the Shuttle was a 'clean slate' design. Would you really want to risk having the watchmakers screw up a next-generation HLLV in the same way? Would it not be better (and from a design PoV *safer*) to go with the existing plumber's design?
ANTIcarrot.
There's just that pesky little problem about radioactive exhaust...
Plus such a ship would be somewhat difficult to stick in a museum after it had reached the end of its operational life.
ANTIcarrot.
As for "Russians, Chinese or French deploy[ing] a nuclear thermal tug and undercut[ing] your price per pound for LaGrange rocket fuel delivery" dream on. The French (or the Europeans in general) don't have the political will to develop nuclear power in space. The Russians don't have the money. And the Chinese won't spend that kind of money for some time.
The chinese are more likely to use zond style capsules and send a couple of people on an Apollo 8 style trip round the moon. Something they could easily manage a few years from now. Rondavouzing a Zond and 1 or 2 soyuz size booster-stages should be well within their capacity by then. Ditto for russian docking technology.
In fact, secretly helping them do just that might be one of the smartest things NASA could at the moment. ![]()
ANTIcarrot.
Asteroid or Luna mining is practical IF it's still very expensive to ship things up from Earth, and there are already other industries in space or you intend to use te full capacity of such a venture in another project. This would be like building a concrete factory in the middle of nowhere (very unprofitable) in order to build a dam close by (more profitable than shipping it in from 'civilisation'.)
With a reduction of launch costs to $500/kg or so (or less!) solar power becomes practical. (How much do Americans pay per kW??) IF there are no severe technical problems with moving the power down to Earth. At present there are no known problems with that.
As to thinking outside the box... I fear that even if you cut off a skeptic's head and carried it outside it would keep it's eyes closed to avoid seeing anything that could upset it's carefully preserved opinions.
ANTIcarrot.
I still point out that on Earth we don't start a mining operation by towing the entire mountain to the suburbs of a major city, we mine it in place.
When we do start mining, we tend to build a small town (or the equivolent) on top of or very near to the mine shaft. Over the lifetime of that mineshaft we do tend to move small mountains of ore to other locations to refine it. It's also usually the case that much of the material in conventional mining is not needed or wanted. Moving the ore this way usually only costs a few $$$ per mile.
Moving an asteroid to GEO or L1 is just doing all in one go and using the only current practical way. It may in the future be practical to move von-neumman mines to the belt and send the results back with solar sails, but neither technology is proven yet. We can also use the vast majority of the asteroid's mass. Hence why not do it this way?
As to the shell/shotgun impact, it depends. If the pieces are less than 10-100m across they'll burn up in the atmosphere. If the 'rock shot' has enough time to expand, most of it will miss earth. 'Air burst nukes' may end up the easiest way to make subtle alterations to an asteroid.
In any case, this is what the mission seems to be for. Turning theory into practice. Though I would be curious how the monitor will cope with the explosion. Close enough for a good view and you risk being hit by debris.
ANTIcarrot.
Are there any applications for scram-jets IN the martian atmosphere? Can't think of any, but flying probes have been proposed before and silly questions sometimes have fun/useful answers.
ANTIcarrot.
ESA on the other hand, from what ive seen, is quite an efficient organisation.
As is Airbus, which was recently reported as pulling ahead of Boeing for the first time.
Remember, for the moment the EU has little political power, and while it can do little to help either organisation, it can do little to hinder them either.
ANTIcarrot.
America's system allows for its 50 States to behave as one entity if the circumstances demand it, which they commonly do, whereas Europe is really just a relatively loose association of countries, still far more interested in their own internal affairs than in a 'United States of Europe'.
Very true. The problem starts though when 'all the states working together' becomes 'all the states want a piece of the pie'. One of the bigger reasons (though not the only one) that NASA couldn't persue the CD-X/Y programme is because it would have involved giving all the money to one company and one state. This was completely unacceptable to everyone else, and so a very promising project was terminated.
Similarly in the early stages of the Eurofighter the Germans reasonably demanded a big share - and got the flight control software. Unfortunately they had no experience in that area and didn't do too well as a result. A couple of years later and things were reorganised according to capacity & experience (as done with Airbus) rather than by order of who would winge the loudest.
Since then both the EU & US are experimenting with new management policies. If the US manages to solve the problems of waste first - then great, and they could have a man on mars by 2020. If an ESA/RSA partnership does it first though, then all the money in the world won't help NASA keep up.
May the least incompetent organisation win. ![]()
ANTIcarrot.
