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Neal Stephenson On Rockets and Innovation

Dr. Gamera writes "Science-fiction author Neal Stephenson gives us his perspective on the history of the development of rocketry. He uses that history to illustrate the phenomena of path dependence and lock-in."

229 comments

  1. Stephenson & Rocket? by Anonymous Coward · · Score: 1

    For a moment I thought we were back in the 19th Century at Rainhill

    1. Re:Stephenson & Rocket? by sznupi · · Score: 1

      We are, among few things he does is basically hoping for "proper" airplanes from our times (we CAN build them! Take a Harrier, remove wings and canopy ... doesn't make it a good idea) vs. boring reality

      Starting as an ICBM (the first operational ICBM, R-7 Semyorka) doesn't prevent getting "the most reliable ... most frequently used launch vehicle in the world". One of the more inexpensive ones, too... (if anything, efforts at departure away from what physics & rocket equation tells us tended to end ... inefficiently)

      --
      One that hath name thou can not otter
    2. Re:Stephenson & Rocket? by Anonymous Coward · · Score: 0

      Ah the Harrier. Great Aircraft. I worked on the Flight Test line at Dunsfold in the 70's.

    3. Re:Stephenson & Rocket? by Anonymous Coward · · Score: 0

      Why is it OK to make fun of that delusional fantasy but Space Nuttery from the Space Age, that's like a Holy Plan for the human race? It's just as laughable and deluded.

    4. Re:Stephenson & Rocket? by Rei · · Score: 4, Insightful

      Yeah, I was really disappointed by this from Neil. It's extremely poorly done.

      1) "Without the Nazis, rockets wouldn't have happened" -- the Nazis merely accelerated something that was already ongoing. All major nations were working on rocketry. There were two primary purposes: sounding rockets, and aircraft. This was, you'll recall, before we knew that jet engines would win out over rockets for airplane propulsion, and all sides were working on rocket-propelled craft. Even if rocket-plane propulsion were to stop, sounding rocket development would have continued to advance to V2-scale. WWII just accelerated things.

      2) "A-bombs were too expensive and militarily ineffective" --really? Taking out an entire city and its mass production capability isn't worth the cost to purify some uranium? Perhaps if you divide the number of bombs dropped on Japan by how much we spent on the Manhattan project, maybe, but most of that was a sunk cost. The world was terrified of atomic bombings.

      3) "Without A-bombs, rocket development would have ceased." -- ignoring the issues in #1, after WWII, rocketry had already captured the public mind. In fact, even during WWII, Von Braun had already been talking up, and getting military interest in, orbital space bombers that would stay in orbit and drop their (conventional) payloads on enemy targets at a moment's notice (plus taking spy photographs, etc, all without risk of being shot down) during WWII.

      4) "All payloads are sized to be like A-bombs" -- not in the least. There's a huge range of payload profiles and lift capabilities of modern rockets. Just because the stacks were originally designed for a specific load doesn't mean that all of their descendants are.

      Probably the most disappointing line, however, was:

      5) "Rockets are as close to perfect as they're ever going to get." Oh really? Scramjets? Nuclear thermal? Strained-bond chemicals? Cryogenic solids and hybrids? The dramatic materials enhancements we're starting ti get (which has a profound effect on rocket performance)? Advanced heat shields? And on and on. Plus, just ignoring radical changes, look at how much of a difference design approaches have toward launch costs -- compare the Space Shuttle to SpaceX, for example. Rockets are nowhere close to being completely optimized.

      There's a lot of legacy that could be criticized with the space industry, esp. the government space industry. Nobody would insist on keeping on reusing as many shuttle components as possible for a next-gen stack if it wasn't all the jobs on the line. Even the "radical", ground-up redesigns, such as SpaceX's Falcon, still uses some legacy parts. So there is a lot of legacy stuff to criticize. But Neal only skimmed over these things :P And he skipped the most important part of such an article: proposing alternatives. So you don't like rockets -- fine. Let's talk alternatives. What do you like -- skyhooks, space elevators, launch loops, ballistic launch, what?

      --
      I guess I just let my urge to spawn soldiers for Satan's dark army get the better of me.
    5. Re:Stephenson & Rocket? by zrbyte · · Score: 3, Interesting
      It's also worth mentioning here that science and technology has some "Tahrir square moments", that nobody expects. The paradigm shifts and disruptive technologies. 20th century physics and technology is full of these moments. These have the strength to break through the "lock-in". Oh and most of the disruptive ideas etc. have come from the "developed world" of the day. Quantum mechanics and internet? Come on Neal, gimme a break.

      Just another example, regarding the "globalization effect" he's talking about: Thorium based reactors that the US doesn't give a rat's ass about, but may well play a major part in solving the energy crysis and how China is thinking about building them.

    6. Re:Stephenson & Rocket? by sznupi · · Score: 1

      AND, also, it has many elements which don't go away despite wishful thinking (BTW, realizing the conclusions of Michelson–Morley experiment or of some dualities getting into the way of elegant wave theory ... not only brought new possibilities, also new barriers) - our science is, less and less over time, incomplete, not blatantly wrong (which would be required by many of the "alternatives" to rockets)

      Why does Neal want to start with rockets, anyway? Surely calling for new era of ships' hulls which aren't constrained by Archimedes' principle (over two thousand years old! Should be trivial to ignore!) will give much quicker and profound effects - imagine the benefits for existing commerce everywhere!

      --
      One that hath name thou can not otter
  2. "we sing about them at every football game" by Anonymous Coward · · Score: 0

    What the hell is this: "we sing about them at every football game"
    I'm not aware of this... I've been to quite a few Saskatchewan RoughRider games and I haven't heard anyone singing about rockets.
    is this some sort of beer drinking song?

    1. Re:"we sing about them at every football game" by rwven · · Score: 1

      "The rockets red glare, the bombs bursting in air..."

    2. Re:"we sing about them at every football game" by rickb928 · · Score: 1

      They don't do that in Canada. Hey, they just recently stopped singing that God save the Queen. I think. We got past that a couple hundred years ago, though more violently than Canada did. Woops, I'll be darned, they ARE different from us...

      --
      deleting the extra space after periods so i can stay relevant, yeah.
    3. Re:"we sing about them at every football game" by rwven · · Score: 1

      I suppose one must take context into account when rtfa.

    4. Re:"we sing about them at every football game" by Again · · Score: 1

      I suppose one must take context into account when rtfa.

      Let's not get carried away here. He read the RTFA. Let's make sure that he gets credit for that.

  3. designed by a horse's ass... by efraker · · Score: 1

    I suspect you've all seen this e-mail forward, but it was basically what this article reminded me of. http://www.astrodigital.org/space/stshorse.html

    1. Re:designed by a horse's ass... by Anonymous Coward · · Score: 2, Informative

      Yes, we've seen it, as well as the refutations pointing out that the lack of rail standardizations proves it a total fabrication.

      Do try to keep up.

    2. Re:designed by a horse's ass... by ron_ivi · · Score: 1

      Doesn't prove it's a "total" fabrication. It may be the case that just some rail specs descended from horses, and other perhaps from donkey asses, shovel sizes, misread specs or the whims or crazy designers..

    3. Re:designed by a horse's ass... by sznupi · · Score: 2

      Either way it's on the level of "human tools discovered to be close to their creators in magnitude of size!" Well duh...

      --
      One that hath name thou can not otter
  4. That was an interesting opinion -- by Bookwyrm · · Score: 1

    While it is kind of easy to look back along the history of nearly anything complex and cherry-pick things to support a given point, the article raised some interesting points.

    It would be interesting to consider the development of the Internet in the same lines and the subsequent lock-in.

    1. Re:That was an interesting opinion -- by decipher_saint · · Score: 1

      I was going to say, I mean if people weren't trying to set land speed records in rocket-powered cars would Von Braun have been as interested in rocketry at all? Who would be the champion for that technology if there were no little people with big dreams??

      --
      crazy dynamite monkey
  5. Odd, unsatisfying conclusion by smellsofbikes · · Score: 3, Insightful

    It's a neat article, as usual with Neal, but the ending is odd. He says the current state of rocketry is at a local maximum, it's not going to get appreciably better, and there may be other ways of putting stuff in orbit that are better, and then he says he doesn't know why we aren't trying those other better things. This, after spending the previous twenty paragraphs writing about how the US has spent four trillion dollars to get to the top of this local maximum, and the old USSR spent about the same, and in the process we've established a huge military-industrial complex based on the money still flowing into that development path, with lots of political inertia greased by manufacturing and administrative money going into congressional districts... and he wonders why we're not considering spending another trillion dollars on a different, unproven system that would probably involve taking money from the people who are now getting it? He's already answered his own question, and that's surprising because he's a very bright person and does a good job of analyzing the subject.

    --
    Nostalgia's not what it used to be.
    1. Re:Odd, unsatisfying conclusion by rickb928 · · Score: 3, Insightful

      Lemme put it this way. He did edify and inform you enough to come to that conclusion.

      He's brighter than you thought, maybe?

      --
      deleting the extra space after periods so i can stay relevant, yeah.
    2. Re:Odd, unsatisfying conclusion by rwv · · Score: 1

      I think the point of the article is to illustrate that he's pulling his hair out wondering why SpaceX and other up-and-coming space organizations are reinventing the wheel. He's saying rockets are hugely inefficient for moving matter into orbit and you'd get more bang-for-the-buck by inventing something new (i.e. a space plane, a space elevator, or even a simple stairway to heaven).

    3. Re:Odd, unsatisfying conclusion by Thelasko · · Score: 1

      He says the current state of rocketry is at a local maximum, it's not going to get appreciably better

      He's also assuming other fields don't develop new technologies that will benefit rocketry.

      For example, microprocessors have become smaller and more efficient. Did the space industry pay for 100% of this improvement? No, but it did benefit from it.

      --
      One of our competitors trademarked the term "hypothesis". From now on, we will call them "boneheaded ideas".
    4. Re:Odd, unsatisfying conclusion by MozeeToby · · Score: 1

      Yes but the cost is sunk, which is something that I would hope the people in charge of budgets understand. We could throw another four trillion dollars at rocket technology and only get a 20% performance improvement for our money, or you could spend a fraction of that cost to investigate truly revolutionary launch technologies. As much as it pains me to say it, every new rocket, new capsule, new extension to one program or another just takes us farther down a road that does not lead to cheap, reliable human spaceflight.

      Meanwhile other launch technologies are given token funding or less. Imagine if we really and truly decided to put funding towards one (or better yet, several) of the 'non-standard' launch technologies. The problem is that they all appear on the surface to be the realm of science fiction, while in fact could have been developed decades ago if the political will had been there. Nuclear powered rockets, ground based laser rockets, launch loops, sky hooks, and space elevators... the general public thinks these things are impossible, and maybe some of them are, but I for one would be willing to risk a few billion dollars of government spending to find out for sure.

    5. Re:Odd, unsatisfying conclusion by Anonymous Coward · · Score: 0

      So, if you explain why something happens in the short run, it therefore follows, that it must happen in the long run, and forever? His point is that in the past, our society busted through lock ins. We aren't still using whale oil for illumination, fer instance.The discovery of wood-based, and then coal-based gas illumination broke that lock-in without enormous investment, albeit thousands of years after the invention of oil lamps. You'd do better to accuse him of impatience, then try to back that up, rather than as much as state that it's a matter of logic that rockets can't and won't be replaced, ever, or for eons. He actually argued both that lock-in happens easily, and that previously, we were much better at breaking those logjams.

    6. Re:Odd, unsatisfying conclusion by Anonymous Coward · · Score: 1

      What are you comparing rockets to in order to arrive at the conclusion they are "hugely inefficient"? This story is absurd. If someone could create another way to get things into space which is more reliable, in the event of a failure causes less environmental damage, and costs less, it would be done. That is a no brainer in our militaristic greed based world.

      Space Plane is exorbitantly expensive and guess what...uses those "hugely inefficient" rockets to reach space. A space elevator is science fiction. Stairway to Heaven....Led Zeppelin broke up years ago. There simply is no tech out there which can come close to the reliability, efficiency, and costs of rockets. that is why everyone is using them.

    7. Re:Odd, unsatisfying conclusion by dr.newton · · Score: 1

      Not everyone considers loss aversion a fundamental law of nature.

      It doesn't matter how much we spent on that stuff. We should still be doing what makes sense for us here and now.

      --
      Just another proletarian malcontent.
    8. Re:Odd, unsatisfying conclusion by kschendel · · Score: 1

      Yeah, I wasn't impressed. Rockets may be inefficient, but they are a hell of a lot better than anything else we have currently -- at least, anything that doesn't require large quantities of unobtanium. Space elevators are right on the edge of what is maybe barely possible in a few years, never mind the past 50.

      He does mention the key fact about getting to orbit -- the need for a massive horizontal velocity -- but it almost sounds like he doesn't really comprehend the energetics involved.

      He had some valid points about payload sizing, but as far as I know that has been a non-issue for years if not decades.

    9. Re:Odd, unsatisfying conclusion by red_dragon · · Score: 3, Insightful

      It's a neat article, as usual with Neal, and the ending is odd, also usual with Neal.

      Fixed that for you.

