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Space Science

NASA Has Plans for 2nd Space Station at L1 439

Keith Gabryelski writes "New Scientist has an article on NASA's unveiling of a "blueprint for the future" of space exploration. It entails a Space Station 5/6ths of the way to the moon. In other news, radiation sheilding on the space station isn't so good."
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NASA Has Plans for 2nd Space Station at L1

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  • by WestieDog ( 592175 ) on Wednesday October 23, 2002 @08:05PM (#4518147) Homepage
    Why not just build on the moon? Why stop at 5/6 the way to the moon?
  • Sure, THAT'LL happen (Score:5, Interesting)

    by thetzar ( 30126 ) on Wednesday October 23, 2002 @08:06PM (#4518151) Homepage
    With the insane ammounts of cost overruns and mismanagement in the ISS project, who thinks that a jaded congress is going to vote a new space station [no matter how much MORE useful than the ISS it may be] any funds whatsoever?
  • by peter303 ( 12292 ) on Wednesday October 23, 2002 @08:08PM (#4518166)
    There is only room for three people for extended stays, due to Congressional budget cuts in the habitation module and escape vehicle. The original intention is seven people. That means the crew of three must spend 75% of their time in maintenance with only a small amount for experiments and other innovation. Unlikely the current administration will increase funding. Many republicans hate NASA because of its environmental monitoring programs. And the previous scientific leader of NASA has been replaced by an accountant (cut and slash).

    The new IMAX movie about the first three years of space station construction is fascinating.
  • :tcejbus (Score:3, Interesting)

    by sstory ( 538486 ) on Wednesday October 23, 2002 @08:12PM (#4518187) Homepage
    space is a harsh place. Radiation, temperature extremes, enormous distances of nothingness. It'll be nice when it isn't almost senselessly prohibitive to go.
  • radiation (Score:2, Interesting)

    by Anonymous Coward on Wednesday October 23, 2002 @08:12PM (#4518191)
    would it be at all possible too recreate the earths field around the space station ,like give them a field generator or something. i dunno. how much power would it need to be effective at repelling the charged particles?.
  • Replacement for ISS? (Score:2, Interesting)

    by siskbc ( 598067 ) on Wednesday October 23, 2002 @08:15PM (#4518208) Homepage
    This may be almost a replacement for ISS. It's become fairly obvious that certain nations (*ahem Russia*) are intent on using the ISS as SpaceDisney, letting any jackass with $20M up there. So NASA might be trying to get their own space station back. ISS was really a political animal anyway (Congress loved the idea of unity or some similar crap).
  • Re:Mixed emotions... (Score:2, Interesting)

    by IdleTime ( 561841 ) on Wednesday October 23, 2002 @08:16PM (#4518220) Journal
    The question is not if NASA can keep a budget, but rather if the politican will accept it if NASA gave them an acurate budget.

    As it is now, I put my $.02 on the idea that NASA is under-budgeting in order to gte the crooks^H^H^H^H^H^Hpoliticans to accept the project.

    Nobody is going to tell me that NASA is not smart enough to put out a price that looks good, get the funding and then slowly, but steadily increase the cost.
  • New scientists. (Score:5, Interesting)

    by Docrates ( 148350 ) on Wednesday October 23, 2002 @08:18PM (#4518234) Homepage
    If i'm to be modded down for offtopicness, well, I deserve it, but I need to get this off my chest:

    I simply can't read new scientist anymore. When the site actually loads (regardless of slashdotting), every single article they publish seems to be the scientific equivalent of the paparazzi.

    I mean, really, one thing is to have a non-peer-reviewed magazine, and an entirely different thing is to intentionally publish exagerated, ridiculous, absolutely un-proved (and almost always un-provable) "facts". Even the simplest of stories is spinned beyond recognition. If a story comes up of some scientists spotting a .00001% deviation from expected results researching *.*, right after they make clear that most likely it's due to faulty measurement equipment, New Scientist will publish that they found aliens, that they have a draft of the alien invasion plan, that Einstains's GToR is therefore void, and that in fact he himself WAS an alien trying to distract us from the truth. And then they _really_ start speculating and tell you that they infer from the inforamtion that Einstein was a shape shifter and that he was also the first husband of Melinda Gates.

