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46  General Topics / News & Commentary / Strong Compressive Structures from CNTs on: February 14, 2005, 02:18:15 PM
I'm mildly skeptical about the idea of using carbon nanotubes to make strong compressive structures- particularly using tensegrity ideas.

In my experience tensegrity structures aren't used much (ok, this is a fair overstatement, space frames are used in a number of structures), but the problem with tensile cables is that they often tend to be quite flexible- particularly stretchy. Usually this flexibility often means that the structure flexes to failure, often with a buckling failure.

Besides, even for tensegrity structures you still need to provide a compressive member, and this member presumably isn't going to be nanotubes under compression. Even if you apply external nanotubes to prevent buckling, the compression of solids is typically the same or worse than their tensile force, and we already use compression plenty, so I don't see that this is going to be a big win. In fact tensegrity structures have internal stresses that mean that you need *more* compressive material than a similar purely compressive structure.

On the other hand; inflatable structures sound potentially interesting, and seem to be tensile-only structures. I can't off-hand see a limit for how big they can get...
47  General Topics / News & Commentary / The Next Step for Private Orbital Transport on: February 08, 2005, 02:34:00 PM
Quote from: publiusr
If you are in an actual Low Earth Orbit, docking with the space elevator will be impossible due to the speed of the orbit. You have to launch straight up to follow the ribbon,


You can't launch straight up because the coriolis effect due to the earths rotation pulls you westwards away from the elevator (in the earth/elevator frame of reference). You actually have to point eastwards quite noticeably to keep up with the elevator.
48  Achieving the Space Elevator / Science & Technology / 100 years from now is it possible..... on: January 30, 2005, 05:24:02 PM
Quote from: Bob Munck
Fair amount of energy to get it out of the lunar gravity well.

Under 1 kWh (if I haven't messed up my maths). Well under 20c per kg, even assuming expensive electricity.

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Better would be SEs on the backsides of Phobos and/or Deimos, sticking up out of Mars' gravity well far enough to throw stuff to Earth. Getting material up off of Deimos would be a snap.  A little solar-powered ion or MPD propulsion system could make course corrections over the entire duration of the long, slow trip to Earth, and free-flying momentum-exchange tethers could be used for capture.

That works too. It's not clear that that would be cheaper though, and it takes 9 months or so to ship.

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We'll want great amounts of mass at GEO for shielding, and no matter how cheap the SE makes it to get material from the Earth, rock that's already up there, almost anywhere in the solar system, will probably be cheaper.

Eventually...
49  Achieving the Space Elevator / Science & Technology / 100 years from now is it possible..... on: January 30, 2005, 12:16:07 PM
I'm sorry, perhaps I'm being slow, but why do you have to use an asteroid for the counterweight?

Couldn't you just lift some rock up the elevator ahead of time from the Earth and then do the slingshot trick with that?

It's actually fairly difficult to move stuff into earth orbit from elsewhere- you need rockets for that in nearly all cases.

I suppose you could also use lunar material raised up using a lunar beanstalk, that would work too, and is probably somewhat easier; although attaching it to the earth beanstalk might be "interesting".
50  General Topics / News & Commentary / The Next Step for Private Orbital Transport on: January 27, 2005, 04:06:36 PM
Quote from: Mumbles
So what is your solution to radiation at GEO station?  Build enough shielding?  Depend on super-conducting magnetic cages to protect you?

Yes, either works and works well. You need a fair amount of shielding- a meter or two. But because it is in orbit, you only have to carry it up the elevator once, and once there it doesn't take away from the capacity of a beanstalk.
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You seem to know the Van Allen belt profile better than me, so I would ask "what is the level of radiation at R-geo?"  (Might be a subject for a new thread, here or somewhere else - GEO station radiation hardening/protection requirements.)

It's just at the upper edge of the Van Allen belt. In fact, quite a bit of the time it's outside it- IRC the sun throws out solar wind in all directions and this hits the earths magnetic field, and this makes an asymmetrical radiation field held somewhat 'downwind' of the earth. GEO swings you in and out of this radiation zone, but you are past the worst of it. But in a solar storm you can get plenty toasty, both direct from the sun and from the edges of the earths Van Allen belt- which gets pumped up at those times.

And there's continual bondbardment from cosmic radiations- this cosmic radiation would cause cancer about every 15 years or so if you don't shield it. So 1-2m of shielding deals with that.

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I agree the rendezvous failure mode is unacceptable.  But this wasn't my idea.  I was just exploring/expounding on it...  I think other people usually have contributions, and I like to hear what they say.

Yes, I don't think it works as stated.