      --
      In Soviet Russia, Jesus asks: "What Would You Do?"
    10. Re:Odd, unsatisfying conclusion by amliebsch · · Score: 1

      The thing is he's saying that without presenting any reasons for believing it to be true. It's certainly *possible* that money spent on a space elevator would be more productive than money spent on rockets. It's also possible that it could turn out to be *less* productive. His argument only makes sense if he has actual reasons for believing the former more likely than the latter, but he doesn't present any.

      His argument is about on the same level as someone arguing that you should dump all your money into lottery tickets. It's a no-brainer - so long as we are assuming that you win, of course.

      --
      If you don't know where you are going, you will wind up somewhere else.
    11. Re:Odd, unsatisfying conclusion by necro81 · · Score: 1
      I think you are missing a key part of his conclusion:

      But none of the bright young up-and-coming economies seem to be interested in anything besides aping what the United States and the USSR did years ago. We may, in other words, need to look beyond strictly U.S.-centric explanations for such failures of imagination and initiative.

      He has laid out a good case explaining why the U.S. isn't dumping its investment to start over. What he is wondering about is why no one else is trying it, either. Think of China: they have resources and means to develop something wholly new. But all they are doing is building solid- and liquid-fueled rockets to fling soyuz-like capsules into orbit. Why?

    12. Re:Odd, unsatisfying conclusion by rwv · · Score: 1

      Rockets required bits of "unobtanium" during the 60s. That's why the article points out that $8 trillion was spent between the USA and the USSR. Neal seems to be asking why we continue to pour money into rockets when we can be pouring money into building a space elevator that can carry stuff to orbit at $10 or $100 per pound instead of $10,000 per pound.

      Part of the folly of the Space Transportation System (i.e. Atlantis, Challenger, Columbia, Discovery, and Endeavour) was the it had unexpected maintenance costs that were partly linked to the reliance on the SRBs. The cost-savings of having a reusable fleet was never realized. Neal is saying, "You need to develop a non-rocket-based technology if you actually want to make space travel cheap!!!"

    13. Re:Odd, unsatisfying conclusion by smellsofbikes · · Score: 1
      Well, a quick answer would be that this is an emergent characteristic of evolutionary processes: competition forces everyone to climb the local maximum, and once they're at the top they stay there because they have to. Anyone who tries to go somewhere else has to descend from the top, and that's competitively unsuccessful. So everyone fights for the very topmost spot, forever, or until the entire ecosystem changes enough that it's no longer the local maximum, and at that point everyone dashes for new local maxima.

      In this case, since the entire ecosystem can't really change, we're just stuck, for exactly the reasons he says, until extremely large entities that can afford to be uncompetitive for a long time go looking for another local maximum, and they're not willing to, for, again, exactly the reasons he says. I'm not seeing any mystery here, just a grim outcome of competition and selection.

      --
      Nostalgia's not what it used to be.
    14. Re:Odd, unsatisfying conclusion by tessellated · · Score: 1

      ...but the ending is odd.

      Obviously you haven't read much from Neal; after having read three or four of his novels you come to expect oddness in the endings.

      --
      'When the Going gets Weird, the Weird turn Pro.' - Hunter S. Thompson
    15. Re:Odd, unsatisfying conclusion by amliebsch · · Score: 1

      How so? As Neal himself points out in the article, liquid-fuel rocket technology had already been under development for decades, and the principles and mechanics involved pretty well-understood by the 1960's.

      --
      If you don't know where you are going, you will wind up somewhere else.
    16. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      Neal is saying, "You need to blindly pour tons of money into any fantasy wunderscenario that's pushed around, while forgetting how some of them were seriously looked at again, and again, and again"

      There was nothing unobtanium-like during the 60s about R-7 Semyorka, the first operational (in 1957) ICBM. Which is used to this day as Soyuz rocket, "the most reliable ... most frequently used launch vehicle in the world".

      --
      One that hath name thou can not otter
    17. Re:Odd, unsatisfying conclusion by nomentanus · · Score: 1

      His argument does not assume this. It may assume that the wholesale replacement of fundamental technology in one field doesn't frequently happen from a whole different field, or that that process happens but is slowing. And he's no doubt right on both those counts. Microprocessors have made rockets a bit cheaper and lighter, but they haven't replaced rocket technology in some bizarre way.

      However your argument assumes that there's no lock-in in other tech like microprocessors! I just have to giggle at that assumption. Silicon just by itself is a massive and frequently discussed instance of lock in.

    18. Re:Odd, unsatisfying conclusion by DerekLyons · · Score: 1

      It's a neat article, as usual with Neal, but the ending is odd. He says the current state of rocketry is at a local maximum, it's not going to get appreciably better

      Well, that portion of the article is mostly bunk because the information based it on come from someone with a vested interest in replacing the current system with his own pet system. (I.E. the article is heavily biased out of the gate).
       

      there may be other ways of putting stuff in orbit that are better, and then he says he doesn't know why we aren't trying those other better things.

      Mostly because those 'better things' almost universally aren't once you get past the the power points and down into the actual accounting and engineering. They either a) don't work* like their proponents think they do, or b) require billions upon billions of upfront investment to save the cost of a few hundred thousands of dollars worth of first stage fuel. (In many cases it's both.)**
      Hence the weak and odd ending - he's taken the bunk he's been fed and treated is as gospel truth. When he realizes that reality doesn't match the vision embodied in the input bunk, he treats reality as faulty rather than examining his input and assumptions. (I.E. GIGO.)
       
      * When I say "don't work" I don't mean "requires a bit of R&D", I mean "requires magic pixie dust, unobtanium, and/or repealing the laws of physics".
       
      ** This is the infamous "chicken-and-egg" scenario well known to the intelligent space advocates, it's going to cost a mega bundle to get rockets up to airliner levels of reliability and cost where in theory the resulting demand will justify the investment - but currently the demand is so low there's no reason to make the investment in the first place. This is why so many advocate dubious schemes like subsidized fuel depots - as an artificial demand and an indirect subsidy for launch providers.

    19. Re:Odd, unsatisfying conclusion by suutar · · Score: 1

      It sounds like what he's arguing is that (e.g.) space elevators can yield a big reward, but rockets cannot. Pushing money at space elevators is riskier than pushing money at rockets, but if rockets aren't going to be able to take you where you want to be, what good are they?

    20. Re:Odd, unsatisfying conclusion by holmstar · · Score: 1

      A space elevator is science fiction.

      What's your point? Rockets capable of getting to orbit were science fiction not that many years ago. There are, at least theoretically, materials strong enough to build one, so the rest of the issues are merely technical challenges to work out, but nothing that's impossible. We aren't talking about teleportation or warp drives here. A space elevator is possible with currently conceivable technology.

    21. Re:Odd, unsatisfying conclusion by kschendel · · Score: 2

      "Rockets required bits of "unobtanium" during the 60s."

      Not really. I don't doubt that there were some advances in high temperature materials, but jet engines were driving the same research as well. The stuff in 60's engines were nowhere near the theoretical edge that a hundred thousand kilometer long carbon fiber nanotube is.

      The early rocket engine problems were mostly related to learning about injector voodoo (the F1), the physical properties of liquid hydrogen (RL10 Centaur), and understanding the bearing and sealing issues related to high powered turbopumps (any number of early engine explosions). None of these required anything like the fundamental advances in material science that an elevator will need.

    22. Re:Odd, unsatisfying conclusion by bhcompy · · Score: 1

      You're surprised that something written by Neal Stephenson has an odd, unsatisfying conclusion ? Everything written by him ends that way(and sometimes with statutory rape)

    23. Re:Odd, unsatisfying conclusion by Anonymous Coward · · Score: 1

      http://quicklaunchinc.com/
      http://www.jpaerospace.com/

      http://www.youtube.com/watch?v=1IXYsDdPvbo&feature=related

      Quicklaunch Inc has the physics and engineering worked out to make a 2000% improvement on rocket's Payload Fraction($/kg).

      Spaceguns(light-gas guns) originally fell out of favor because of sonic boom type complaints from locals, and because the G-Forces involved were unsurvivable by humans(but not fertilized embryos...) and because of sonic boom type complaints from locals.

      The first problem doesn't apply towards moving material supplies in to space(water, RP1, other rocket fuels, aluminum etc.) and they've resolved the second problem by putting it in the ocean.

      Robots and Satelites don't mind G-forces nearly as much as fleshbags.

    24. Re:Odd, unsatisfying conclusion by amliebsch · · Score: 1

      Because they do take us where we need to be, today. If the money for Y comes at the expense of X, then *not having X* is a cost of Y too.

      --
      If you don't know where you are going, you will wind up somewhere else.
    25. Re:Odd, unsatisfying conclusion by DarthVain · · Score: 1

      Sounds like yesterdays discussion on molten-salt reactors...

      I'm seeing a theme here... :)

    26. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      There simply is no tech out there which can come close to the reliability, efficiency, and costs of horses. that is why everyone is using them.

      Forgive the adjustment of your comment, but it does serve to underline the point - rockets carry all of their fuel with them. There's no reason why we can't build a gantry several kilometers high which supplies energy to ships to help attain higher speeds as they launch. So for one they start higher, and for another they start faster. Maybe that will only be a significant factor in getting to LEO, but from LEO you can go much farther a lot easier. Make the trip to LEO easier, and the whole thing becomes a lot simpler and cheaper. Like a staging post.

    27. Re:Odd, unsatisfying conclusion by Rei · · Score: 3, Interesting

      Even in theory, "maybe". The strongest single SWNTs measured thusfar are just over 60GPa, a far cry from the predicted 120+ GPa. That may sound like a small difference, but the taper factor means that's a geometric increase in the mass of a space elevator; you really need at least 100GPa for the bulk fiber for it to be even worth consideration. And that's for *bulk fiber*, not for individual tubes, which are always going to be a lot stronger than a bulk fiber.

      Plus, space elevators have all sorts of other problems -- inefficient power transport, slow transit times and thus throughput, major undampened oscillations, and on and on. Launch loops are a much better choice in pretty much every regard, and could be built with today's materials and technology. Oh, sure, they're not as glamorous, not as much a staple of sci-fi. But that doesn't change what's the best way to get into space.

      --
      I guess I just let my urge to spawn soldiers for Satan's dark army get the better of me.
    28. Re:Odd, unsatisfying conclusion by mosb1000 · · Score: 1

      There's no reason why we can't build a gantry several kilometers high which supplies energy to ships to help attain higher speeds as they launch.

      I can think of a couple reasons.

    29. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      Science fiction was riddled with spaceplanes. Rockets...not so much.

      --
      One that hath name thou can not otter
    30. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      what's the best way to get into space

      How can you know that?

      Did the Shuttle deliver on even one of its main points, as advertised? How are we along with building megastructures?

      --
      One that hath name thou can not otter
    31. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      Few km of height is largely insignificant, else you would see spaceports on major highlands; a launcher works primarily horizontally, for speed - and tower could provide very little of that (remember there's a square in kinetic energy...)

      In fact, we already have a launcher which does more than your fantasy could ever accomplish - Pegasus rocket (check it out). It is one the least cost efficient launchers around.

      Please, drop the wishful thinking.

      --
      One that hath name thou can not otter
    32. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      Why isn't he pulling his hair out wondering about automobile manufacturers unwilling simply drop the wheel? Where is my flying car?

      --
      One that hath name thou can not otter
    33. Re:Odd, unsatisfying conclusion by lennier · · Score: 1

      or even a simple stairway to heaven

      I'd start with some kind of zeppelin technology, possibly augmented with light emitting diode propulsion.

      --
      You are not a brain: http://books.google.com/books?id=2oV61CeDx-YC
    34. Re:Odd, unsatisfying conclusion by lennier · · Score: 1

      He has laid out a good case explaining why the U.S. isn't dumping its investment to start over. What he is wondering about is why no one else is trying it, either. Think of China

      Didn't he also answer that in the first part of the article, though? He spent a number of paragraphs to remind us that there's nothing actually worth spending money going into space for, except for communication satellites, the market for which in geosync is limited by the number of orbital slots which are now full, and which cost tens of thousands of dollars per pound in engineering for the extreme environment of space without even considering the particular launch method.

      So to sum up: there's no expected commercial payoff for expandede access to space, it cost $4 trillion and the threat of a civilisation-ending war for rockets to enter the market, it might conceivably cost as much for alternative launch methods to get there... so what's the point of the article again?

      tldr: space $ = comsats, but we already have enough comsats kthxbye

      or is he saying we need more comsats? or there might be magical other things we could do in space if only we didn't need rockets to get there? But he never gets to saying what those might be.

      --
      You are not a brain: http://books.google.com/books?id=2oV61CeDx-YC
    35. Re:Odd, unsatisfying conclusion by Rei · · Score: 1

      1) Does the Shuttle that was actually produced remotely resemble the Shuttle that was being proposed at the time?

      2) One can only make decisions based on the current known body of evidence. Which is that space elevators are not a reasonable thing to pursue in contrast to actively-suspended structures such as launch loops.

      --
      I guess I just let my urge to spawn soldiers for Satan's dark army get the better of me.
    36. Re:Odd, unsatisfying conclusion by Mike610544 · · Score: 1

      Maybe it will take him some time to lose that reputation, but his latest novel Anathem had an ending like an 80s John Hughes movie.