    Now, I haven't read this article (not that I could even if I wanted to, NS' site goes DoS when they're linked from my cousin's non-porn website), but I'm sure I'll get more substance out of /.er's comments than NS (if you can believe that!)
  • radiation shielding (Score:2, Interesting)

    by bbc22405 ( 576022 ) on Wednesday October 23, 2002 @08:18PM (#4518237)

    In other news, radiation sheilding on the space station isn't so good.

    Lead and tungsten are your friends.
    (I suppose that this might be a good time to come out in favor of developing a cheap, non-man-rated left vehicle, suitable for lofting dense, space-station-module-sized things into LEO...?)
  • by Hays ( 409837 ) on Wednesday October 23, 2002 @08:22PM (#4518257)
    The time between when Columbus "discovered" the new world and Magellen circumnavigated the globe was 30 years. It has now been 30 years since Apollo 17, the last time man visited the moon, the last time man left low earth orbit. I think it's a great failure of our race that we've dragged our feet such.

    To think that technological advance is blazingly fast in this day in age is misleading. We're not doing too well at hitting the important targets. NASA might just now be waking up to this, but it's yet to be seen if their budget wakes up to it. (Nasa funding was 4% of the national budget at the height of the Apollo program, it's less than 1% now)

    So I applaud their very recent efforts to finally mention some vague goals away from Low Earth Orbit. L1 is a fine stepping stone, but Mars is where the public eye is. Nasa administrator Daniel Goldin had some brave words about the possibility of sending men to Mars in this decade or the next, but Bush put a bean counter in charge of Nasa pretty quickly to throttle cost overruns from the ISS.

    What we really need is a president giving NASA a kick in the pants, and the funding to follow, as Kennedy did. Either that or wait around for private space exploration to become worthwhile, and we're going to be waiting quite a while in that case. Another space race? maybe China? I hope so. Because the current NASA schedule is anything but ambitious.
  • by pbranes ( 565105 ) on Wednesday October 23, 2002 @08:23PM (#4518269)
    After the Apollo missions, there was no budget to keep up the plans for the Apollo V spacecraft. If NASA wanted to land men on the moon again, they would have to reinvent the great rocket science of Wernher von Braun. NASA should just shoot for going to the moon now and establishing a science based set of missions.

    Apollo was not built around science. It was built as another battlefield of the Cold War. The space program wasn't even important until the Soviet Union beat America into space. When NASA can make routine, scientific trips to the moon, then they can concentrate on building a space station at L1 and worry about getting to Mars.

    The Space Shuttle is routine now, and usually stays within budget. NASA should build on this technology, slowly and gradually. We will learn so much more this way rather than putting a thermometer and a seismometer on the moon as quickly as possible.

  • Moon surfing? (Score:2, Interesting)

    by .sig ( 180877 ) on Wednesday October 23, 2002 @08:40PM (#4518372)
    uh, I don't mean to point out the obvious, but you don't need thrusters to stay in a stable 'orbit' on the surface of the moon. If they built a station on the moon, I really doubt it'd go very far on it's own.

    Of course, it'd be easier to leave from L1, as they would have to fight the gravity of the moon to get back into space. I hope that's what you meant...

  • by ashitaka ( 27544 ) on Wednesday October 23, 2002 @08:46PM (#4518415) Homepage
    This! [l5news.org]
  • by AaronPSU79 ( 536655 ) on Wednesday October 23, 2002 @08:52PM (#4518456)
    IANARS (rocket scientist) but what are the possibilities of utilizing the asteroid just discovered that shares the earths orbit for some form of station. A snippet from this article: http://news.bbc.co.uk/2/hi/science/nature/2347663. stm

    "Although only about 100 metres across 2002 AA29 may play a role in the manned exploration of space out of all proportion to its size.