Technically it is possible to build an apparent perpetual motion machine. That is to say, a machine that is gaining energy from a source which we cannot identify or masure. Some kind of quantum generator may run this way for instance. But somehow I doubt this gravity wheel is quite the same thing.
ANTIcarrot.
What about the impact of a loss of skills? In an optimised four person exploration crew, aren't they going to be rather screwed if they lose a quarter of their expertise?
What about landing and take-offs? If you need two crew and one spare for a safe take-off, then you're cutting it fine to go down to the surface.
Finally what about the psychology of the crew? In the past they've all died together. How would they cope with the loss when they're a few billion miles from the nearest human being, and thirty mm away from the lethal harshness of space?
It's all very well saying, people die, get on with it. And I agree to a large extent. But there are other trade offs to consider.
ANTIcarrot.
And how has NASA's infrastructure, skills, and preexsisting technology coped with the simple task of building something like Mir?
Not too well has it? Does anyone know how much Mir actually cost? I'd be willing to bet over it's entire lifespan from idea to burnup it cost less than the ISS has to date. Possibly less than ISS launch costs to date. ![]()
An ESA/RSA tag-team would be more than capable of giving NASA a run for it's money.
ANTIcarrot.
PS: Doesn't the RSA get 'lander' experience everytime a soyuz comes down? ![]()
Well Esa is to get bigger, both greece and luxemburg are to join.
So Esa will get a slightly bigger budget, but as it really is a cheap space organisation will it mean any big plans coming to fulfillment. Esa always tries to do space missions and research as cheap as possible it does not have Nasa's money. The smart-1 mission is example of a succesful mission, Why successful, It has shown how to use an Ion engine effectively, It is using its instruments already, its a success.
According to Bigalow:
US space valve: $100,000
EU space value: $5,000
Big budget doesn't count for much if you're paying 20 times the going rate. If the EU shops around, or buys Russian, they could still achieve more than NASA. Especially if it stops trying to carbon copy NASA. (Shuttle/Hermes etc) Or if it simple doesn't charge itself $10B to administer a $5B project - like NASA sometimes does.
ANTIcarrot.
But real live construction, like bolting/welding together Mg alloy trusses to make an airlock frame, or installing/replacing new contaminant sensors on the insides of Hab walls... not a chance.
NASA's Robonaut prototype is getting to the level of sophistication required to operate any human machinery. With improvements in control gloves & power/weight, and space rating, it could do almost anything a human could - within a few thousand km of the armchair at any rate. With a simple robot arm to grab ahold of hardpoints on the space craft, it could do many jobs easier than an astranaut floating free.
True this maymean sending people to Mars to stay in tin cans and operate the robots outside, but so what? Such people will be construction workers, not astranauts. If they want to go out and enjoy themselves they can do so one their own time. ![]()
ANTIcarrot.
Whoa, look at the photo's of that engine, looks like something out of the X-Prize contenders' sheds.
In otherwords Russia has levels of control and efficiency in thier budget that NASA and Congress can only dream of! Not all organisations use diamond tipped drill bits to mill wind-tunnel models out of solid lumps of advanced titanium alloy. ![]()
ANTIcarrot.
One of my main objections to the idea of an aerospace plane (for example) as this point in the proceedings is that it would require very considerabe time and money on developing new propulsion systems which either don't exist yet or are in their extreme infancy--and compared with BDB would deliver a tiny payload. The beauty of something like BDB is that it does not need vast R&D; it's just a good old fashioned fire-and-go rocket, writ large. To spend $40 or $50 billion development money on some other way of lifting very large payloads would seem pointless, a waste of money,
Agreed. Hence my rule of no shuttles! And the beauty of the prize system is that the aerospace companies will not thier engineers to waste *THEIR* prize money in the same way they allow them to waste government money.
So push things just a little more, to say 40,000 tons GLOW, and we must be approaching something like 1,100 or 1,200 tons in LEO for about $400/Kg.
Suppose you needed to put up 2000tons/month. How easy would it be to scale up production of such vehicles?
Consiquence of BDB:
If you're launching thousands of tons of steel alongside your cargo, then it might make sense to reuse that steel in SPS construction. Alternatively very big BDBs with good enough thermal properties could survive reentry completely intact to be recovered. Recasting the steel might work out cheeper than buying new. Do your launch costs take this kind of thing into account?
Where exactly is this vast demand for energy, that cannot be easily met by cheaper investments earth-side?