      --
      ... also, I can kill you with my brain.
    37. Re:Odd, unsatisfying conclusion by Eivind · · Score: 1

      50.000 :)

    38. Re:Odd, unsatisfying conclusion by Yoozer · · Score: 1

      Why isn't he pulling his hair out

      He appears to be bald already.

    39. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      Few km of height is largely insignificant,

      11km of height is quite significant, I assure you.

      else you would see spaceports on major highlands; a launcher works primarily horizontally, for speed - and tower could provide very little of that (remember there's a square in kinetic energy...)

      The tower doesn't need to point straight up. Do take a look at this http://yarchive.net/space/exotic/tower_launch.html

      In fact, we already have a launcher which does more than your fantasy could ever accomplish - Pegasus rocket (check it out). It is one the least cost efficient launchers around. Please, drop the wishful thinking.

      Please learn the difference between realism and dogmatism. ;)

    40. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      Can you have a read of this first http://yarchive.net/space/exotic/tower_launch.html

    41. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      And why do you think 1) might be the case, hm? (do our airplanes resemble this wishful thinking?) You really don't see, "ahh, this is the way, it will be great!" analogies? Where are any actively suspended buildings?! (nvm of a scale of megastructures)

      --
      One that hath name thou can not otter
    42. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      So? 11km is in the range of Pegasus launch (did you bother to check?) Even inclined track (not simple tower anymore!) is unlikely to surpass a jetliner at speed...

      --
      One that hath name thou can not otter
    43. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      The pegasus is also mentioned in that link I supplied, which is from 1996. Also I didn't say it should be a simple tower ("which supplies energy to ships to help attain higher speeds as they launch"), I was thinking more an evacuated maglev rail tube of some sort, supplied by electric on the ground level, which is vastly cheaper than rockets. Again, have a good read of that link, there's plenty of technical information in there too.

      The only currently-flying exception to this is Pegasus, a very small booster that's light enough to carry on an airplane. Even that was only feasible because an existing airplane (NASA B-52) was already configured to carry similar-sized rockets (X-15), thus saving development costs.

      Despite this, even a few km can supply a quite respectable advantage, and that's before you start powering anything.

      Some of the advantages of high-altitude launch:
      (1) You start with a fraction of the potential energy needed to get to
      orbit.

      If you could launch at 10000 ft above sea level, you could reduce
      your velocity change to get into orbit by approx. 250 m/s. However, you
      need about 8000 m/s to get into orbit. A 3% improvement.

      But three percent is a *tremendous* improvement. A RL-10A has an Isp of
      about 450 seconds; thus, exhaust velocity Ve is about 4400 km/sec.
      Structure & payload mass fraction is exp[deltaV/Ve]; a RL-10A powered
      vehicle could achieve a maxium amount of structure plus payload to 8
      km/sec of 16.3%. Typically about 5% of this is actually payload. A 3%
      decrease in delta-V to orbit increases this to 17.3%. This increases the
      *payload* to 6% of the gross lift-off mass -- a 20% increase in payload.

      (2) You start at a lower atmospheric pressure.
      a. reduced atmospheric drag loss

      Which wasn't commented on by Bromley or by Pat, but is a significant
      effect, at *minimum* equal to the potential energy gain.

      b. vehicle can be designed with less attention paid to
      aerodynamics. Lower aerodynamic design penalty means higher performance
      designs (ie., smaller fineness ratio allows more efficient tanks)
      c. More optimum trajectory possible; you can curve toward
      horizontal thrust much faster since you start out closer to out of the
      atmosphere
      d. Max-Q occurs at a much lower pressure; lower aerodynamic
      stress on the system means vehicle can be designed lighter.

      Pat, prb@clark.net commented on this one:
      I think Max-Q is going to be at the same altitude or lower depending
      upon tank fineness.

      To the contrary. Max-Q is the product of air density, the square of
      velocity, and a vehicle-dependent factor which depends on mach number.
      For a given acceleration profile, Max-Q occurs at the same altitude
      *above the launch site* independent of how high the launch site is. That
      is, the actual value of dynamic pressure will decrease linearly with the
      initial pressure.

      True, if you decrease the fineness ratio to gain tank fraction, you will
      then increase the Max-Q again. This makes the whole thing an engineering
      trade-off-- how much do you gain in tank fraction and robustness, versus
      how much of the decrease of Max-Q do you lose? Doing such trade-offs is
      why we pay engineers.

      However, I don't have a good number which tells me how much of the
      structural mass is due to making the vehicle robust to survive Max-Q.
      Anybody have a guess?

      e. Aerodynamic vibrations lower; allows less robust payload
      (e.g., lighter)
      f. Wind loads on vehicle in flight much lower
      g. Acou

    44. Re:Odd, unsatisfying conclusion by sznupi · · Score: 2

      "Evacuated maglev rail tube of some sort"? "Vastly cheaper than rockets"? You... are not joking? Oh my...
      Do you see anything comparable in operation?... (nvm large masses, high accelerations, huge energies involved if the maglev payload is a rocket, nvm "popping" the tube...)

      The "tremendous improvement" they talk about is merely at the cost of quite possibly not practical, one of a kind megastructure. Forming with the rocket a potentially quite problematic, high-speed dynamic system during launch.
      Vs. having the same gain for just somewhat enlarging the first stage (also via quite straightforward "multiplication" of it, what Delta IV Heavy sometimes does, what Angara will do to an even larger extent), continuing to use simple launch facilities and decently easy, at this point, procedures. On a static platform.

      You provide great examples why "dumb rockets" do remain attractive (and remember, people similarly enthusiastic about their dreams - even people from the same institutions - gave us the Shuttle; it also had great advertising before the reality set in)

      --
      One that hath name thou can not otter
    45. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      Do you see anything comparable in operation?... (nvm large masses, high accelerations, huge energies involved if the maglev payload is a rocket, nvm "popping" the tube...)

      And this is why imagination is a basic requirement for advancement. As it turns out, engineers are working on one right now. http://en.wikipedia.org/wiki/Vactrain A mere century ago the idea of a network of high speed passenger airliners with the capacity we have today would run into the very same objections you raise here, large masses, high accelerations, huge energies involved, never mind popping the tube at high altitudes, etc.

      The "tremendous improvement" they talk about is merely at the cost of quite possibly not practical, one of a kind megastructure. Forming with the rocket a potentially quite problematic, high-speed dynamic system during launch.

      All of which is well within the boundaries of today's engineering. Heck, most of it was within the boundaries of engineering two decades ago, at least. And what a project, the first true spaceport! My god, what a project, no one country could manage it, you'd need international co-operation on a massive scale, will, impetus, a route laid out for longer term benefits, it would be a thing of awe and splendour. The biggest difficulties you would face would be political to be honest, but thats a matter of simply convincing enough people, and spread out over a large enough population, the per capita investment costs wouldn't be too serious. Probably less than the US spends in a few years on the military.

      Vs. having the same gain for just somewhat enlarging the first stage (also via quite straightforward "multiplication" of it, what Delta IV Heavy sometimes does, what Angara will do to an even larger extent), continuing to use simple launch facilities and decently easy, at this point, procedures. On a static platform.

      The bottom line is, right now, they cost too much, way too much. This is a means to significantly reduce the unit costs for payload, and hence open the road to the sky above us. If it was as cheap to ship cargo/facilities/people to orbit as it was to ship them across the oceans, we'd alread have orbit well colonised, and be taking advantage of the near limitless resources of space.

      Build this, build LEO fuel and resource dumps, build a proper station and refinery up there, build drones to assay near earth resources, build extractors to bring back those resources or produce them on-site, ship the raw materials back to orbit and produce finished goods, drop them down or use them to build out even more infrastructure, and so on. You could ultimately outsource most of the industrial heavy lifting to orbit, along with food production and a lot more. I appreciate this is a long term plan, as in a couple of centuries, but if you don't get started you won't get finished, and what a world we'd have then.

      You provide great examples why "dumb rockets" do remain attractive (and remember, people similarly enthusiastic about their dreams - even people from the same institutions - gave us the Shuttle; it also had great advertising before the reality set in)

      In fairness the shuttle was changed considerably from its initial specifications, it is the definition of "designed by committee".

    46. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      The issue that you, for some reason, do not see is that your maglev tube would require everything a typical rocket and its launch already does. EVERYTHING! And MUCH more (plus - first demonstrate the viability of underlying concept in a monumentally more simple application, then ...wait, not even then can you start promoting it as some wundersolution in quite different scenario!)

      Also, real world does have practical limits and wishful thinking doesn't take them away. It didn't with the Shuttle, when we "really, really wanted it" (why do you think it's unlike the spaceplanes from works of fiction?! (on which its designers, also of early "specifications", were undoubtedly raised...) But even those, when thoroughly looked at by actual physicists and engineers - HOTOL, for example - turn out not really better, in best(!) case scenario, than a "dumb rocket" using comparable materials science ... one which we don't even have, and which a spaceplane requires to be even barely doable)

      --
      One that hath name thou can not otter
    47. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      The issue that you, for some reason, do not see is that your maglev tube would require everything a typical rocket and its launch already does. EVERYTHING! And MUCH more

      So? We're talking about putting pylons 11km into the air. At no point did I say this was something that could be done by a hobbyist with a lathe. All of the basic principles are well established, and indeed in use at the moment. Adjusting them and scaling them up is by no means impossible, to say nothing of inconceivable.

      first demonstrate the viability of underlying concept in a monumentally more simple application, then ...wait, not even then can you start promoting it as some wundersolution in quite different scenario!)

      http://www.youtube.com/watch?v=i1q_rRicAwI&feature=related

      http://en.wikipedia.org/wiki/Vactrain

        http://www.youtube.com/watch?v=IPduAYKk_6I

      Also, real world does have practical limits and wishful thinking doesn't take them away. It didn't with the Shuttle, when we "really, really wanted it"

      Sorry, at this stage you're just dragging your heels and saying "nuh-uh". For once will you please rtfa.
      http://www.therefinedgeek.com.au/index.php/2009/09/03/space-shuttle-reusable-craft-by-committee/
      The shuttle was a bad fit for everything because it was designed by committee. That doesn't mean the basic concept was wrong or mistaken, or even impossible. Really at this point I'm going to bookmark this conversation to use in further discussions on why dogmatism has replaced imagination and creative thinking.

    48. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      This is your style of imagination (if you are really capable of asking "so?" when faced with how your pet fantasy would require EVERYTHING, but with much tighter tolerances for error, than what it's meant to "replace" ... plus a megastructure of doubtful practicality even in easiest of conditions), airplanes from "our" times (and we CAN even build them! Take a Harrier, remove wings and canopy ... doesn't mean it's anywhere near a good idea) - vs. boring reality

      But please, do link to this discussion, it might help some other seekers of philosopher's stone.

      --
      One that hath name thou can not otter
    49. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      This is your style of imagination (if you are really capable of asking "so?" when faced with how your pet fantasy would require EVERYTHING, but with much tighter tolerances for error, than what it's meant to "replace" ... plus a megastructure of doubtful practicality even in easiest of conditions), airplanes from "our" times (and we CAN even build them! Take a Harrier, remove wings and canopy ... doesn't mean it's anywhere near a good idea) - vs. boring reality

      Yeah, you've descended into abuse now. Here's what's really happened: you've come across a concept, which I supported with technical discussions, real world examples, and a variety of articles, which is far outside your comfort zone, as in that area where you feel the real world exists and can be controlled, a conservative place where nobody steps too far out of line.

      You responded to this intrusion by raising nonsensical objections (the space shuttle? really?) and ignoring the facts presented to you, dancing around your intuition that this all must be somehow against the laws of physics or something, which puts you right in the same ballpark as creationists and flat earthers.

      With the best of intentions I say it is this kind of knee jerk counter-rational dogmatism, inspired by a misunderstanding of what science actually does to advance, that is strangling innovation and creativity, and it would appear Mr. Stephenson agrees with me.

      But please, do link to this discussion, it might help some other seekers of philosopher's stone.

      Indeed I will.

    50. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      Mr. Stephenson is an author of literary fiction. But how you are convinced only those few precious brilliant engineers have the right solution, in how long writings you're willing to glorify them, how you stepped back to claiming you're victim of some sort of "abuse" by reality, is another telltale sign.

      Heck, even how you fail to notice / are unwilling to strongly point out (lest it puts your pet fantasy in bad light?... I waited few enough posts) the basics of such megastructure, literally aiming only for a very narrow range of inclinations.

      --
      One that hath name thou can not otter
    51. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      Wait, wait... you seriously think those are "simple applications" of the concept?... or any kind of application, for that matter?

      --
      One that hath name thou can not otter
    52. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      Mr. Stephenson is an author of literary fiction. But how you are convinced only those few precious brilliant engineers have the right solution, in how long writings you're willing to glorify them, how you stepped back to claiming you're victim of some sort of "abuse" by reality, is another telltale sign.

      Not abuse by reality, abuse by you, linking to a page containing some sort of mad air display and calling it my imagination. This is personal abuse, intended to create insult, which is a far cry from actually dealing with the detailed technical information which was actually put before you. This can go round in circles for as long as you desire to get the last word in, so if you've nothing constructive to add we'll draw a line under it.

      Heck, even how you fail to notice / are unwilling to strongly point out (lest it puts your pet fantasy in bad light?... I waited few enough posts) the basics of such megastructure, literally aiming only for a very narrow range of inclinations.