    Already researchers are speculating that it could be visited by an unmanned spaceprobe or even become the first object after the Moon to be stepped on by astronauts.

    The object could tell us a lot about the composition of asteroids.

    Some have speculated that it could be nudged into a permanent Earth orbit where it could be studied at greater length."

    If you could nudge this thing into the right orbit wouldn't it make a wonderful station? Lots of room, some raw materials, and you could burrow into to escape the radiation. I understand that some asteroids are nothing more than loose collections of rocks and dust. But it's an intriguing, and plausible idea.
  • by Anonymous Coward on Wednesday October 23, 2002 @08:53PM (#4518460)
    Mostly incorrect, if you had read the article about radiation, you would understand the fundamental problem with lead is because of its weight, but not the way you are thinking. The problem is that the large nuclei (the middle of the lead atoms). These are struck by the cosmic ray, releasing more deadly radiation to the crew inside, so your precious lead sheilding would kill them all. Which is why the shielding described in the article (copied below) is a light plastic.

    Radiation inside the ISS, and the now defunct Mir, is caused when the fast, heavy ions that make up cosmic rays collide with the aluminium hull, releasing a shower of secondary particles into the living quarters.

    To mitigate this effect, the ISS has been fitted with additional polyethylene shielding that contains lighter atomic nuclei, which are less likely to throw out neutrons when hit by cosmic rays.
  • by Yorrike ( 322502 ) on Wednesday October 23, 2002 @09:05PM (#4518525) Journal
    The USA: Taking the I out of ISS.

    It's like a playground spat: "We don't want you bringing your friends to our treehouse, it's for members only!"

    Of course, the reason Russia can afford to keep contributing to the ISS, is because of those "jackasses". The US needs to stop whining. Russia obviously has a huge interest in the ISS, or they wouldn't bother selling rides to finance their parts of the project.

  • by Goonie ( 8651 ) <robert.merkel@be ... g ['ra.' in gap]> on Wednesday October 23, 2002 @09:06PM (#4518536) Homepage
    In sci-fi novels, the radiation problem is usually solved by a "magnetic shield" which I presume bends the particles around the ship (or at least the inhabited parts).

    Maybe the magnetic fields required are too strong to be practical. IANA physicist.

  • by phriedom ( 561200 ) on Wednesday October 23, 2002 @09:09PM (#4518558)
    I thought Lagrange points collected a lot of dust, which would be bad for optics. Its not like you can vacuum that stuff up either. If you are 5/6ths of the way to the moon already, why not just go the rest of the way? A luna's gravity keeps the dust down and provides many other benefits. I expect Luna would also supply SOME building materials, like maybe 10 foot thick rock walls to stop cosmic rays, for example. The lunar gravity would be a disadvantage for launching other missions from there, but perhaps that could be compensated for.

    If there are more informed people out there who see what I don't, I'd love to hear it.
  • by lostchicken ( 226656 ) on Wednesday October 23, 2002 @09:26PM (#4518662)
    Not to be picky, but this is Slashdot. Picky is what we do here. The rocket for the lunar Apollo missions was the Saturn V series booster, not the Apollo V.

    The Saturn series was used after the Lunar Apollo four times (correct me if I'm wrong). Three were Apollo CSMs (one to ASTP, two to Skylab), and one, a Saturn INT-21 (a modified Saturn V) boosted Skylab, which really was a good scientific experiment, to orbit.
  • by georgenfrank ( 461654 ) on Wednesday October 23, 2002 @09:32PM (#4518698)
    Just how big is the Lpoint before you are not in it anymore?
  • Acceptable risk? (Score:5, Interesting)

    by Stoptional ( 469673 ) on Wednesday October 23, 2002 @10:32PM (#4518856) Homepage Journal
    Many here have spoken of the "insane" "horrendous" "crazy" amounts of money spent on IIS. How many think that this money was spent *mostly* to make sure that no one died?

    Was it a good thing to spend that money on? Is the IIS over-engineered in favour of preventing un unfortunate death? (Aside - How many of you, after viewing the interior of an Apollo era craft, would still go into space in one of those?)