I am wondering if a modified form might work though. If you hang a rotating bolus off of the elevator, then a rocket might be able to jump vertically off the ground and grab the tip, and then climb along the cable to the beanstalk. That wouldn't endanger the beanstalk too much, and provided it wasn't at too low an altitude you might be able to fully shield it without adding too much weight to the beanstalk. But I haven't done the maths, and it's probably a bit iffy.

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In absence of a method that I feel to clearly be superior, I believe we will end up with small, shielded, man-rated containers for a long, slow climb up the cable.  But that is just me...

I'm thinking taxis from LEO to anywhere using fuel raised up the beanstalk and aerobraked down to LEO. Access to LEO by rocket. Refuelling like that is *great* if the beanstalk is cheap- rocket fuel is cheap enough. But right now we have to launch it on rockets, and that's not so good.

Shielded man-rated containers work too. But it's slow; and probably going to be cramped initially. But eventually, with a really massive cable it's maybe not a problem.
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Mumbles

p.s. incidentally if you lift a LEO launcher up a beanstalk, say 300km before lighting the rocket, it helps a lot- the vehicle avoids having to hack through the atmosphere, it doesn't have to gain any further altitude, and the rocket nozzles see only vacuum which makes them about 20% more efficient, and at 300km you're below nearly all the Van Allen belts, so the radiation isn't a problem. Also you're only using the beanstalk for a couple of hours, so you can use the beanstalk more frequently.
51  General Topics / News & Commentary / The Next Step for Private Orbital Transport on: January 27, 2005, 10:00:31 AM
Quote from: Mumbles
I think the previous post meant that rather than firing a LEO rocket to get to LEO ORBIT, with the requisite orbital velocity in addition to the altitude gained, you could just use the rocket to go (mostly) straight up.

Nitpick: LEO is Low Earth Orbit. So LEO Orbit is redundant.

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By not having to add the orbital velocity, and using that energy to increase altitude, it might be possible to rapidly transit the Van Allen radiation belts and then grab on to the SE cable for the rest of the trip.

Yes, I know, but it doesn't make any sense. Don't forget that the cable *is* moving *fast* at GEO, and even at GEO you aren't completely out of the belts even there- and you need a GTO capable rocket to get that high; never mind about actually connecting to the cable.

So, if you use a LEO capable rocket going straight up, can you get past the belts? No; you'll latch onto the cable *way* below GEO, still well within the belts, and if you miss the cable you are doomed (reentry angle being way off); and if you hit the cable, the cable is doomed as well.

I'm not saying it wouldn't help, I'm just saying it wouldn't help enough; and there seem to be large practical issues with doing it anyway.

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Mumbles
52  General Topics / News & Commentary / The Next Step for Private Orbital Transport on: January 26, 2005, 04:48:17 PM
Unless I'm missing something, which is entirely practical, it doesn't seem terribly practical. The closer you connect to the beanstalk at GEO the nearer to being a GEO-capable launcher you need. GEO-launchers are expensive, roughly 3x more expensive than LEO launchers.

And the Van Allen belts extend most of the way to GEO. So it doesn't look like you would be saving much. Then there's the problem of standing on a column of flame whilst you try to attach to the cable; and without cutting the cable.

It's probably better to just launch to LEO, and refuel with fuel dropped off of the elevator and aerobraked into a suitable orbit for docking. Or something.
53  General Topics / News & Commentary / The Next Step for Private Orbital Transport on: January 24, 2005, 03:44:18 PM
The problem with this thread is that it is predicated on the idea that going a few thousand miles suborbitally is substantially cheaper than going to orbit.

Well, it is cheaper.

Consider that more than one orbital launcher is just a modified ICBM.

The payload difference between orbital and intercontinental suborbital for the same launcher is only about ~30%; so the price is 1/(1-0.3), about 1.4x higher for orbital than a few thousand miles.

So a few thousand miles is only going to be 70% the orbital price. That's currently running at $10 million or so. So the suborbital price is about $7 million. You'd have to be in a *tearing* hurry.

Still, if you stick wings on it, you can do better than a purely ballistic approach, but it still won't be cheap.

Then there's the safety issue. Currently passengers are lost about 1-2% of launches. That would probably preclude it being used for anything but reaching orbit. It's only acceptable for orbit because there's no other way to reach orbit.

So I think it's a no go, unless someone does something *really* clever.
54  Achieving the Space Elevator / Science & Technology / Ribbon construction on: January 14, 2005, 05:26:31 PM
Quote from: Bob Munck
The payload of the SE is about 2% of its total mass, so you're cutting its capacity in half.

So make it 500 or 1000 km apart. It doesn't matter much.
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That's pretty significant. I'd be interested in what these joints are made of, given that they weigh only a kilogram and are capable of supporting 25,000 kg or more.