      So you didn't bother to read the tower launch discussion page then.

    53. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      The issue is, you glorify it, you forget to mention basics which nullify hypothetical advantages and go even more against practicality.

      Even your nickname seems to be determined by such fantasies ... and you're trying to pretend to not be heavily emotionally invested, under wishful thinking, perhaps even blindly in awe of those few shining beacons of an engineer?

      --
      One that hath name thou can not otter
    54. Re:Odd, unsatisfying conclusion by Intrepid+imaginaut · · Score: 1

      practicality.

      You keep using that word. I do not think it means what you think it means.

      Even your nickname seems to be determined by such fantasies ... and you're trying to pretend to not be heavily emotionally invested, under wishful thinking, perhaps even blindly in awe of those few shining beacons of an engineer?

      I see you've been at this with other posters on the thread as well, including Rei. At some point you must realise, if people stop arguing with you, it doesn't mean you've won, it means you're all alone.

    55. Re:Odd, unsatisfying conclusion by marcosdumay · · Score: 1

      I don't know why we should concentrate on only one of the alternatives. But if so, yeah, I'd vote for launch loops that use rockets for the latter stages.

    56. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      I certainly agree it means different thing to you (might not to such a degree to Rei - so unfortunately, you haven't found sufficiently like-minded poster, not to mention the issue of persecution complex... either way, probably different pet projects; luckily, that's not enough to bring us into (too many...) train-wreck projects of wishful thinking)

      --
      One that hath name thou can not otter
    57. Re:Odd, unsatisfying conclusion by mosb1000 · · Score: 1

      I was gonna say cost. . .

    58. Re:Odd, unsatisfying conclusion by Rei · · Score: 1

      IT's not "why I think" 1). There's a well documented history of the Shuttle out there which you've apparently never read. The Shuttle had its budget basically slaughtered due to the Vietnam War (plus rate of payloads for it to launch as well; frequent launches are required of reusables for economic viablility). They were forced to make a ton of compromises which significantly increased its operating cost, and even that wasn't enough to get back into budget, so they had to beg the Air Force for money. The Air Force imposed a bunch of new requirements on it which further ruined its economic viability.

      Explain how exactly that applies here.

      --
      I guess I just let my urge to spawn soldiers for Satan's dark army get the better of me.
    59. Re:Odd, unsatisfying conclusion by tabrnaker · · Score: 1
      I don't know anything about the equations involved but was wondering.

      What is the efficiency point for 'rail gun' size, energy expenditure, and weight of payload?

      If payload size is large enough say, 100k, couldn't we just design some aerodynamic capsules, give them some whale fins, slap on some shark skin texture on the outside. Line up the rail gun with whatever magentic fields are in the area (every little bit helps right) and then just shoot payloads and have a mechanism or plane catch the payloads at the top of their trajectory and take them the rest of the way to a space station. assuming of course that it would be possible to launch something high enough that the mechanism or plane is in some sort of non-decaying orbit.

    60. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      You asked somebody who chooses to not bother with the equations... but for whom "intrepid imagination" seems crucial.

      (generally, the simplest ~Newtonian equations for speed after acceleration, kinetic energy, work required give some large scales (last time I toyed around with the calculations, it looked practical enough for a very small projectile; and a track of preferably at least two dozen km, in the style of V-3 cannon), like coupled with few dozen km "aerial maglev" (start to see the problem?); "non-decaying orbit" is just... orbit - there's no "catching" at multi-km/s approach velocities, look at relative speeds of tanker and fighter when coupling / decoupling during aerial refueling ... even when landing on a carrier, or even when using Fulton, the speeds are still negligibly slow; it's not even about equations, not even wrong ... as far as wondering goes, our capabilities have very few limits - but that isn't carried over to RL)

      --
      One that hath name thou can not otter
    61. Re:Odd, unsatisfying conclusion by sznupi · · Score: 1

      Below you've demonstrated you have no idea (or choose to have "no idea", choose to invent "problems" for approaches which might possibly get in the way of your pet ones) about the absolute basics of rocketry, indeed of Newtonian physics... that's not a good position to start lecturing me about history of the field.

      Especially if on the basis of "we would be awesome, we promise! It was just this pesky reality..." - STS history is full of such promises (but if you'd want something even more wild... if you think how something more expensive and complex to develop would do the trick - lowering costs was supposed to be the point, that includes development costs; don't treat reality which hit as some unfortunate circumstance) Or we might look at another piece - when Soviet engineers (vs. politburo) were saying "no way in hell we want to build something like it" (opting instead for small lifting body launched as a dumb payload ... that's basically even how they did their shuttle, when pushed)

      Nicely applies to HOTOL (or every other spaceplane which was looked at rigorously), with marginal gains at best (for a cost). Even better to dynamically suspended megastructures (current body of evidence supports them, really?). Putting a blind eye on practical side of things was the problem.

      --
      One that hath name thou can not otter
  6. Definition of path dependence and lock-in by Anonymous Coward · · Score: 0

    Funny, that the article fails to define the two concepts that its supposed to illustrate. Bad (popular) scientific writing. I would not have expected this from someone who supposedly knows how to write (albeit fiction).

  7. Wow that was just bad. by LWATCDR · · Score: 1

    Really that was just really bad. Satellites have never been "limited" to the size and weight of Hydrogen bombs.
    Frankly it was just some kind of odd ramble that had no real facts at all. The History was also just dumbed down to about the level of a fourth grade book report.

    --
    See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    1. Re:Wow that was just bad. by Anonymous Coward · · Score: 0

      have you read his books ... it is the same at least they are aptly named. The Confusion ... INDEED

    2. Re:Wow that was just bad. by urusan · · Score: 1

      Really that was just really bad. Satellites have never been "limited" to the size and weight of Hydrogen bombs.

      Except that's not really what he said...the very next paragraph elaborates on this point.

    3. Re:Wow that was just bad. by rickb928 · · Score: 1

      He's right, you're wrong. Satellites are limited to the capacities of the launch vehicles available, and those vehicles were designed for the bombs. Or the bombs aer designed to the limitations of the vehicles. Same problem for satellites, though they didn't drive vehicle development until fairly recently. Even now, it's as much packaging as rocket that limits satellite design. The USAF seems pretty interested in the X-37 to deliver military satellites, and I wonder how big the

      Delta/Thor rockets are still very popular for satellite launches, and are the result of the PGM-17 program, the USAF Intermediate-range missles. Replaced soon by Atlas rockets. We know these well as the launch vehicle for various space probes and Mercury capsules.

      Personally, I would have never gotten on top of a Redstone for even a suborbital test, but then again, IANATP. Al Shepard deserves a cookie for that. Grissom, of course, blew the hatch and screwed the pooch, allegedly, though expecting that thing to float seems optimistic in hindsight.

      --
      deleting the extra space after periods so i can stay relevant, yeah.
    4. Re:Wow that was just bad. by sznupi · · Score: 2

      May I introduce you to the International Space Station - an artificial satellite of a mass greatly exceeding capabilities of any launcher (and before the inevitable: no, it's not simply a fiction of rocket limitations - we build even ocean going ships in segments nowadays; modularization and, eventually, mass production, is simply a very good idea)

      And FYI, the new toy of USAF, X-37, is launched by "dumb rocket" (with Russian main engine...); it's a "spaceplane" mostly because of its envisioned niche usage scenarios, so it can afford wasting most of its mass for airframe.

      --
      One that hath name thou can not otter
    5. Re:Wow that was just bad. by rickb928 · · Score: 1

      The ISS is a satellite, but launched in pieces that fit on rockets or in the Shuttle.

      Nice try, though. Somehow, limitations of launchers still prevails. Until we develop better space construction techniques, we're stuck.

      --
      deleting the extra space after periods so i can stay relevant, yeah.
    6. Re:Wow that was just bad. by maxume · · Score: 1

      You're dangerously close to pointing out the exception that proves the rule.

      Sure, the multi-billion dollar government research platform is modular, but where are all the modular commercial satellites?

      --
      Nerd rage is the funniest rage.
    7. Re:Wow that was just bad. by sznupi · · Score: 1

      Don't ignore the possibility of other limiting factors and/or how larger satellites are not needed for most scenarios. Generally, we are not using the heaviest rockets around to launch commercial satellites.

      Heck, even quite average launchers are often used to put more than one satellite into orbit.

      --
      One that hath name thou can not otter
    8. Re:Wow that was just bad. by ISoldat53 · · Score: 1

      Just like his books then.

    9. Re:Wow that was just bad. by cowboy76Spain · · Score: 1

      The missiles were designed for intercontinental flight... launching a manned capsule to the moon requires way more thrust.

      Of course, technology designed for missiles was useful when building space rockets, but there is more to it.

      Also, I find the assumption that "had not been than the URSS was ruled by a dictator, there would have been no weapons arm race". Nonsense. The second comer is always the next adversary, let it be military or economically. Even UK and France, being allies to the USA, chose to develop their nukes in order to mantain some autonomy. And yes, probably they had help from the USA, but that was offered only because the URSS was the great danger.

      --
      Why can't /. have a rich-text editor? Editing your own HTML is so XXth century.
    10. Re:Wow that was just bad. by sznupi · · Score: 1

      ...and ISS modules don't hit the limits of current launcher technology. We are well on our way to the most sensible approach to construction (seriously, how did you miss that was the point? W8, you don't mean physical fit, don't think other methods could be much less streamlined, right? Transporters?...)

      --
      One that hath name thou can not otter
    11. Re:Wow that was just bad. by sznupi · · Score: 1

      If one looks at early days of Manhattan project (and slightly before it), it's a bit less clear regarding who got help from whom. Or when checking out Miles M.52 aircraft, in relation to Bell X-1.

      --
      One that hath name thou can not otter
    12. Re:Wow that was just bad. by maxume · · Score: 1

      The quote in the article (about satellite size and H-bombs) is about the existence of ICBMs dramatically lowering the start up costs of the early satellite launchers, not about weapon sizes dictating launch capabilities throughout the history of space flight. So we have gone a bit off the rails. The part where the weapons development absorbed much of the costs is quite obviously true, the discussion about the primary driver of greater lift capability is somewhat muddier, but it seems to me that National pride projects (mostly launching humans) have been the big source of funds.

      --
      Nerd rage is the funniest rage.
    13. Re:Wow that was just bad. by RockClimbingFool · · Score: 1

      What about modular systems?

      Directv, GPS, Iridium? Are you going to say those don't count because they aren't physically connected?

    14. Re:Wow that was just bad. by BJ_Covert_Action · · Score: 1

      The Delta and Atlas rockets used today pretty much only share the name of their predecessors. I am not sure there is a single piece of technology on either of the current vehicles that was employed by their original programs, or, hell, even their predecessors two generations removed.

    15. Re:Wow that was just bad. by maxume · · Score: 1

      I would say they don't count because they aren't modular systems due to launch mass restrictions, they are modular because that is the sensible way to get good geographic coverage.

      --
      Nerd rage is the funniest rage.
    16. Re:Wow that was just bad. by jfp51 · · Score: 1

      You are correct that the UK and France have their own nuclear arsenal but the way they went about it was completely different. The UK is tied much more closely to US nuclear bomb technology because the US licenses the design to the UK. Of course, the UK maintains launch authority for their warheads. France, on the other hand, developped their nuclear weapons systems from scratch and are completely independent from the US from a manufacturing perspective.

    17. Re:Wow that was just bad. by rickb928 · · Score: 1

      The seeds of the US v USSR conflict were sown at the end of WWII, specifically in Berlin, with some of the war spoil controversies thrown in. Stalin was prepared to finish what Hitler started, but alas, that didn't work out. Or maybe it did.

      --
      deleting the extra space after periods so i can stay relevant, yeah.
    18. Re:Wow that was just bad. by LWATCDR · · Score: 1

      He is right about what? We have to find something better than rockets?
      First the Delta4 has nothing in common with the Thor/Delta of old except the name. The same is true of the Atlas V/
      Also the Atlas and Thor where in service at the same time. Thor's in Europe and the Atlas here in the US.

      If you really read the what he wrote it simple said that satellites are the way they are because launchers are the way they are and then adds in a good mix of bad details and fantasy. Well duh....
      The rest of it was just rambling. Or if you are a big fan of science fiction what we really need are some General Products hulls with hyper drive and Outsider gravity drives like the Puppeteers are using to move their home world. Too bad we don't have the CAD files for those.

       

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    19. Re:Wow that was just bad. by rickb928 · · Score: 1

      My interpretation is that thor, Delta, Atlas, Saturn, Ares, they are all essentially vertical launchers. If I could wave a wand and throw money at it, I would like to see something like a real plane, but spaceworthy

      --
      deleting the extra space after periods so i can stay relevant, yeah.
    20. Re:Wow that was just bad. by Rei · · Score: 1

      SSTO spaceplanes require either radical improvements in materials or solid improvements in ISP to become a reality. The latter case means either airbreathing (scramjet), metastable/strained bond fuels, or other propulsion methods such as nuclear.