    Let's look at a little history. If during the 18th century, we had spent an equivalent amount of dough on sailing ships (with the (un)stated goal of preventing deaths (monarchs HATE to look bad)) I think we'd still be looking for our assholes with a mirror. We'd never have left Europe. The economy of the day would not have tolerated it.

    My father-in-law was one of the Canadians who helped develop the nuclear power station system called CANDU. His stories are quite telling. His take on risk? - during development of CANDU the engineering studies required would fill a couple of banker's boxes. Today, those studies would fill a small stadium. With a exponential rise in cost. Why? What's the return? A couple of lives? A dozen lives?

    My point is - we have tried to reduce the risk to zero and this is not only stupid, but unwise. Stupid because there will always be a risk. How much money are we going to let timid politicians/bureaucrats spend on that last .005% of risk reduction? Unwise, because we lose the ability to pursue our dreams. We're deadlocked.

    "Acceptable risk" is a term that has been lost from the West's vocabulary and it is time to bring it back.
  • by abucior ( 306728 ) on Wednesday October 23, 2002 @10:49PM (#4518925)
    While reading about the problems with radiation shielding, I came up with perhaps one way they could reduce exposure: Add improved shielding to the sleeping closets. If they can cut out 90% of the radiation in an area that the average astronaut will spend 30% of his or her time in, that`s a significant savings for relatively little added weight.
  • by Dr. Spork ( 142693 ) on Thursday October 24, 2002 @01:23AM (#4519636)
    You know, a couple of rounds of budget cuts later, their next grand space station will be another useless pile of expensive junk just like the first one. The problem is that it will be squatting one of only five stable points at which long-term space projects can be built.

    Well, I don't like it. What gives NASA the right to squat on what is probably one of the five most valuable places in the universe (from our perspective)? Will there be a deal arranged that in 50 years, when a better space agency comes up with a better project for the liberation point, they'll move their junk out of there? There had better be. Seriously, the UN has to get on this fast. Right now, the USA has basically called dibs on two of the five liberation lunar liberation points, plus there's that second-generation telescope that they want to put into the liberation point behind the earth, where it is always shielded from the sun. Well, this is the ideal place to build a telescope, and once something is there, everybody else, even people with a better telescope idea, are shit out of luck. They'll have to spend billions to make heat shielding because NASA is squatting on the one spot where the heat shielding is natural (permanently in the shadow of Earth).

    If I were the UN, I would set a squatting limit of 30 years on any given liberation point. If somebody wants to use it after that, whoever was there before has to get the fuck out and clean up after themselves. I think it's likely that in 30 years all the liberation points will have something, and in another 30, countries will be duking it out over who gets to go there next. The people who want it most will have to compensate the other people who want it. In any case, this is not too soon to be thinking about making international laws about this.

  • by cats-paw ( 34890 ) on Thursday October 24, 2002 @01:54AM (#4519731) Homepage
    The article talks about IONS colliding with atoms and causing secondary radiation. I would like to get clarification on this point.

    If it really is ions causing the problem then a strong magnetic field should provide some protection, just as the earth's field does. In fact the article talks about a significant increase in radiation when outside the earth's magnetic field.

    A strong magnetic field might be enough to allow deep space travel. If it's primarily electromagnetic radiation, i.e. photons then your screwed, of course.
  • by Cef ( 28324 ) on Thursday October 24, 2002 @01:56AM (#4519738)
    Not that you'd probably want to use the water afterwards, but there is no reason you can't use it beforehand.

    Using waste water could work. Wether reclaimed from air, or from body fluids, this would only have been jettisoned into space or reprocessed (and reprocessed water tastes like crap!) anyway.

    For that matter, waste biomatter may actually be good at shielding radiation, but you wouldn't want a leak anywhere on the inside of the station! Ewwwww!

