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On Orbital Fuel Stations

dylanduck writes "Being able to fill up your spacecraft from a fuel depot in orbit round the Earth or Moon is key to the long-term prospects of astronauts exploring the solar system, according to NASA engineers. Trouble is NASA doesn't want to build it themselves. So there's $5 million for any enterprising groups who can develop a simple version themselves."

25 of 152 comments (clear)

  1. It's doable by PatrickThomson · · Score: 3, Insightful

    Obviously you need atoms up there, which have to come from somewhere, but splitting them into fuel is easy, you're floating in space with all this sunlight. The problem is that if you carry a kilo of water from the surface and then swap it for a kilo of hydrogen/oxygen when you get to space, the benefits are minimal (easier storage?). This would work well coupled with a captured icy asteroid, even a small one.

    --
    I am one of many. My idea is not unique, nor do I expect my voice alone to sway you. I speak in a chorus of opinion.
  2. Hmmm by hyfe · · Score: 4, Insightful
    Erm, you still have to get the fuel up there right? .. and the cost of putting something up there is still reasonably proportional to weight?

    So sure, once you get liquid hydrogen from the moon / some other energy source it'd be usefull.. which pretty much means we need a moonbase first.

    --
    "" How about taking the safety labels off everything, and let the stupidity-problem solve itself? """
    1. Re:Hmmm by Funkcikle · · Score: 5, Funny

      "$9 a gallon? Let's just orbit a bit longer till we find a cheaper one."

    2. Re:Hmmm by MichaelSmith · · Score: 3, Insightful
      Erm, you still have to get the fuel up there right? .. and the cost of putting something up there is still reasonably proportional to weight?

      Fuel depots make sense for aircraft on Earth because you can use cheap surface transport to deliver the fuel, store it, and then load it into your aircraft when needed.

      This might work in space if you have ion powered slow boats to ship the heavy stuff, and fast human carrying vehicles to load up on fuel. But we are not that advanced yet. If we go to mars any time soon it might make sense to launch the cruise stage unmanned and then hook it to the command module in earth orbit. That would be a kind of fuel dump.

    3. Re:Hmmm by Darkman,+Walkin+Dude · · Score: 3, Interesting

      There might be methods whereby you wouldn't need to carry the fuel with you, for example with a space elevator. However, just what advantages would a space elevator offer over a tower launch? (I've used parts of this post before, but I have since refined my ideas). I contacted a man responsible for a similar idea a while back, the skyramp (warning: hideous javascript menu may break firefox), Carlton Meyer, and had a dialogue in which he pointed me to a tower launch archive.

      The ideas I see bandied about there are similar to what I had in mind, which would be essentially an 11km tall tower (think pylons rather than skyscrapers, based at sea), with evacuated airless launch tubes, using nuclear reactors to power a maglev or pulley system to accelerate vessels to escape velocity. These would then emerge above the end of the troposphere, with it's associated weather and air pressure, and have little to no fuel needed to match the earth's gravity, meaning you could do a lot more while you were up there. At a reasonable acceleration (5 to 7 g's) you would be in geostationary orbit. From there you could build a fully system wide ship or ships, as its much easier to escape the planet's gravity from GEO than from the surface.

      Not only would this enable multiple launches daily, it is, unlike the space elevator, readily achievable with today's technology, and financially viable as well. Given NASA had an annual budget of $16.2 billion for 2005, and a nuclear power plant costs a cool billion to build, give or take, we could have this up and running in a few years.

    4. Re:Hmmm by cnettel · · Score: 2, Insightful

      I somehow imagine that the pylon construction could be far more expensive than the power plant part.

    5. Re:Hmmm by adam1234 · · Score: 2, Insightful

      Most of NASA's budget inevitably goes to people (ie, payroll) and bureaucratic oversight, not operations.

    6. Re:Hmmm by Eivind · · Score: 2, Interesting
      Is 11km really enough that you don't need to worry about air-friction emerging from the tube at escape-velocity ? (well almost, you said geosynch orbit. But that is like 90% escape-velocity anyway)

      I very very very much doubt it. Even at 31km you still have 1% of the sea-level air-pressure, and at 9km healthy people can still breathe unaided. (as witnessed by the fact that people have climbed Mt. Everest without oxygen)

      I don't know the air-pressure at 11km, but I'd guess around 15% of that at sea-level. Are you suggesting that punching trough 15% of sea-level air at speeds around 40.000km/h causes negligble frictional losses ?

      I haven't done the math, but I think it's more likely the resulting friction would make re-entry look gentle, thus you'd need to start out going *even* faster to compensate the frictional losses.

      In short, I think releasing a spacecraft at 11km with sufficient speed to reach geosynch is impossible, you would have to release it with such a speed that it'd immediately burn up.

    7. Re:Hmmm by Firethorn · · Score: 2

      a tube 11km kept as a vaccum?
      Sure you do this in your big particle accelerators, but there are precious few maglev trains 11km long, never mind running them vertically inside a particle accelerator style environment!


      Translation: It'd be expensive.