      --
      I guess I just let my urge to spawn soldiers for Satan's dark army get the better of me.
    21. Re:Wow that was just bad. by LWATCDR · · Score: 1

      "If I could wave a wand and throw money at it, I would like to see something like a real plane, but spaceworthy"
      yea but until we get magic or a major breakthrough in materials and propulsion that is what we have. The X-33 showed promise but problems with the composite propellant tank killed it. "BTW they had done on an AL tank that would even lighter but they killed it anyway."
      So as I said a bunch of bad history, miss informed opinion and rambling. So no I was not wrong and he is right only in the simple statement that it would be really cool to have cheap access to space and big dumb boosters will not provide that.
      Which is nothing but a big duh... That was the idea behind the Shuttle in the late 60s early 70s. Thing is that they built the Shuttle but didn't build the space tug, space station "until the ISS", and many of the other projects that the shuttle was supposed to support. That and they changed the design to make the development cheaper but the per flight higher.
       

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    22. Re:Wow that was just bad. by rickb928 · · Score: 1

      I'm not so much focused on 'cheap access to space', as in reliable, faster turnaround, reusable. I don't think we can do that with the current model of vertical lift, aka Shuttle/Thor-Delta-Ares-etc, but if a true Shuttle replacement could be launched more horizontally, this might solve the problem of big rockets pushing things straight up (at first). That demands big motors and big fuel burn rates.

      I know, we need materials and propulsion advances. Similar problems in transportation, especially passenger cars, and we are playing with batteries as an interim step towards other energy sources. Not directly applicable to space travel, but similar fundamental problems - changing the paradigm.

      It takes vision and committment. Both lacking in our nation and government.

      --
      deleting the extra space after periods so i can stay relevant, yeah.
    23. Re:Wow that was just bad. by LWATCDR · · Score: 1

      Wow I guess you really have no real grasp.
      Let me put this simply. reliable, faster turnaround, reusable == cheaper.
      Unless you build a stupidly gold plated system.

      "Similar problems in transportation, especially passenger cars, and we are playing with batteries as an interim step towards other energy sources. Not directly applicable to space travel, but similar fundamental problems - changing the paradigm."

      All of of the problems are bounded by chemistry, physics, and material science. You know that harsh thing called reality.
      Actually vertical take off for a space may not be a huge penalty. With a horizontal takeoff you must support the weight of the fuel on the landing gear which is a separate weight structure from the thrust bearing structure since one will be taking a horizontal load and one the vertical load. Since the thrust load will be large to start with to get into orbit Then add in the lifting surfaces that will be needed to left the weight of the massive fuel load which will then be nothing but dead weight when landing. Then the wing spar needed which will be another massive structure adding even more to the weight. Which will add more to the weight of the landing gear which will mean more fuel which will mean more load on the spar, more wing area, and.....
      It only makes sense if you vastly decrease the fuel fraction AKA a large increase in specific impulse over the what we now have. The problem there is Hydrogen has the best power to weight ratio. There are other trade off fuels where you can have a denser fuel so you save weight on the structure by adding some to the fuel like by going with CH4.
      That is why a SCRAM jet makes so much sense since you will not need to take as much oxidizer with you if any. But those do not work at zero airspeed so then you must have some way to get them up to speed. Then since you do not have to carry all that LOX the math gets better.

      So yes it was all a bunch of Duhh.... Jibberish, bad history, ,uninformed opinion, and fantasy.
      There are other trade offs like air launching like the Pegasus and Rutan is doing. There you are using an airplane as a reusable first stage.
      The problem there is that there are few large aircraft that suitable to air launch a large rocket. You could build a folding wing system and then use a druge to extract a larger booster from the back of say a C-5.
      But simple truth is that a lot of really smart people are working really hard on this problem. It is just insane that this rambling mess of a document got any attention at all. The only reason is the author because the content was just terrible.

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    24. Re:Wow that was just bad. by rickb928 · · Score: 1

      "Wow I guess you really have no real grasp.
      Let me put this simply. reliable, faster turnaround, reusable == cheaper."

      Wow, I really do have a grasp. Thanks for restating the obvious.

      "With a horizontal takeoff you must support the weight of the fuel on the landing gear which is a separate weight structure from the thrust bearing structure since one will be taking a horizontal load and one the vertical load."

      I think this is a common problem for all aerodynamic vehicles, isn't it? We've done some good work in that area if I recall.

      "Then add in the lifting surfaces that will be needed to left the weight of the massive fuel load which will then be nothing but dead weight when landing."

      Are you describing the Shuttle again? Is that a good model for future spaceflight? Just asking. ps - 'dead weight' when landing decribes an entire vehicle, if you're pointing out that lifting surfaces are 'dead weight'. Like landing gear. What? So capsules are the most efficient vehicle, right? Are they the most useful? Is there a difference?

      "Then the wing spar needed which will be another massive structure adding even more to the weight."

      I'm guessing spars will be part of the lifting surface structure, but if there is an alternative, cut these.

      "Which will add more to the weight of the landing gear which will mean more fuel which will mean more load on the spar, more wing area, and.....
      It only makes sense "

      Yes, it does. I'm not as daft as you think I am, though I'm not writing the same stuff as you. this sometimes leads people to think someone 'doesn't get it'.

      --
      deleting the extra space after periods so i can stay relevant, yeah.
    25. Re:Wow that was just bad. by LWATCDR · · Score: 1

      "I think this is a common problem for all aerodynamic vehicles, isn't it? We've done some good work in that area if I recall."
      Actually as aircraft get larger and larger the weight of the landing gear goes up even quicker. Take a look at a 747s landing gear compared to say a 737 some time. The problem gets worse as the fraction of the weight that is take up by fuel goes up. A single stage to orbit craft is hard. The is why we don't have one yet.

      Then you have the problem of the wing. As your speed range and fuel fraction go up the problem gets worse and worse.
      It is easy to make a wing that works at between 50 MPH and 100 MPH. It is actually pretty hard to make a wing that works well from say 100 MPH and 500 MPH. To make a wing work well between 200 MPH and 10,000 MPH is extremely difficult.
      So if you have enough thrust to reach orbit you will probably have enough thrust for a vertical take off. By going for a vertical take off you can keep the lifting surfaces smaller since they will only have to take the landing weight and you can keep the structural weight lower since the wings are smaller and the landing loads a lot lower.

      "I'm guessing spars will be part of the lifting surface structure, but if there is an alternative, cut these."
      Spars are the support structure. They must be sized based on physical loads of vehicular weight. The lifting structure are based on the speeds involved and aerodynamic properties.
      Spars often have to take none aero loads such as landing gear loads as well as the loads imposed by the wing.
      Cut them?

      "Yes, it does. I'm not as daft as you think I am, though I'm not writing the same stuff as you. this sometimes leads people to think someone 'doesn't get it'."
      Let me ask this? Do you have any knowledge of structural engineering, aerodynamics, or material science?
      It takes a great deal of effort and knowledge to design an airplane that can take off from a 300 foot strip, fly four people 1000 miles at 200 mph with only a 200 HP motor. Actually I am not sure any plane can do that yet a few are close.
      Now to build something that can take off at 200 miles an hour, fly into orbit, and come back has not been done yet and may not be possible with today's tech. It is going to take a while and it is going to take at least a scram jet.
      No I am pretty sure that you really just don't get it. What you want is as out of reach of us today as a 747 was in 1918. What we really need is a DC-3 at this time. The shuttle was at best the Spirit of Saint Louis or a Victor Vimy.
      I do think that if we tried we could build a Shuttle that would be a DC-3 today if we took everything that we learned but the political will still isn't there for the expense. Hopefully we can get a working Scram jet which may get us to the DC-7 level.
      But yes you your posts are full of fantasy and it would nice ifs.

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
  8. Why not, indeed? by rickb928 · · Score: 4, Interesting

    Stepheson makes this point late in the article:

    "There is no shortage of proposals for radically innovative space launch schemes that, if they worked, would get us across the valley to other hilltops considerably higher than the one we are standing on now—high enough to bring the cost and risk of space launch down to the point where fundamentally new things could begin happening in outer space. But we are not making any serious effort as a society to cross those valleys. It is not clear why."

    It's somewhat clearer why, to me.

    I want to buy a more fuel-efficient car, and keep my current, less-efficient car. My current car is useful for many things, but commuting to work could be done by another, more efficient one. Here, however, is the rub. Despite the improvement in fuel economy, it is still a net increase in cost to me for a fairly long time. Acquisition, insurance, and upkeep consume most of the fuel savings. Yes, it would be better for he environment also, but that doesn't immediately or directly impact my costs very much. So I put off buying that car.

    Our current methods of delivering object into space work well enough, and the alternatives are both unproven and not sufficiently advantageous to warrant immediate adoption.

    However, as we re-enter manned space exploration, we will be looking for heavy-lift options that don't actually exist today, and those present the opportunity to develop new methods. Avoiding the vertical portion of a rocket launch also avoids the need for massive thrust to overcome gravity that directly. Stephenson alludes to this, and 'space planes' are the current focus, along with some multi-mode concepts. NASA'a failing Ares program is a fair example of lock-in that Stephenson is writing about. Being more open to the development of ultra-high-speed vehicles and their engines might offer both better alternatives and true advances. But that takes ingenuity and a willingness to risk that NASA doesn't seem to possess right now. Bad climate to propose trillion-dollar space programs, though we've been willing to propose trillion-dollar stimulus packages for more mundane projects, such as propping up failed financial institutions.

    Imagine the impact of a trillion-dollar space plane project. Would US students consider a career in engineering if they saw both the opportunity to be part of a cool new future, and the employment options as well? Would this give US aerospace companies something else to sell instead of weapons systems, and is that a good thing? Would it spur international competition, and is that good? Would it divert China's resources into something besides crushing the world's manufacturing competitors? Does that matter? Would a trillion dollars given to this project do more good than giving it to the bankers? Will the bankers also flourish in the glow of this project?

    --
    deleting the extra space after periods so i can stay relevant, yeah.
    1. Re:Why not, indeed? by sznupi · · Score: 3, Insightful

      There's one key word in that quote - "if". "There is no shortage of proposals for radically innovative space launch schemes that, if they worked..."

      When we really seriously look at spaceplanes (say, HOTOL or Skylon studies), it turns out they aren't likely to end up any better (in best case scenario!) than "dumb rocket" using comparable technology, materials science ... on the level which we don't have yet, and which is required to make the spaceplane even borderline doable!

      While, perhaps, we haven't utilized yet all the possibilities of dumb & simple approach, in some ways we are worse than first effort

      --
      One that hath name thou can not otter
    2. Re:Why not, indeed? by tekrat · · Score: 1

      For all the logic in your last paragraph, it ignores the obvious: That America isn't about making game-changing leaps in technology anymore. It *is* about a few people, trying to amass as much money as they can, as quickly as they can.

      Thus, it is about giving a trillion dollars to bankers, because they are the ones controlling the government, and they don't care about "building" anything, other than the number of digits in their personal accounts.

      --
      If telephones are outlawed, then only outlaws will have telephones.
    3. Re:Why not, indeed? by nomentanus · · Score: 1

      So you repeat his argument, with your own extremely similar example; and then say that big science and big projects cure all. And, yes, sometimes they help a bit by creating novel circumstances that allow the development of say, the safety helmet (Golden Gate Bridge.) Not to mention Tang. But usually big projects follow new technological breakthroughs and novel engineering designs, they don't create them. The rocket tech developed in and after WWII caused the Apollo project, not the other way 'round.

      Right now, a huge breakthrough in interplanetary propulsion, plasma propulsion, is being funded, a bit, by NASA. To it's credit: but way too little funding given the extraordinary advance that this new tech represents, and the huge projects it would allow us to perform - say by returning a very rich asteroid to earth orbit. Only if we dump far more money into the lock-in breaking research now can we have the big projects later.

    4. Re:Why not, indeed? by sznupi · · Score: 1

      say by returning a very rich asteroid to earth orbit

      Say what?

      --
      One that hath name thou can not otter
    5. Re:Why not, indeed? by nomentanus · · Score: 1

      I like this comment because extreme wealth disparities are in fact a huge cause of lock in. Maybe, as some argue, wealth disparities don't affect happiness since that is created by relative differences in wealth, not absolute. But the already very rich can only lose by game changing innovation, so the sharply increasing disparity in the U.S. does heavily reinforce lock-in.

      Eventually, such wealth concentration becomes self-referential:

      "nearly a quarter of the 400 wealthiest people in America on this year’s Forbes list make their fortunes from financial services, more than three times as many as in the first Forbes 400 in 1982. Many of America’s best young minds now invent derivatives, not Disneylands, because that’s where the action has been, and still is, two years after the crash."

      http://www.nytimes.com/2010/12/26/opinion/26rich.html?pagewanted=2

      And yes, Houston, we have a problem:

      "One study concluded that each percentage-point increase in the share of national income channeled to the top 10 percent of Americans since 1960 led to an increase of 0.12 percentage points in the annual rate of economic growth — hardly an enormous boost. The cost for this tonic seems to be a drastic decline in Americans’ economic mobility. Since 1980, the weekly wage of the average worker on the factory floor has increased little more than 3 percent, after inflation.