    Also, you could generate oxygen and hydrogen from water by electrolysis (well you'd have big solar panels anyway). You could use these as a propellant, since any craft at the L1 point still would need some sort of station keeping thrusters (any craft docking/departing the station, or small impacts from space debris, will change the station's balance and momentum, knocking it out of the "perfect centre" it should be sitting at), and this could provide some of the required fuel. Or you could use some of the oxygen to add to the air mix, and the hydrogen in fuel cells.

    Only problem with using a liquid as a shield is that when the station is in darkness it'll be frozen, and when it's in light it'll be warm or boiling. Water changes a LOT in volume with heat, so the hull would have to be able to stand that change. And any leak where there is liquid or steam would have to be plugged, otherwise you'd end up with the liquid ejecting into space and propelling the station out of it's nice stable placement.

    In the meantime, just make sure the astronauts dose up on their caffiene and they'll be fine. *grin*
  • Re:Half right (Score:2, Interesting)

    by GileadGreene ( 539584 ) on Thursday October 24, 2002 @01:58AM (#4519743) Homepage
    Not exactly, yes, L1 is an "unstable" Lagrange (or libration) point, however if you put an object in ORBIT around the L1 point it is extremely easy to keep it there. It is analagous to the motion of a top, yes, the top is unstable and will fall, but if you spin it it will remain upright. The difference is that very little fuel is required to maintain the orbit about the libration point.

    True. But the dynamics in that halo orbit are very messy. Just getting to the orbit is a pain - the trajectory requires a lot of work before the mission - and if you need to perform a maneuver while you're in your halo (e.g. to rendezvous and dock), well, good luck. One small delta-v in the wrong direction and you're on the unstable manifold of the halo and an express elevator to whoe knows where.

    There are plans for a probe at the Earth-Sun L1 point (about 4 times farther than the moon)that will similiarly orbit that L1 point but for different reasons. If it were precisely at the L1 point, then we would have point our antenae directly at the sun to communicate with it. The noise from the sun would make it essentially impossible to communicate with, hence the offset.

    Actually, I can almost guarantee that the reason the probe is going to a halo or lissajous orbit is that it is well nigh impossible to stay at the Sun-Earth L1 without burning an insane amount of fuel. The Sun-Earth L1 is unstable. I would however not be surprised to find that the particular orbit selected (the size of the halo) was driven by the need to achieve a certain angular separation from the sun.

  • by GileadGreene ( 539584 ) on Thursday October 24, 2002 @02:16AM (#4519805) Homepage
    Putting a space station at the Earth-Moon L1? snort What yahoo at NASA HQ came up with that one? They obviously didn't bother to check with anyone who actually knows anything about libration points.

    Why is this stupid? Here's why:

    1. The Earth-Moon L1 is an unstable point. Put something there (if you can), and it will immediately drift away.
    2. Yes, there are these things called halo orbits and lissajous orbits, that are essentially periodic orbits around the libration points, but their dynamics are very complex.
    3. Did I mention that the dynamics in this region is very complex? Actually getting onto a halo or liss is not anywhere near as simple as computing a hohmann transfer - it takes a lot of careful precalculation. The region around the L1 point (and all libration points) is governed by three-body dynamics - highly nonlinear, potentially chaotic, very messy to deal with.
    4. Even assuming that you successfully put your space station at L1, how the hell are you going to get anything else to rendezvous with it? (see previous point) I can't even imagine trying to carry out docking maneuvers in that kind of gravitational environment.
    5. The reason it's cheap to get to a halo (the efficient "superhighway" they keep talking about) is that you can hop on the stable manifold associated with the halo (essentially a sheaf of trajectories that asymptotically approach the halo) where it passes near the earth. But this cuts both ways, since the halos also have unstable manifolds that lead away from the halo (and are also cheap to get onto). One small burn in the wrong direction, and "whoops!", you're on the unstable manifold leading away from the halo and off to who knows where.

    So what do you have when you break it down: A dynamically complex region of space that will make proximity maneuvers extremely difficult to perform. And if you make one small mistake in those difficult maneuvers, you're basically headed for Pluto. Bottom line: L1 is just about the stupidest place to put a space station that you could pick.