Tensile strength of 6063 -T6 aluminium alloy is 240MPa. So, to hold up 25,000kg you require 250,000N of force. That's an area of 0.001m^2, so a hook length of about 30cm would be about a kilogram (~2.7g/cc).

But that's in the middle, at GEO. Near the bottom it would be a teeny, tiny fraction of this weight.

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What material could possibly keep the nanotube from slicing through it like a laser beam through butter?

Nanotubes? You just need to spread the pressure over a wider area. You use nanotubes to do that. :-)
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Carbon nanotubes are one nanometer in diameter.

You lose. Aluminum atoms are even smaller! :-)

Seriously, I don't think nanotube cables are made of single nanotubes. They're good, but not *that* good.
55  Achieving the Space Elevator / Science & Technology / Ribbon construction on: January 14, 2005, 02:26:58 PM
I don't see that there should be just 2 segments. There's no reason that I can see why you can't have 22 segments or 222 segments for that matter. The only downside is that the joints weigh more than the nanotubes, so the average weight of the cable go up as you add more segments, but the strength is the same (the joints would be atleast as strong as the nanotubes either side, for obvious reasons).

But a joint might only weigh a kilogram or less; and the nanotubes weigh around a kilogram or so per kilometer, so a joint every hundred miles is only adding 1% to the weight of the cable or so- I don't think that this is terribly significant.

There are questions about how to make a joint at all though. Nanotubes are pretty slippery. In principle nanotubes can be formed into a long loop I guess, but how easy that is in practice I have no idea. If a loop can be formed then wrapping the loop around a rod at each end would be a reasonable architecture I guess.
56  Achieving the Space Elevator / Economics & Finance / Instructive Failure on: January 09, 2005, 06:59:06 PM
Space elevators do have one thing in their favour however- they're new. That means that there's a half-decent chance that the seed elevator may be launched for pure research purposes- as in, stick it up, and see how long it lasts.

Research has a pot of money that can be plundered for this. If the seed elevator survives then funding for the full thing probably becomes a lot more obtainable- but beyond the seed there's still going to be that market risk angle, and nobody knows how that will turn out.
57  Achieving the Space Elevator / Science & Technology / Ribbon construction on: January 04, 2005, 01:26:45 PM
Quote from: Bob Munck
Ten isn't enough.  The whole SE masses about 45 times its capacity; therefore you need about 50 threads to insure that having a single one break won't strain the remaining 49 beyond their limits.  In practice, you'll need hundreds.

OTOH, the SE is likely to have a safety factor of perhaps 2, so losing even 1/10 of it's strength isn't likely to be terribly significant.
58  Achieving the Space Elevator / Science & Technology / Passenger Shielding on: January 03, 2005, 05:55:42 PM
My gut feel is that whatever the answer is, the answer is way, wayy wayyyyy too much shielding is needed.

I had an email exchange a couple of years ago, Brad indicated he was hoping a foot of metallic shielding might be enough. But that's a very high weight; and even for the most optimistic projections it's gonna *cost*- and the cost gets added on to the price of the ticket, since you have to lift it each time, and it takes payload away from the elevator.

The best way is probably to use freight to protect the passengers, for example water, or rocket fuel, or building materials. That way somebody *else*pays for their payload and the passengers only pay for themself and their consumables.

Still, it's going to require a big elevator to be able to carry all the shielding that people need. Maybe 100 tonne payload or more.

Incidentally, the bigger the elevator, the better. Shielding weight is proportional to surface area (diameter squared); whereas shielded volume is proportion to diameter cubed. So the shielding weight per person is inversely proportional to the number of people carried.

As I understand it, electromagnetic shielding can be employed, but needs a very large amount of power, and doesn't end up saving much weight; or atleast it didn't with designs for protecting space habitats. I expect that this would be similar.
59  Achieving the Space Elevator / Science & Technology / Cargo & Passengers on: January 02, 2005, 11:36:41 AM
Quote from: modavis
No, I'm entirely serious. The crux of our disagreements seems to be twofold:
 
 (1) You're saying "We know how to build much better rockets, all that's needed is to buckle down and do it."

Not quite. I'm saying that by far the most important point is to address the tourism market, since that is the only way that launch volume can grow, since it seems for all launch systems, and all future launch systems that prices will be brought down. It is *not* simply a matter of improving rockets, quite the contrary, cheap, inefficient and nasty rockets might be perfectly good if they were reliable; it is a question of developing more appropriate launch systems to address that market; whether they are nanotube based or fuel based.
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(2) We disagree about how much better is necessary to get into a virtuous circle of profitable, self-sustaining expansion in space activity. I think we'll probably see more reliable $5000/lb or a bit better soon, with significantly lower infrastructure and operations costs than current launchers, from SpaceX, SpaceDev, Xcor & co. But I think $500/lb and lower is where we need to be for that virtuous circle, and I don't see it coming from rockets in the foreseeable future.