      The United States is the rich country with the most skewed income distribution. According to the Organization for Economic Cooperation and Development, the average earnings of the richest 10 percent of Americans are 16 times those for the 10 percent at the bottom of the pile. That compares with a multiple of 8 in Britain and 5 in Sweden."

      http://www.nytimes.com/2010/12/26/business/26excerpt.html?pagewanted=2

    6. Re:Why not, indeed? by Peeteriz · · Score: 1

      Good enough solutions are the mortal enemy of great solutions.

    7. Re:Why not, indeed? by Jarnin · · Score: 1

      However, as we re-enter manned space exploration, we will be looking for heavy-lift options that don't actually exist today, and those present the opportunity to develop new methods.

      I think you mean "if" we re-enter manned space exploration. The U.S.A. has completely lost it's technological edge when it comes to space flight. Sure, the military probably has something up it's sleeve, but NASA has, um, nothing that can get a human into orbit after Endeavour's final flight in late April. Sure, they're talking about making another man-rated heavy lift launcher, but they've been doing that for the last 3 decades with nothing to show for it.

      I'll be shocked if we have a new heavy launch vehicle actually produced by NASA in the remainder of my lifetime. More likely; a private company will have a heavy launch vehicle that can be man-rated, but never will be due to the lack of cash the U.S.A. has to spend on such things.

      Sorry to be a buzz kill, but the glory days of manned U.S. space exploration are over.

    8. Re:Why not, indeed? by Rei · · Score: 1

      Mass production in rocketry is good. It's not a godsend. One of the primary failure modes in rocketry is stage separation. Apply that concept to OTRAG. Also, running many engines in once right near each other isn't as easy as it sounds; failures from one can screw up those around them, vibrations can propagate through the structure, etc. See the Soviet N-1 rocket for an example. More problems abound. The more stages you have, the greater your integration and testing costs as well, which is already an extremely high cost, and would increase linearly with the rocket count. You're *very* vulnerable to pogo with this design. The already abysmal payload fraction keeps getting worse when you take into account things like accounting for different burnout times. Your rocket must start off asymmetrically loaded with fuel (off balance) in order to keep burnout times as close to equal because of when the rocket turns to the horizontal plane, you have to throttle down or off the engines on one side -- either that, or you have it be asymmetrically loaded at burnout.

      As for "Rocket a day", mass produciton is no magic wand. It doesn't make your *total* costs lower; it makes your *per-unit* cost lower. Let's say you're making 50 widgets a year for $1 each. You may be able to mass produce the widgets, making 5,000 a year for $0.50 per unit. But you sure as heck better have a market for 5,000 widgets at $0.50 a year, because you're proposing to spend 50 times as much manufacturing widgets. In terms of rocketry, this just won't happen, because the total you have to spend on rocket launches increases so much faster than the price declines will stir up new business.

      You also get into the problem that not all rockets are created equal. Payloads to different orbits vary widely. Where they can be launched from varies widely. Some rockets are man-rated. Some can handle in-flight restart. And on and on. A Pegasus is not a substitute for a Delta-IV Heavy. And not only do you have do you have widely varying launch needs, but you have basic human nature: different companies want to make their own stack (and everyone thinks they can do a better job than everyone else), and different companies want their own launch systems for reasons of national pride.

      Both "Rocket-A-Day" and OTRAG have serious flaws.

      --
      I guess I just let my urge to spawn soldiers for Satan's dark army get the better of me.
    9. Re:Why not, indeed? by sznupi · · Score: 1

      Yes, yes ... and some fantasy, massively more complex system (say, a launch loop) is a solution to all those troubles. As was the Shuttle. Please...

      BTW the main problem of N-1 was politically rushed schedule (gee, I wonder how "we must do this!"-driven megastructure would fare...) - its engines never even test fired as a group, before launch attempt.
      But there's another outwardly quite complex rocket, few engines, many more nozzles, very "crude" timing of separation, the closest to mass production - it's also the most reliable ... most frequently used (obviously) launch vehicle in the world

      Of course, from your description of "requirement" to be asymmetrically loaded, to "allow" assymetrical thrust & mostly horizontal flight... it's clear you have no idea about the basics of rocketry, of physics (say, parts manifesting themselves in gravity turns, which dominate the dynamics of launch); just ideological derision of technology that "took away" the dreams described in works of fantasy, just puffy wishful thinking.

      --
      One that hath name thou can not otter
    10. Re:Why not, indeed? by rickb928 · · Score: 1

      Well, I hope not. Ares is a bust, but looking at the commercial projects gives me hope that we can get off the vertical lift scheme and build real space planes. It seems as if there is an economy to a lateral lift that would solve some problems, but not being an engineer means I can't work out the details.

      Then again, neither can the engineers.

      --
      deleting the extra space after periods so i can stay relevant, yeah.
  9. Better at Sci-Fi than Science History - skip it by advid.net · · Score: 1

    I think he should stick to sci-fi instead of writing bad journalism with a poor story of rocketry.

    He has many points wrong, he thinks he has guessed how it went and why but failed to it.

    At least he should have read Von Braun book about rocket science, but obviously he didn't.

    I stoped reading his "perspective" here :

    centrifugal force counteracts gravity

    ...

    1. Re:Better at Sci-Fi than Science History - skip it by Anonymous Coward · · Score: 1

      "I stoped reading his "perspective" here :

      centrifugal force counteracts gravity"

      That is actually not a horrible laymans explanation.

    2. Re:Better at Sci-Fi than Science History - skip it by PvtVoid · · Score: 1

      I stoped reading his "perspective" here :

      centrifugal force counteracts gravity

      Uh, why? That's a perfectly accurate statement. One simple way to write the condition for a circular orbit, for example is that the gravitational and centrifugal forces are equal and opposite.

    3. Re:Better at Sci-Fi than Science History - skip it by element-o.p. · · Score: 1

      Meh...it perpetuates the myth that there is actually a force that acts to pull an object outwards, when in reality it is simply inertia. I prefer the way my high school physics teacher described orbits: if you throw something into the air, it will eventually fall back to earth. The harder you throw the object, the farther across the earth it travels before it falls back again. If you throw it hard enough, it will reach a point where it falls around the earth, rather than back to it. At that point, it is in orbit.

      --
      MCSE? No, sir...I don't do Windows. Yes, I am an idealist. What's your point?
    4. Re:Better at Sci-Fi than Science History - skip it by Rei · · Score: 2

      Come now, do you really expect me to do coordinate substitution in my head while strapped to a centrifuge?

      The reality is, of course, that there aren't really any significant forces acting on you at all. You're travelling in a straight line when in orbit. It's space that is bent.

      --
      I guess I just let my urge to spawn soldiers for Satan's dark army get the better of me.
  10. Fuel Depots by Anonymous Coward · · Score: 0

    One word, "Fuel Depots". Well that's two words, sorry.

    See Rand Simberg's thread on this article here: http://www.transterrestrial.com/?p=31999

  11. Fail by Anonymous Coward · · Score: 0

    Stephenson really needs to go back and re-read the actual history of events, not the Cliffs Notes version. There are some embarrassing errors in there, including the mistaken idea that the hydrogen bomb was developed specifically for use with ICBMs. In fact, all of the H-bombs used in nuclear tests were either dropped by high-altitude bombers or placed (in the case of the thermonuclear prototypes in the Ivy Mike and Castle Bravo shots) in specialized installations on the ground. None of them were delivered by ICBM.

    In short, the effectiveness of the ICBM is a fallacy that started with Robert MacNamara and has been perpetuated by ill-informed historians ever since.

  12. Total Fail by NEDHead · · Score: 1

    What a bad article! I am not even sure what the point of writing it was. There was neither a useful proposal for an alternate approach, nor even a clear call to action of any sort.

  13. I don't think his premises support his conclusion by amliebsch · · Score: 3, Insightful

    Suppose you accept his premises that our current state of rocket technology evolved in part due to key improbable events. As a result, we've continued that technology, to "climb to the top of that hill" as he puts it. That doesn't, by itself, automatically mean there must be higher hills to climb. We may have purposefully or accidentally climbed the highest hill we are currently capable of climbing. Perhaps we would have been further along with some other technology if we hadn't climbed this hill, but it might not have been better overall. Right? I mean, it could have turned out like our quest for magnetically confined fusion.

    Blind people develop superior hearing to sighted people. I'd still rather have my vision, and I don't think that's entirely due to path dependency.

    Same mistake with the combustion engine. Yes, we are getting close to maxing out the technology. But it's not clear that, if we had not developed it in the first place, we would have come up with something more effective in its place. It's not even clear we would have come up with something *as* effective. It's not even clear we even have anything plausible *yet* that would be as effective.

    The fundamental mistake in this article seems to be an assumption that the grass is greener in the counterfactual, but he presents no evidence to persuade us that this is actually true.

    --
    If you don't know where you are going, you will wind up somewhere else.
  14. Why aren't we trying something new? No unobtanium by edremy · · Score: 2, Interesting
    Alternates fail simply due to the lack of materials.
    • Spaceplane? The Lockheed VentureStar fits all the bills- except that there's no tank material that can hold LH2 at the needed temperatures and still be light enough to get to orbit on a single stage.
    • Elevator? Unobtanium all the way. Some theoretical studies show that carbon nanotubes *might* have the needed tensile strength, but given that we can't reliably grow flawless ones a millimeter long the 22,000 mile thing is a bit of a tough problem.
    • Big gun? Workable, but you can't send anything fragile, including people

    I think if he looks a bit more deeply it has very little to do with lock in and everything to do with the fact all the wonderful SF ideas out there simply can't be built with our current level of technology.

    --
    "Seven Deadly Sins? I thought it was a to-do list!"
  15. Re:I don't think his premises support his conclusi by sznupi · · Score: 2

    That doesn't, by itself, automatically mean there must be higher hills to climb. We may have purposefully or accidentally climbed the highest hill we are currently capable of climbing. Perhaps we would have been further along with some other technology if we hadn't climbed this hill, but it might not have been better overall.

    It might be actually slightly the other way around - did we already forget the absolute dominance of "spaceplanes" in scifi of 30s, 40s or 50s?! (even design attempts - Silbervogel, or early winged visions of von Braun) Flying saucers even, at some point...

    No doubt fueled by rapid advances in aircraft technology at the time. What almost everybody wished for. And we still do, it's easy to remember and relate common experiences of air travel, while forgetting how it's "supposed to" look like (airplanes from "our" times as envisioned ~130 years ago, no doubt influenced by rapid advanced in marine technology), when approached in the same style as "spaceplanes" (actually, I wonder how much the Shuttle was influenced by designers and decision-makers growing on spaceplane scifi ... and we know how that ended, it didn't deliver on any of its main points as advertised; not a lot of flying boats around, too)

    --
    One that hath name thou can not otter
  16. Replace rockets sound great... by Anonymous Coward · · Score: 0

    Oh you don't actually have a plan you just wanted to bitch. The space elevator is a great idea in theory but we need to build one hell of a rope and the material science aren't up to the task yet. A space plane? You mean a plane with rockets that would at best be a minor improvement if we could perfect it. So rocketry isn't exactly cheap or fuel efficient, but it does seem to get you out of one hell of a deep gravitational well.

    Maybe we could build ionic craft in orbit they can hit higher speeds than rockets, but not fast enough to go anywhere interesting in a lifetime.

    Truly interesting work in this field is going to be theoretical math and science for at least most of our lives.

  17. Re:I don't think his premises support his conclusi by necro81 · · Score: 1

    That doesn't, by itself, automatically mean there must be higher hills to climb.

    But in the two areas he focuses his conclusion on - rocketry and energy - there are demonstrably higher hills to climb. There are other architectures and paradigms that, on paper or in experimentation, guarantee better efficiency, lowered risk, lower cost, etc. If we, collectively, only had the fortitude to start climbing again.

  18. Re:Why aren't we trying something new? No unobtani by Tekfactory · · Score: 1

    Don't forget the;

    Roller Coaster Scramjet

    Lighter than air or neutrally buoyant Space elevator

    High Altitude Lighter than air Rocket Launch Platform

    White Knight X carrying Giant rocket

  19. A nice addition to Jacob's (and Smolin's) Thesis by nomentanus · · Score: 1

    A great article by Neal Stephenson, that I was lucky enough to stumble upon yesterday, after months of thinking over related difficulties in science, and particularly physics (in part, as Lee Smolin has written about.) I'm going to say that Jane Jacobs' argument in "Dark Age Ahead" subsumes Neal's, although Mr. Stephenson adds a great deal. She argued that what was exploratory science has now been replaced by a lot of people who look the same, since they still wear lab coats a lot[ but who are just spouting cant, merely copying previous “scientific” opinion, or just making it up on the spot; and are dreadfully reluctant to challenge whatever has previously been held to be “obviously true” - whether there was ever any evidence offered in support of that opinion or not. In other words, an academic priesthood that has a stunning degree of priestly inertia – the opposite of what science is supposed to be.

    Lee Smolin argues much the same of physics in “The Trouble with Physics”, and I'd like to argue that the field of medicine is still worse for priestly nonsense. (I ask you, in what other field would the advocacy of something like “evidence-based medicine” be novel, and revolutionary?)

    Jacob's argument easily extends to saying that only very large technological changes force the “science” priesthood to adapt and change occasionally, by revealing large new realms of incontrovertible evidence. But, ouch, now Neal Stephenson, using rockets as an example, argues that technology may be ossifying more than we suspect, too, making the logjam complete.