  • by jpmorgan ( 517966 ) on Thursday October 24, 2002 @02:48AM (#4519901) Homepage
    Let's see, NASA, you know the people who send space probes galavanting around the solar system slingshotting around the sun, planets, moons etc... to reach their final destination thinks that building a space station in an L1 point is a good idea. Obviously, you know better than NASA and don't try to figure out why they'd pick L1 over say L4 or L5. *sigh*

    While maintaining position at L1 is technically more challenging than maintaining position at L4 or L5, it has a higher payoff. For one, you won't be trying to build your space station in a veritable gravel pit in space. Secondly, it's trivial to launch vehicles from the point - you just let them go and they'll drift off without active station keeping. And considering how the intended primary purpose would be as a place to launch other missions from, that's a slightly useful thing.

  • by mcc ( 14761 ) <amcclure@purdue.edu> on Thursday October 24, 2002 @03:07AM (#4519942) Homepage
    This brings up an interesting question i never quite understood-- can you put something at a lagrange point if there's already something there?

    If the SOHO satellite and the proposed space station are both at L1, how close will they be? Visible distance?

    How big are these "point"s? I get that there's going to be one optimum point, which is L1's location, but how big is the area where the effects of L1 are still felt to the degree where it's a useful place to park something? I.E., how big is this space station's playpen?
  • by B3ryllium ( 571199 ) on Thursday October 24, 2002 @03:29AM (#4519996) Homepage
    I've heard that Beryllium is commonly used in nuclear facilities to protect against neutron emissions. Since the article suggests that the Neutron emissions are the cause of the radiation (supposedly), perhaps a layer of Beryllium shielding would be called for?
  • by SpiderJ ( 471622 ) on Thursday October 24, 2002 @04:48AM (#4520190) Homepage
    Right, so I'm by far not all that knowledgable on this subject (i.e. I'm pronably incorrect but feel free to educate me; that's why I read /. ), but here's what I've picked up:

    The moon is in orbit because of a gravitational pull by the Earth. It's velocity (or whatever the proper term is in astrophysics) is what makes it seem to change its visible side.

    For it to have gained that velocity/trajectory/momentm/whatever, the moon had to have, at one point in the history of the universe, collided with the Earth. The physics of the collision set the moon at a certain range from the Earth. The geography of the Earth changed from the impact, and the moon was sent spinning off into the orbit it has.

    Now, the moon was off in orbit over the Earth, having absorbed some kinetic energy from the planet. My current knowledge tells me that the exchange of said energy aeons ago pushed the moon into a trajectory around our planet that is slowly pushing the moon away from the Earth. I believe at a rate of 2 inches a year.

    So, I'm wondering if the LaGrange (sorry bout the spelling folks) points are completely stable. Has the math been done to account for the continual shift in distance, or am I mistaken?
  • by Anonymous Coward on Thursday October 24, 2002 @09:45AM (#4521534)
    We had a heavy-launch infrastructure in the Saturn 5 rockets that launched the Apollo missions. NASA dismantled the factories, etc. for building them in order to promote the Space Shuttle. The shuttle was supposed to be cheaper because it's reusable. Sigh....
  • by Greedo ( 304385 ) on Thursday October 24, 2002 @10:02AM (#4521691) Homepage Journal
    How can the gravitational pull of the Earth and Moon be balanced at points L2 and L3? Maybe the gravitational force from both bodies is the same at those points, but both points, the Earth is on the same side of the point as the moon, making them not-so-ideal for satellites or space stations I would think.

    The forces wouldn't cancel each other out. Right?

    (Actually, I can see how L3 would work, if the satellite had the same orbital period as the moon. But L2 confuses my little general-arts-degree mind.)
  • by WeeLad ( 588414 ) on Thursday October 24, 2002 @10:19AM (#4521829) Journal
    If we sent two people to mars, one would die

    What about Luna? Is the Moon still within the Earth's magnetic sheild? It is many times farther out than the ISS. We sent a couple of people there, or so they tell me. Did they have any adverse health problems? I would think that the shielding used on that trip was probably not as advanced as todays sheilding.