      From the proposals I've seen, it's a decent idea. Every pound of fuel you can drop from the vehicle makes it that much cheaper. Not having to deal with atmosphere for the first part, or maybe only the 11km pressure is of great assistance.

      One problem I see is how do you keep the tube evacuated while leaving a clear path for the ship?

      --
      I don't read AC A human right
    8. Re:Hmmm by NOLAChief · · Score: 3, Informative
      If we go to mars any time soon it might make sense to launch the cruise stage unmanned and then hook it to the command module in earth orbit. That would be a kind of fuel dump.

      Effectively that's what's being planned with the earth departure stage for the proposed lunar missions. That stage would be launched on the Cargo Launch Vehicle into earth orbit, where a CEV launch would rendezvous with it for a trip to the moon. See the Project Constellation article here.

  3. In outer space the asteroid captures YOU! by Xner · · Score: 2

    Given the mass ratio between anything we can send up and the average icy space rock, it's more likely the icy asteroid's gravity will capture the craft than the other way around. Not that it's a bad thing, mind you.

    --
    Pathman, Free (as in GPL) 3D Pac Man
    1. Re:In outer space the asteroid captures YOU! by mwheeler01 · · Score: 2, Interesting

      Given the mass of a space station or an asteriod, the attraction of gravity really wouldn't have any real noticeable pull on either object. The asteroid would have to be ginourmous, and therefore unmanageable to have any real pull and I think at that point they start calling them small planets.

      --
      Pretty widgets? What pretty widgets?
  4. Have we learnt nothing. by Kaptain_Korolev · · Score: 4, Funny

    Honestly, have we learnt nothing from Jerry Bruckheimer's excellent film Armageddon.

    Refuelling in orbit is dangerous!

    Next they'll be suggesting we man these orbital filling stations with drunken Russians. I only hope Ben and Bruce are there to sort things out when matters go awry.

  5. I, for one, welcome our oxygen yielding overlords! by holdenholden · · Score: 3, Insightful
    I say good for NASA. They are finally starting to realize that science can be done outside the government laboratories too. An (academic-type) researcher wastes plenty of time begging for money, writing grants and often balancing a teaching load. In industry, on the other hand, you worry less about budgets and more about what you are trying to achieve and how to achieve it. There is a flip side as well--in academia you are free to work on pretty much anything you like, while in industry you work on whatever your manager wants you to work. In the happy case when your interests and the company's interests coincide, you are only limited by your skills and your knowledge.

    Space One proved that a competition with a good incentive can produce results faster than state sponsored research. I hope the trend will continue.

  6. Zero Gee problems? by Cicero382 · · Score: 4, Insightful

    Has anyone else noticed that zero G is a constant PITA for nearly all space applications?

    A short list includes:

    Human health (bones, muscles, fluid accumulation etc)
    Environment (air flow, hygeine)
    Fluids in general (measuring, pumping)
    Going to the toilet (or john)

    And lots of others.

    I have a question: Why aren't we putting some effort into artificial gravity? I mean centrifuge effects - not Star Trek. After all, we're expending all this effort into individual engineering solutions for each problem. If we had AG of some sort, wouldn't that remove the need for that?

    Just my 2 pennies worth.

    1. Re:Zero Gee problems? by GroeFaZ · · Score: 3, Insightful

      Obviously, the cost-benefit-analysis, at the current state of technology, does not speak in favor of simulated gravity or the engineers would've done it already. Rocket engineers must justify every pound of mass they want to put into space (which is, by the way, an argument against manned space flight), and, while needless to say, it's just a LOT easier and cheaper to let an astronaut pee into a plastic bag and toss it out the window than designing the rocket with 2 huge rotating discs tens of meters in diameter. Ditto for all other points you mentioned.

      If and when our technology has matured enough so we can start designing RAMA-style spaceships or large spacestations with permanent crews of dozens or hundreds, then this or another kind of AG will certainly be included.

      --
      The grass is always greener on the other side of the light cone.
    2. Re:Zero Gee problems? by smilindog2000 · · Score: 3, Insightful

      It's not as bad as people think. You need a long cable, with a good tensile strength to weight ratio. A simple steel cable will do. On one end you attach the space station, which could be as small as a single module of the current space station. The other end needs a weight, supplies, another half of the space station, space junk... whatever. Then you spin the thing. No big deal.

      To dock, you pull up to the middle and grab old of the rotating cable. You then lower yourself down to the station, and enter through a hatch on 'top'.

      I think for long-term living in space, it's a win. For the short term, it adds complexity and cost that nobody wants to pay for.

      It's not rocket science :-D

      --
      Beer is proof that God loves us, and wants us to be happy.
  7. Delivering Fuel by DanielRavenNest · · Score: 5, Interesting

    When I worked at Boeing, I was in charge of a fuel-depot study.
    The method we looked at was a BFG to launch the fuel into orbit.
    The big gun used hydrogen gas that is quickly heated in a heat
    exchanger, then pushes a 600 kg projectile to 2/3 of orbital
    speed. The projectile uses some onboard fuel to go the rest
    of the way to orbit, then delivers the remaining 100 kg of fuel
    to the orbital gas station. The projectile de-orbits and is
    recovered to be reused. The projectile is rugged enough that
    it can land on anything without damage.