    The historical extension of this argument is that progress slowly moves around the globe because every civilization can advance only so far until it lapses into immovable complacency headed by economic or academic special interests who are doing just fine as things are, thanks. Then the torch passes to another civilization; for example, China to India to Arabia to Europe, over the last few millenia. Yet today, globalization ties us together so closely that there is now nowhere left for that torch to go. Globalization means globalized lock-in, too.

    In other words, to return to Neal's example: “Why did the Chinese invest in developing a rocket capability rather than try to skip ahead to a better technology, since they had no infrastructure or educational investment in the old tech? Why were they locked in?” Arguably, however, developing economies are often even more locked in to obsolete technologies, for which no alternative has yet emerged. The gains in capacity by copying are so great, for so little investment (starting buying rocket tech at a discount from Russia) and with such great political benefits, that the outcome is all too predictable, both in technology, education and science.

    I wish there were some way to convince the Chinese that no society is rich until it can afford to fund research efforts that fail frequently, publicly, and thoroughly. Then again, I wish I could convince us! Here in the U.S., centrally planned science funding that is ultimately supervised by an easily embarrassed Congress has everything to do with lock in, since innovation at the margins is the only reliable way of obtaining research funds, period, end of sentence, end of marked innovation.

  20. A new player would change the rules by petes_PoV · · Score: 1
    If another state, without an incumbent rocketry industry, was to get serious they would effectively start with a clean sheet of paper. They would not have to go to the trouble of developing all the preceding rocket based technologies, and could leapfrog to the next hill (albeit not to the top of the hill - at least not to start with). If that paid off and they were able to put payloads into orbit for a tenth, or a hundredth of what conventional technologies were charging that would be such a disruptive technology that the old regime would be out of business within a decade.

    The key for that new state would be to keep their developments a closely guarded secret, purely to increase the time advantage they had until every other spacefaring nation could work it out for themselves. The question then becomes, do the other states try to play catch-up and slavishly emulate what the new guy is doing, or do they try to leapfrog them onto the hill after that?

    --
    politicians are like babies' nappies: they should both be changed regularly and for the same reasons
  21. Horizons by ISoldat53 · · Score: 1

    The main problem to advancement is horizons. His solutions are looking at horizons that take generations to come to fruit. But, political horizons are two years apart. The status quo is the safer bet. The future belongs to someone else.

  22. Re:Why aren't we trying something new? No unobtani by Anonymous Coward · · Score: 0

    At the start of the space program they couldn't build rockets that would reliably not explode. Over the coarse of it they developed a wide range of new materials and technologies (ceramic tiles on the shuttle, velcro, hydrogen fuel cells, and any number of polymers for example), which made what was impossible with the technology of the day common enough that people think it's boring.

    The point of the article is that alternative launch methods may be beyond today's technology, but developing the technology of tomorrow would be a more worthwhile use of the resources that would otherwise go towards milking that last couple tenths of a percent of efficiency out of the technology of yesterday.

  23. Hybrid space plane? by scharkalvin · · Score: 1

    I've always wondered why to get to space you HAVE to start on earth with rockets. Air breathing engines can get us up to almost 100,000 feet in one or two stages. A large 'first stage' could use a combination of turbine engines to get up to around 50,000 feet at sub-sonic speed, then switch to scram-jets to get to hyper-sonic speed and 100K+ feet. Then a rocket powered second stage would go the rest of the way into space while the first stage glided back to earth (or flew under it's own power if there was still fuel left).

    IIRC the original plans for the space shuttle were along these lines.

    1. Re:Hybrid space plane? by sznupi · · Score: 2

      Check put Pegasus rocket - it does to a large degree what you want. And is one of the most expensive, per kg, launchers around.

      The general problem is how "enthusiasts" forget about physics, about rocket equation, about how majority of the acceleration must happen outside the atmosphere, how there's a square attached to speed in kinetic energy (which comes from the energy of propellant). Read about HOTOL or Skylon, too. When rigorously looked at, ending not better (in best case scenario!) than a normal rocket using similar materials (which we don't have yet, and which are required for a spaceplane to even barely work - all those fancy, complicated flight sequences accomplishing... to lift structures... which are necessary for said sequences)

      --
      One that hath name thou can not otter
    2. Re:Hybrid space plane? by BJ_Covert_Action · · Score: 2

      That's definitely a possible method to achieve orbit. However, you need to realize that the big hurdle in getting to orbit is not altitude, it's velocity. Yes, you can hoist a big ass rocket up to 100,000 feet and launch it from the back of a hypersonic plane. It turns out, however, that you still need a really big ass rocket (I know, lot's of technical details there) to achieve orbital velocity no matter how high you launch from. That said, it tends to be a lot cheaper and easier to launch a big ass rocket from a stationary, land based platform, than it is to launch it from a flying, attitude-subject-to-weather-conditions plane.

      So is it possible? Yes. Are we trying it? Yes, some companies/organizations are. Will it be the final answer to space access? Well, maybe, but it will probably prove to be just as complicated and expensive as rocket launches. Then again, maybe not. We'll find out in another couple decades when the technology comes to fruition.

  24. Physics by RogerWilco · · Score: 2, Interesting

    I think the article is ignoring some basic physics that has driven us to these outcomes, both his rocket and his oil dependency example.

    To get anything into orbit needs a very good weight/energy ratio. The only thing that can provide this itself are your typical rocket fuels. There's two other options:

    - Atomic: this usually goes out the window when you consider manned vehicules due to the weight of shielding, and for unmanned vehicules the environmental effects.

    - Cheat by leaving a significant part of your mechanism on the ground. Space cannons, magnetic rails and the like. The problem here might indeed be one of technology. even a very fast car (Thrust SC2), might go about at the speed of sound. Sounds pretty fast? It's still nowhere near enough what you'd need. The escape velocity is about 11 km/s, the speed of sound about 300 m/s. Now we need to think in energy, so we need to use E = 1/2 mV^2. Or in other words we need to compare the square of the velocities. 300^2/11000^2 = 0.00074 or about 0.075% of the energy required.
    Going much faster and the friction with the atmophere melt your vehicule.
    So to get anywhere with a space cannon type system, it needs to be on a very high platform, probably 10km or more, and then be big enough to accellerate a payload to 10-20 times the speed of sound.

    When you look at the basic physics, you very quickly end up with rocket-like devices.

    A similar thing holds true for our dependency on oil. It again boils down to weight/energy ratio, but with much bigger safety, usability and logistics constraints.
    The math is not as straigthforeward, as it's mostly economics, but only rocket fuels give much more power to weight ratio then the conventional fossile fuels.

    --
    RogerWilco the Adventurous Janitor
    1. Re:Physics by nomentanus · · Score: 2

      And bees can't fly. Until you look at the problem another way. For example, ablative materials, or a two stage shot to reduce initial atmospheric resistance, etc, etc, etc. Who needs to be told that the need for a search for new tech that isn't obvious, can't be contradicted by saying that there is no blindingly obvious path to that tech right now? Boring a hole in a magnetron blew apart the equation that "proved" that producing microwave radar was forever impossible (see cavity magnetron) - but first you have to imagine that there is something your present equations haven't imagined or encompassed. What we have here is a failure of the imagination...

    2. Re:Physics by jgtg32a · · Score: 1

      OT, but did they ever come up with a mathematical answer as to why bee fly?

    3. Re:Physics by Anonymous Coward · · Score: 0

      I fear that it's much more cynical than that.

      It's my belief that we abandoned the much less expensive launch technology of space-guns in favor of rockets due to a perceived lack of military applications with the former.

      While rockets(ICBMs) can have mobile launch platforms and are easy to hide, space guns have historically been built on mountains to help cut down on atmospheric drag.

      The problem being: that they were difficult to move(READ: aim), and the resulting seismic shock-waves from firing it made it of little tactical value due to it's ease of discovery and destruction during a Nuclear First Strike/Sneak Attack.

      Further, judging from Gerald Bull's difficulty with G-force deformation of solid rocket motors^A, I would speculate that a nuclear warhead would be far too fragile to use in a space gun.^B

      Now that I have speculated on the motive, I'd like to address the subject of feasibility.

      There are two ways to solve the problem of atmospheric drag. I believe SHARP's John Hunter, of Quicklaunch Inc, is proposing a hybrid rocket/space-gun approach with the space-gun doing the dirty work of the first several rocket stages^C(I don't remember if his proposal takes advantage of hydrogen gas jets on the nose cone to supercavitate^D through the atmosphere.).

      Additionally, while difficult, it would be possible to use a high altitude launch platform supported by a lifting gas such as Helium, Hydrogen, or even Methane to initiate ignition in a much thinner atmosphere, thereby increasing fuel efficiency.^E

      Another proven method of reducing atmospheric drag is to draw an artificial vacuum.^F This would be most easily accomplished by building a mass driver or space gun in a tunnel taking advantage of existing land formations suck as antarctic ice sheets, or by building a subway tunnel.^G

      Finally, we know from nuclear testing that high explosives can generate vacuums. If a moored balloon had a series of high explosives attached to it's tether, those explosives might create a "tube" of low pressue if properly synchronized with the firing. Otherwise, I'd love to sea a feasibility study on detonating an air burst directly overhead a blast hardened space gun in order to generate the necessary vacuum.

      References
      ^A http://en.wikipedia.org/wiki/Project_HARP
      ^B http://en.wikipedia.org/wiki/W88
      ^C http://www.youtube.com/watch?v=1IXYsDdPvbo&feature=related
      ^D http://en.wikipedia.org/wiki/VA-111_Shkval
      ^E http://en.wikipedia.org/wiki/Rockoon
      ^F http://en.wikipedia.org/wiki/Vactrain
      ^G http://settlement.arc.nasa.gov/Nowicki/SPBI110.HTM

      Further Reading:
      http://en.wikipedia.org/wiki/Super_High_Altitude_Research_Project

    4. Re:Physics by Intrepid+imaginaut · · Score: 1

      The escape velocity is about 11 km/s, the speed of sound about 300 m/s.

      Yes but you don't need to get to escape velocity, just LEO and build from there.

      So to get anywhere with a space cannon type system, it needs to be on a very high platform, probably 10km or more, and then be big enough to accellerate a payload to 10-20 times the speed of sound.

      Oddly enough, quite doable.

    5. Re:Physics by Intrepid+imaginaut · · Score: 1

      What we have here is a failure of the imagination...

      Indeed, which is itself a failure of the scientific method.

    6. Re:Physics by Anonymous Coward · · Score: 0

      OT, but did they ever come up with a mathematical answer as to why bee fly?

      Yes, but the entire story of a scientist or engineer "proving" bees can't fly was semi-mythical in the first place. There are several theories about how the tale got started, but there is no record of either the proof itself or who was responsible for it.

    7. Re:Physics by slashqwerty · · Score: 3, Interesting

      Now we need to think in energy, so we need to use E = 1/2 mV^2. Or in other words we need to compare the square of the velocities. 300^2/11000^2 = 0.00074 or about 0.075% of the energy required.

      The big problem with rockets is that the fuel has to travel with the vessel. I haven't done the math but I have heard roughly half of the fuel is spent accelerating the other half to the speed of sound. If you have a land-based system that accelerates the vessel to the speed of sound you can make the vessel half the size (or replace half the fuel with payload).

      Speaking of the fuel, most of the weight comes from the oxidizer. With a hydrogen-oxygen rocket you need one oxygen atom for every two hydrogen. Oxygen has an atomic weight of 16 while hydrogen has an atomic weight of 1. So 89% (16/18) of the mass is oxygen.

      Imagine if you had a railgun that accelerates a ram-jet past the speed of sound, the ram-jet burns oxygen from the air and accelerates to nearly orbital velocity, finally a rocket takes over to reach orbit. If we could get that working we would have much better access to space.

      It is worth noting Burt Rutan uses a mother ship to launch his space craft. The mother ship gets up to speed by burning oxygen from the air in standard jet engines. The spacecraft then drops off and launches with a substantial head start.

    8. Re:Physics by strack · · Score: 1

      ive never seen equations abused in such a manner. you completely ignore the mass of fuel that you dont have to accelerate along with the rocket in order to get it to, say, mach 6 out the end of a launch rail.

    9. Re:Physics by Big_Breaker · · Score: 1

      Quicklaunch doesn't get nearly enough attention.

      The heavy, durable stuff should be shot out of a gas cannon and only the squishy humans should ride the rockets.

      http://www.newscientist.com/article/dn17931-blasted-into-space-from-a-giant-air-gun.html

      http://www.youtube.com/watch?v=1IXYsDdPvbo

    10. Re:Physics by DerekLyons · · Score: 1

      The big problem with rockets is that the fuel has to travel with the vessel. I haven't done the math but I have heard roughly half of the fuel is spent accelerating the other half to the speed of sound.

      Correct for the first part, wrong for the second. (It's more like .05-.10 or so.)
       

      Imagine if you had a railgun that accelerates a ram-jet past the speed of sound, the ram-jet burns oxygen from the air and accelerates to nearly orbital velocity, finally a rocket takes over to reach orbit.