Car use. Either electric or hydrogen cars will mean massive increases in power consumption. Also a little known country called China is beginning to wake up, and it's citizens want the same level of luxury we have. Which means 4 times the consumption of the US once they've finished. Ditto for India.
Yes there are eath alternatives. But most alternatives are severely limited in expansion or location. They should *still* be built on general principle, but they won't solve the whole problem without a major breakthrough.
Nuclear I'm somewhat wary of, especially fission. The disposal is a BIG problem. The only solution (linked to massive particle accelerators) requires so much power that it can only be run by another power station. ![]()
ANTIcarrot.
JimM:
A bad idea. The trade-off does not sound worthwhile. <snip> Cheap can come awfully expensive in this business.
I thought one of the lessons from the shuttle was that not spending the money up front can screw you later on? The second sentence works both ways.
But in any case, in principle a reduced price/kg can be got simply by scaling up the BDB. You start modest and make 'em bigger as confidence (and demand) grows. No need to sepnd extra billions and wait years.
Maybe. BDBs may have practical upper limits on thier size and cost/kg that aren't immediately apparent. It's important to get the cost down before you start serious construction. Whatever system could best do that.
Enegry is in essence free to any energy company in any case.
Which would be the point: The moment they do this they stop being a bunch of kooks burning their money and become a real electricity company with an economical product they can sell. It's a matter of showmanship.
Lars_J:
I just don't see the energy market ever getting bad enough that it would make economic sense at current launch costs.
Perhaps you missed the bit where we talked about spending up to $40B bringing the costs down...
Another case of "build it and they will come" situation, I suppose,
You suppose wrong. This is a situation more like the C-5 Galaxy, the Super Guppy, or the Beluga transport aircraft. Each was built for a specific customer for a specific purpose. It's not 'build it and they will come' but 'build it because you already have a customer lined up who's specifically *asking* you to build it and has already given you a down payment'.
ANTIcarrot.
I wouldn't, for two main reasons:
Oh where's your sense of drama? Just think of all the constipated expressions on the Boeing and McDonnald Douglas executives as the prize was awarded to Bigalowe.
Actually I'd like the end product to launch at *less* than £500/kg. Of if $2B-$5B could get us that I'd prefer to spend $10B and get down to $300-400/kg.
A 500MW SPS could probably be built for $3-5B. It would be a neat trick if the company built this first and then never paid any electricity or heating/cooling bills again - ever!
ANTIcarrot.
I used $40B as that's a big enough sum to satisfy most peopel that it's doable. I don't think a well managed development would actually cost that.
Personally I'd run it as a competition: company to win gets $40B cash, plus whatever profits they can get out of the $500/kg. EG: If they manage to get it down to $250/kg they pocket the difference. Arrangement will last until the launch of 4 SPSs or 200,000tons, at which point contract will be changed. If launch company offers costs substantially lower than $500/kg an extended contract may be offered. And no damn shuttles!
Should be enough insentive there for a company (any company) to really want to get the costs down.
Your point about the channel tunnel is well made. However after the tunnel many companies woudl not want to take another such gamble, especially now. And oil companies would not want to be seen as rats deserting a sinking ship, least it affect their share prices. It's possible though.
But I imagine industry would be more agreeable with one or more governments standing by as garantors.
ANTIcarrot.
The thing is able to lift 10,000lbs payload.
Ah. My mistake. Though it wouldn't have happened if you weren't using those silly lb things.
Good. Although I don't think they need neccessarily be government built.
In stand-alone business plans I've asumed it would take $40B to develop a system that could launch at costs less than $500/kg. Add that to the cost and bring the sold electricity to 6c/kwh (as NASA does) and you need to spend a lot of money to break even. IIRC, at UK prices you'd need to spend $120B, build 4, and operate them for 24 SPS years before you broke even.
That's quite a lot of money for private business to raise on it's own.
ANTIcarrot.
Quote
>>3000 tons into LEO for the cost of one shuttle trip?
>Well, what can I say? I know Shuttle is expensive,
>but $1.8 billion per trip? Who's kidding who now?
£3M/10tons = $300/kg.
3000tons = 300 launches = $900M.
Current estimates for shuttle launches are hovering at just over $1B. Check you maths please, particularly if you're going to be condescending afterwards.
>>Under $1000/kg?
>$660/kg, actually.
So, as I said, under $1000/kg. And again, check your maths.
>But of course then you have to add profit, insurance (on the
> vehicle itself, not the other things), ground handling
> facilites, etc. So maybe you could sell at about twice
> $660/kg....