I think somewhat higher would create a cycle; it's not even clear that we aren't already in the cycle. I've seen potential costs a lot lower than $500/lb for rockets.
 
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As for Goddard, the highest certified flight was 3,294 feet on August 9, 1938. Clary cites a claimed 7,500 feet in 1935, so I'll make it "a mile and a half" unless you can direct me to another source.

I found a reference to 9000 ft, so well over a mile anyway.

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I'm not sure what you think it accomplishes to keep saying that cost-effective nanotubes may never arrive. Everyone here knows that, and knows that the SE idea is stone dead without them.

No, that isn't my point either. My point is that the cost models for a laser-powered space elevator is not massively if at all lower than rockets, until you are launching *massive* quantities.

That's *really* bad. Nearly all big systems are small systems with the capacity to grow. Look at the Channel Tunnel. That's a big system. It took 200 years to build...

The 'fuel'- electricity is more expensive. The development and construction of the infrastructure is more expensive and the risks are enormously higher. It seems to me that few people here have really got this point. If I were to bet, even if nanotubes popped out tomorrow, I might well still bet on rockets. Indeed, because rockets seem to support tourism, and elevators don't (directly), it seems that rockets need to flourish for elevators to grow.

It's not that the emperor has no clothes, he's certainly decent, but he's certainly wearing a skimpy swimming costume, and it's rather chilly. The clothes designers need to put some more clothes on him.
60  Achieving the Space Elevator / Science & Technology / Cargo & Passengers on: January 01, 2005, 07:17:03 PM
Quote from: modavis
You show me your 10- or 20-story-high aluminum drink can that puts payloads in orbit, and I'll show you an Atlas V dropped four feet. Smiley
 

No doubt you're jesting, but a fully fueled Atlas very much is designed to fall atleast a few inches. An early rocket did that, due to engines shutting down and exploded. It's now part of the spec that it be able to fall maybe a foot intact.
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In other words, the same old "we just gotta have the will, the vision"  that has produced so many fleets of viewgraphs and Powerpoints thundering into the skies over the last 30 years.  

Now you're just being facetious.
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Goddard (who contrary to the "neglected genius" myth, probably received more financial support than any other U.S. scientist of his time) did fine fundamental research, but never got a rocket as much as a mile up,

Wrong!
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How very obtuse of them not to have noticed all the subsonic jets already flying and proliferating rapidly when its development began. No, the Concorde's expected market was "travelers who will pay a 4-5x premium over subsonic jet fares to save time." There weren't enough of them.

Wrong again. So far as I can tell British Airways ran Concorde at a profit. The real problem was that the airlines wouldn't buy Concorde, because they were happy with their subsonic transports- they didn't have to take the risk.

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It's small at the going rate of $10K-20K per kilogram. We're aiming for roughly 1/50th of that with the initial SE, and well under 1/100th of that soon after.
 
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As I said in another thread, the financial math that has allowed fiber optics to eat into the comsats' market share could well turn around rapidly if comms vendor could spend 1/50 as much per kg on launch, meaning much bigger power supplies and antennas.

Nah, forget about it. Fibers have orders of magnitude more bandwidth, and coupled with terrestial radio are looking more and more cost effective. Telecommunications through satellite is only good for quick deployment. I don't see it dying in the short term though.

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Sorry, but I think most of the current space tourism boomlet is a result of artfully directed publicity around the X Prize competition. You've never explained why, if the vast untapped demand for a few minutes of free fall and a great view -- which has surely existed all along -- took 50 years to get us from an X-15 to a check from Richard Branson, the floodgates are now going to open wide so rapidly.

Because they've never had a check from a Branson before! A money man has actually paid for it! A money man actually *can* pay for it! And there seems to be a market! There's even some signs of confidence that rocketry isn't a government only thing. Now, all the billionaires are falling over each other to get their own private launch system; it's a status symbol.
 
But, my best guess is that if Branson fails for market reasons, orbital tourism is doomed, and the Space Elevator may even be doomed also.

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Relax; it's just their role as the primary way to put mass into orbit that's doomed...

Not till cost-effective nanotubes arrive if they ever do. And only if none of the possible 'gotchas' kill the beanstalk idea stone dead. I can think of atleast 5 reasons why it may never, ever be built. Whatever else you can say about rockets, they do actually work.
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