    The big gun is very cheap ($100M) compared to electromagnetic
    launchers, because it is basically a length of pipe, compared
    to a series of coils, switches, and big power supplies. On the
    other hand, it is more expensive to operate.

    The velocity split between the gun and the projectile depends
    on the size of the projectile and how much traffic there is to
    orbit. For the case we were studying, delivering fuel to
    carry comsats to GEO, we were launching 100 kg a day, or 30 tons/yr
    (allowing for downtime).

    DRN

    1. Re:Delivering Fuel by rufty_tufty · · Score: 4, Interesting

      Attempt to use BFG to get into orbit - mostly successful, damn politics though.
      http://www.astronautix.com/articles/abroject.htm

      --
      "The weirdest thing about a mind, is that every answer that you find, is the basis of a brand new cliche" -
    2. Re:Delivering Fuel by tarpitcod · · Score: 2, Interesting

      I wonder if it is feasible to fire a solid block of ice (projectile shaped) into orbit. I wonder how much would ablate due to frictional heating. If you use a large enough electrical arc at the base you could use some of the ice of the projectile as the reaction mass.

      The density is obviously lower than liquid water - but theres no throw away / reuse of the casing required.

      Making the projectiles would require freezing water into the projectile form. It may be cost effective to make a larger solid ice projectile and accept the ablative loss.

      If you really want to get serious about space exploration you have to consider the energy density of what your sending. The best use of the ice / water on orbit may be as reaction mass for a nuclear thermal rocket.

      --Tarp

  8. chemical reaction propulsion by zogger · · Score: 2, Insightful

    I doubt there will ever be a cheap/easy/affordable way to do this with chemical reaction rockets. If there was it would have been thunked up by now, doncha think? What you see is what ya get, big ole rockets carrying a relatively small amount of stuff up at great cost.

      We won't become much of a space faring race until we have *advanced physics drives of some sort that work with gravitrons or something along those lines.

    *note:said "advanced". We need to be able to understand and manipulate gravity in some fashion, right now the best we can do is we sort of measure it AFAIK.

    One chemical alternative: wildcard long shot: could we build rockets where the structure (parts of it anyway) of the rocket itself could be transferred to being fuel? A cannibalizing rocket in other words, save a lot of weight that way and get more fuel to orbit.

        This idea is a variation on the "caseless ammo" concept. I saw one of these rifles before that used this sort of ammo, made by Daisy the BB gun guys, it worked perfectly fine, no brass at all. The concept never caught on much, but it worked. So maybe there is a way there to get a lot more fuel into orbit for much less cost than currently. Don't ask me for a detailed chemical composition outline though, no idea, just the concept of cannibalizing rockets.

  9. Re:Orbital Mechanics by solitas · · Score: 2, Informative

    By and large, a change in mass shouldn't affect an orbit - speed and altitude (orbital radius) are interdependent. It would affect drag (atmospheric & from the 'solar wind' - less mass = less momentum so drag would slow it down faster), but that's about all.

    --
    "It's time to take life by the cans." ~ Bender ("Bendin' in the Wind", ep. 3-13)
  10. Not necessarily. by WindBourne · · Score: 2, Interesting

    Assume it is water to be split. First it has easy requirements for storage. Compared to h2 and o2, it is positively trivial to store and work with (in liquid and solid form). 2'nd, this does not need to be shot up there. It could also be shot up an electronic railgun, or a maglev, to get the initial acceleration. It should be possible to get it going into top subsonic and then allow a much smaller rocket to take it up. Nice advantage of this, is that it could be used on a continutal basis for other cargo that is relatively inert to high Gs.

    --
    I prefer the "u" in honour as it seems to be missing these days.
  11. Re:I, for one, welcome our oxygen yielding overlor by susano_otter · · Score: 2, Informative

    Actually, the article summary is a little misleading.

    NASA's role has always been vision, specification, oversight, and operations. Design and construction have always been contracted out to the public sector, and to the universities.

    Classic examples of this method are the Gemini and Apollo projects. NASA's document, Chariots for Apollo gives a fascinating account of how this process works.

    --

    Any sufficiently well-organized community is indistinguishable from Government.

  12. Re:Water? by Larthallor · · Score: 2, Informative

    No, hydrogen is explosive. I'm not sure what neat trick you saw, but I would guess it was likely a decrease in pressure after an explosion caused by two gases combining to become a much denser liquid. In other words the container (attached to a balloon?) contained the explosion and then the water vapor condensed lowering the overall pressure.

    Anyway, one of the reasons why to use hydrogen is that the hydrogen/oxygen reaction has an extremely high specific impulse for a chemical rocket. Here is a Wikipedia link that explains more, but basically it is generally one of the most efficient chemical rocket fuels available.

    Also, of course, it (water) is super cheap, abundant and safe to lift.