You said $3M per flight. At a vehicle cost of $150M and 100 flights costs rise to $450/kg. (But hey, if they're giving them away, why not just pick up half a dozen and screw insurance?) Ground handling is included by definition in the $3M per flight.
Profit need not be added at this stage. If a company makes a delivery to your door, they make a profit not on the delivery but what they are selling you. The delivery is done at cost.
There must be a more convincing reason for manned orbital spaceflight than popping up to take in the view. There must be a reason that will convince the government, the military, or business, to pay for the venture.
On this we agree. One possible solution to this would be government built SPS systems.
Mass: 50,000tons
Power generated at ground station: 5GW
Launch costs: $15B
Insurance costs: $7.5B
Construction cost*: $8B
Ground station: $2B
My last bill: 7p/kwh = 12c/kwh
Energy generated = 43.83 billion kwh
Income generated per SPS-year: $5.26B
Total income (ten years): $52.6B
*Construction cost based upon two Nimitz class aircraft which equate the mass but which are much more complex. Assume assembly of components in space that are prefabricated on earth.
So that's a good $15B 'profit' for one SPS system. If government built, no money need be borrowed, so no pesky investment. If 12c is too high a price (and it's at least in part a product of the current high exchange rate) sell it at a lower cost or sell it in other countries! If one country stops buying, aim at another! (Try 'moving' any other type of power station!)
There are profitable things you can do in space, and launch systems like the theoretical one you have described will be the thing that will make them practical. Once started, the market will already exist, and new launchers can be developed for it. After that it should be reasonably self sustaining.
Hence I find your view that no one would want a $300/kg launch system to be entirely unsubstantiated.
And one last point: Even if you are right JimM, and the first spaceline is sued out of existence, then the R&D costs will get completely written off before the new owners get ahold of it - which would lead to a knock on effect on launch costs. So if it happens it may well reduce the cost of launch rather than increase it.
ANTIcarrot.
I was aware that the Warsaw Treaty $75,000 limit was history
Of course you were. That must have been why you waited until after I brought the subject up, and Algol supplied the counter arguement, to say so.
Might I also note that the new agreement is apparently volontary, and international carriers can apparently still opt to limit their liability.
The victims only have to show that the airline was negligent in causing their injuries.
- Article
In other wards, a spaceline would ONLY have to pay out after a challanger style screw-up, just as I said at the start. What's more these rules apply to an industry which has 100 years of experience to say what is reasonable and what is not. A spaceline startup may will not be a 'common carrier' and will not have that experience. It will not be as easy to prove they must have known about a problem. And prove it the prosicuter must, beyond reasonable doubt.
(ANTIcarrot, on the basis of this example demonstration of your forensic skills you'd get slaughtered in a courtroom.)
Maybe, and I freely admit I should have read to the end of the article before posting. but at least I try and present proof and cite sources. You don't, and so I doubt if you'd get in at all.
The widow sues the carrier for failing to disclose that flying suborbital invalidates standard whole life policies.
I doubt that would win, as a person is responsable for their own life insurance. It's a contract between the millionare and the insurers, and his responsability to check anything risky before he/she does it. It's like if he went up into orbit, and then cut his own wrists. Even though he died whilst in their care they would not be held responsable for something the millionare did to invalidate their life insurance.
Depending on local law, the passenger may be required to prove they have travel-insurance, but that's about it.
Agree that providing single-trip life insurance is probably profitable, but it should be kept seperate from ticket price.
Even at direct operation cost ($3million/trip) only, they would not have any customers.
3000 tons into LEO for the cost of one shuttle trip? Under $1000/kg? Start up space-organisation for less than $50 million a year? Oh yes. Sure. No one would want one of those.
If insurance is available, strong contracts and waivers in exhange for insurance coverage should be easy enough to draft and thereby circumvent the liability issue entirely.
Strongly agree - and remember saying something similar at the start. ![]()
ANTIcarrot.
I'd agree about the 'narrow definition of profit' bit. SPS construction *would* be profitable, but building the first one would cost somewhere in the reigon of $75B. Building 4 would cost $120B total, and they would pay for themselves after 24 SPS-years of operation. With an average SPS life of ten years, the four of then would produce $80B profit. After that an SPS would cost $25B and generate roughly the same amount of gross profit.
So yes, it can be 'profitable', but the sums involved are way outside the range of current industry. The government could, with some commercial participation. And IMHO, it's a better way to spend money than $300B for mars, or $70B for Iraq, or $60B for the F22 for that matter. ![]()
ANTIcarrot.