    How much radiation were the people on the Apollo missions receiving compared to a year on Earth?

  • by Twirlip of the Mists ( 615030 ) <twirlipofthemists@yahoo.com> on Thursday October 24, 2002 @10:45AM (#4522052)
    As noted elsewhere, the SOHO is at the Earth-Sun L1 point, inside the orbit of the Earth. We've been talking about the Earth-moon L1 point, between the Earth and the moon. Different things.

    As for your other question, a libration (or Lagrange, or Lagrangian, or whatever) point is just that: a point. L1 is the dimensionless point in space where the gravitational forces pulling toward Earth and toward the moon exactly equal one another. If the center of mass (also a dimensionless point) of a body is parked exactly on the libration point, then the body will experience no net gravitational pull in either direction, because the forces will be balanced.

    Of course, keeping the center of mass of a body parked on the L1 point is not a trivial thing. Even the pressure of light from the sun will be enough to nudge it slightly out of position, and once out of position, the body will tend to fall further out of position due to gravity of either the Earth or the moon. So the real question is this: how gentle or steep is the gravity gradient surrounding the L1 point? In other words, how much does the force of gravity change over time as one moves in and out of the L1 point?

    Remember that gravity is an inverse-square relation. The force varies with the square of the distance between two objects. So when the two objects are close together, the force varies a lot over a small distance. But when the objects are farther apart, the force varies less over the same distance. When bodies are far, the gravitational gradient (distance rate change of force) between them is said to be shallow or smooth, and when they're close together it's said to be steep.

    All that adds up to is this: it's easier to keep a body at the Earth-Sun L1 point than at the Earth-moon L1 point because the gravitational gradient is steeper in the Earth-moon system than in the Earth-Sun system.

    Now, the L4 and L5 points are different. L4 and L5 are local attractors; you could put an object in orbit around L4 or L5 itself, and it would tend toward stability. So it's easier to put multiple objects at L4 and L5 than it is to put them at L1, L2, or L3.
  • by WillWare ( 11935 ) on Thursday October 24, 2002 @11:11AM (#4522242) Homepage Journal
    It's good to see this discussion informed by some knowledge of orbital mechanics (a lot more than I have, obviously). For those of us playing catch-up here, some links: 1 [caltech.edu] 2 [vt.edu] 3 [stk.com].

    This is obviously a richly researched topic with lots of published papers. Some [ieec.fcr.es] of them talk about new algorithms for tackling the complex dynamics you're talking about. And of course there's always Moore's Law; the computers used for Apollo missions were about as powerful as (or maybe much less than?) Palm Pilots.

    It's probably quite feasible to give the L1 station a radio link to an orbital mechanics cluster on the ground, which can be as big as is needed, and could run equations of motion for a couple dozen nearby orbits in faster-than-real-time.

  • by GileadGreene ( 539584 ) on Thursday October 24, 2002 @03:08PM (#4524288) Homepage
    You misinterpret my post (or "smug troll"). I'm not saying that we should put stuff at L4 or L5. I'm saying that putting something at any libration point is going to be tough. Three body dynamics are not easy. Even NASA (if you talk to the people who actually understand trajectories) admit that libration point trajectories are far more complex than your typical conic section.

    Regarding SOHO, it was not teh first, and is not the only spacecraft at a libration point (I believe that the first was ISEE-3 - the most recent I know of is Genesis). But it is a far different proposition to place a spacecraft in a single, carefully pre-planned orbit and keep it there than it is to jump between halos, and perform proximity operations or rendezvous and docking (which would be needed for a manned platform, or even an autonomously assembling spacecraft). I'll say it again: the dynamics in the vicinity of a libration point are very complex, and presently our understanding of them is limited.

  • by p3d0 ( 42270 ) on Thursday October 24, 2002 @07:01PM (#4525861)
    Fair enough. Thanks for the reply. You must admit, though, there's a world of a difference between saying "libration points are very complex" and calling NASA scientists stupid yahoos who "didn't bother to check with anyone who actually knows anything about libration points".

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