      The least of the (multiple) problems with your scheme is that ramjets can't achieve more than a fairly small faction of orbital velocity, and does that at a fairly small fraction of the altitude required. (Car analogy time: This is like using another car to tow your car a mile while accelerating it to 5mph - and the using your own car to accelerate to 55mph and complete your seventy mile commute.) The end result is you spend billions in R&D and upfront costs and few hundreds of thousands of dollars in assorted operational costs to save a few hundreds of thousands of dollars in first stage fuel.
       

      It is worth noting Burt Rutan uses a mother ship to launch his space craft. The mother ship gets up to speed by burning oxygen from the air in standard jet engines. The spacecraft then drops off and launches with a substantial head start.

      It's worth noting that this is pretty much irrelevant to the matter of orbital flight as the energies and speeds involved in suborbital flight are vanishingly small fraction of those involved in orbital flight. Rutan's solution doesn't scale well.

  25. He's right on how it started, wrong on why stuck. by Animats · · Score: 1

    Arthur C. Clarke, who'd been pushing space travel for decades via the British Interplanetary Society and his SF works, was interviewed during the runup to one of the Apollo launches. He said "If we'd have known this was going to cost twenty billion dollars, we would have given up and gone home." Before Sputnik, space travel was a hobbyist thing.

    Chemical rockets to oribt just barely work. Most of the mass is fuel. For a single-stage-to-orbit rocket, with the fuels with the best possible energy density (LOH and LOX), 97% of launch weight must be fuel. With two stages, it gets better, but not much better. So rocketry is about weight reduction, which is why everything is so fragile and failure rates are so high. If the mass ratio were better, rockets would be built with aircraft-type weight budgets and would work much more reliably. But, launching from a 1G planet, we're stuck with those numbers. That's why Richard van der Riet Wooley, Astronomer Royal in the 1950s, said "Space travel is utter bilge".

    Many alternatives have been tried. Launching from an aircraft works; Pegasus is launched that way, as is the Virgin craft. But it's not a big win. Big guns? Feasible, but only for stuff that can handle a few hundred Gs, like water or air shipments.

    Takeoff with a suborbital spaceplane? That was Ronald Reagan's idea in the 1980s. Ben Rich, head of Lockheed's Skunk Works and designer of the SR-71 propulsion system, decided that Lockheed wouldn't bid on that. The materials problem was too hard. "We used titanium. You know something stronger?".

    Atomic rockets are feasible, and have been ground-tested. Early plans for Apollo had a nuclear powered second stage and a Nuclear Assembly Building at Canaveral. It's messy, but it would work. The cost back then was calculated as half a human life per launch from cancer, amortized over a large population. That might not stop China.

    Fusion would be great if we could do fusion power. (The "helium-3" enthusiasts tend to gloss over that fact. He3 fusion is harder than Dt-Dt fusion, which we can't do either.)

    Launch lasers are a neat idea, but it takes a gigawatt to launch a metric ton. That's not impossible; one could in theory have a huge collection of lasers at Mojave, and, launching late at night, could use all 6GW from Hoover Dam, plus extra power brought in from the LA area. The Apollo lunar module was about 10 metric tons. The biggest continuous laser ever built, though, produced a megawatt for 70 seconds, So we need 4 more orders of magnitude, or 10,000 such lasers, to do a launch.

    I recently had this discussion with someone who's entering the X-Prize competition. He's a bright young guy with an interest in space. But he can't see any new ideas working, other than even more clever weight reduction.

  26. It's not true. by mosb1000 · · Score: 1

    Liquid fuel rocket research did not start in NAZI Germany. It is very likely in my opinion the technology would have been used to launch payloads to orbit initially no matter the course of history. It's inventor specifically imagined using the technology for launching payloads to orbit, and it was the only technology even remotely capable of achieving that at the time. H.G. Wells imagined shooting a payload out of a giant cannon, but the Germans were working on that too. Even today, the imagined alternatives (Scramjets, space elevators among others) may prove to be impossible, infeasible, or more expensive. Irregardless, research on such alternatives is ongoing, and it disingenuous to imply that it somehow is not.

  27. Re:Why aren't we trying something new? No unobtani by pellik · · Score: 1

    You seem to have missed the part about how our current level of technology is the result of 60 years and 4 trillion dollars of rocket technology innovation. Of course other ideas are a long way off, but before WW2 our current technology was just as intimidating.

  28. Re:I don't think his premises support his conclusi by amliebsch · · Score: 1

    Strange, then, that he didn't present these in his argument, don't you think? I just disagree that this is about "fortitude." It is about being sensible. The way to develop emerging technologies is *incrementally,* by exploring possibilities and slowly increasing the funding of the ones that show promise, as long as they continue to show promise. We have in fact been doing this, but none of the competing technologies have *in reality* shown much promise yet. Many of them are still at early stages of basic feasibility, because ancillary technologies (like materials) have only recently become sufficiently developed.

    --
    If you don't know where you are going, you will wind up somewhere else.
  29. Re:Why aren't we trying something new? No unobtani by amliebsch · · Score: 2

    Ironically none of your examples are correct.

    - The heat shield tiles were originally developed for ICBM warheads (using composites technology developed in other fields)
    - Velcro was a commerical invention having nothing to do with the space program
    - Hydrogen fuel cells were invented in 1838. The ones used by NASA were invented by a commercial company, G.E., in 1959.

    So it really is more of a case that increasing technological development enabled the space program, not the other way around.

    --
    If you don't know where you are going, you will wind up somewhere else.
  30. Engineering Culture by BJ_Covert_Action · · Score: 5, Insightful

    I like how one of the things Stephenson blames in his article for the rocket lock-in is, "engineering culture," that is resistant to change. I often find that nontechnical folk (and no, sci-fi writing does not count as a technical pursuit) use terms like, "engineering culture," or "scientific elitism," to describe phenomena brought about by actual technical details. In other words, that engineering culture doesn't develop simply because we engineers are resistant to change. It develops because we engineers crunch the numbers and have to deal with reality.

    Anyone who thinks that engineers working in the space launch industry are resistant to change just for the shits is pretty misinformed. When it comes right down to it, we're the ones who would love to find a new Pandora's box technology that could get us into space faster, cheaper, and safer. Hell, we have devoted our lives to pursuing the development of the space industry. If anyone wants to see men and women living on Mars, manufacturing in orbit, and fucking onboard inter-galactic colony ships, it's us. Unfortunately, we don't have the luxury that sci-fi authors have of writing about some great new idea and just assuming it will work. We have to test material strengths. We have to plot thermal loads. We have to damp harmonic oscillations. We have to produce enough energy to overcome gravity. Those aren't trivial tasks. And we don't get to defy the laws of thermodynamics and gravity with some hand-wavy bullshit about, "couldn't this idea totally work in theory?!"

    So yeah, there are lots of proposed theories and ideas on how to get to orbit. Great, congratulations Mr. Stephenson, you have an imagination. And, awesome, you can see sunnier hilltops across the valley that reach higher than the one we are standing on now. That's a great fantasy land. I hope you enjoy living in it. But while you draft up clever metaphors based on cherry-picked "facts" and unrealistic assumptions, those of us working in the industry, you know, the ones doing the math, actually have to look at the numbers. And those distant, high hilltops you see, well they might not be as high as you think. And all those, "innovations," on how to get to space, well they might not be as Earth-shatteringly ingenious as you think.

    I'm not saying there's not room for improvement, there definitely is. But until someone shows me some numbers that prove a space-elevator, a launch loop, or a space fountain can be built, today, without unobtainium (in the form of some material, or some epic power source), I am going to delegate those ideas strictly to fantasy-land for now. And as for things like space planes, hypersonics, multi-propulsion-type vehicles, and so on, we are trying them, to an extent. And, believe it or not, just like rockets, they are still fucking difficult to get right. That's why it takes a long time to develop them. In the end, chucking something out of our gravity well is no easy task, no matter what method you take. And it is expensive, in both time and energy, no matter what technology you utilize. So stop lamenting about how poor off we are compared to where we could be. We're doing everything we can with what we've got. If that's not good enough for you, vote to give us more money or design a small, portable power-plant that can produce a proper metric fuckton of thrust.

    In the end, engineering culture is just a term being used to say, "technical shit that I don't understand well enough so I'lll use it as a scapegoat to justify my preconceived notions"

    1. Re:Engineering Culture by nomentanus · · Score: 2

      I'm pretty sure Neal knows that individual engineers actually spend a little time blue-skying, mostly on their own. After all, he cites the fact that engineers have brought forward possible alternatives. But other engineers cheerfully recommend against investing the large sums necessary to prove the tech and make it an economic competitor. He is saying more about investment, and funding. But re Engineering culture, I had a father who was an engineer, and while he was much more open minded than most of his ilk, he was nonetheless astonishingly closed minded and very quick to tell me that, say, flat display screens were an impossible tech that would never exist, no matter how long the universe lasted, 'cause you couldn't flatten a cathode ray tube. People self-select themselves for engineering school because they have a very deep psychological need for certainty, not because they love career-changing surprises.

    2. Re:Engineering Culture by Anonymous Coward · · Score: 0

      Word!

    3. Re:Engineering Culture by Weedhopper · · Score: 1

      And I wonder who it is who developed the flat screen technology that you are undoubtedly reading this reply on now?

      Engineers reserve their greatest acclaim for the guys who change the game, not those who preserve the status quo.

    4. Re:Engineering Culture by Anonymous Coward · · Score: 0

      No.
      "Engineering culture" is a term meant to differentiate the believers from the thinkers.
      Thinkers are called, "Scientist culture."

    5. Re:Engineering Culture by Anonymous Coward · · Score: 2, Funny

      My favourite example of this came from a graduate social science course an ex of mine was taking. The professor maintained, vehnemently, that rockets and bullets looked the way they did because engineers were historically all male, and obsessed with the destructive power of their own penises.

      I wonder what that professor imagined a rocket designed entirely by women would look like.

    6. Re:Engineering Culture by Anonymous Coward · · Score: 0

      Exactly. This so called `analysis' is short on everything from historical truth to technical fact and is generously sprinkled with Stephenson's trademark sensationalism. Germany was not, as he writes `the most technologically advanced nation on the planet' at the beginning of WWII and Hitler's madness had some rationale in it: Germany desperately needed resources, especially oil. Invading, say USSR was a logical choice to protect Romanian oil fields and try to get access to the ones in the Middles East (soviet Azerbijan, for example). German tanks were rather lousy compared to even American ones, not to mention the Russian T-34 (yes, it changed in 1943 but it was too late). His (Hitler's) `airforce' was no match to RAF or the USAF, his artillery was mostly dated to WWI, he did not even have a reliable truck (look it up, German's main means of transportation was the horse). Moreover, his general staff had no idea about planning such an ambitious operation. This myth of a German superstate is just that, a myth. Hitler played a forced hand and played it very poorly.

      Stephenson's statement that satellites are so expensive because thy have to fit a certain `mold' is due to basic economics, not some mysterious `engineering cabal': try to price a simple thing like a connector that is in every way equivalent to USB A but is not USB A and you will feel the difference immediately. Satellites are mostly `one-off' projects, of course they are expensive. In this sense I always laugh when I hear how well the Mars rovers were engineered since they outlasted their design lifespan by months. To any real engineer this is a sure sign that market economics had no hand in it: well engineered products always last about as long as they are designed to. It is all about the sweet spot of cheap vs desirable. Cheap, fast, or beautiful, pick two.

    7. Re:Engineering Culture by Intrepid+imaginaut · · Score: 1

      "engineering culture," or "scientific elitism,"

      Two very different things, engineers are not scientists. The mindset needed for the two disciplines are worlds apart.

    8. Re:Engineering Culture by Audiophyle · · Score: 1

      You and Neal both made some good points. I do think that path dependency and lock-in are very much present in the space industry, at least in my experience, but some of the changes he's proposing may be in fantasyland at this point. Space missions have a certain objective in mind, whether it's to sell phone time, sell imagery, or study geysers on a moon. The group that wants to do these things usually don't overly care how it's achieved as long as the objective is achieved, and it's as cheap as possible.

      Rarely are aerospace companies in the business of trying out radical new designs because of the huge expense involved (typically). They want to make their shareholders happy, because it is a business after all. One word that is hugely important in the space business is the word legacy. When some satellite, rocket, or component has legacy, it means that it has flown before with mission-accomplishing results, and thus instills confidence in the product, and it will be a lot cheaper to build than the alternative. Program managers and board members would love nothing more than to have your spacecraft, rocket, and overall mission to be completely legacy-based. When something is completely legacy-based, it lacks innovation.

      I think Neal's point is that rockets and satellites do not see huge amounts of innovation because of the crazy expense for the customer, so we tend to be path-dependent and locked-in to tried and true designs.

      The real innovation is going to come from an ambitious young group that can find someone crazy enough to back them for years on end and make a business out of it. It's not going to come from big aerospace companies since all of those are held accountable by their shareholders. So yeah, this is in the sci-fi fantasyland category for now... until it happens.

    9. Re:Engineering Culture by DerekLyons · · Score: 1

      You Sir (or Madam) win the prize for "most sensible post on the topic". I wrote one myself, but it pales next to yours.

    10. Re:Engineering Culture by Anonymous Coward · · Score: 0

      In the end, engineering culture is just a term being used to say, "technical shit that I don't understand well enough so I'lll use it as a scapegoat to justify my preconceived notions"

      Engineering Culture includes managment and the politics of grant funding. He's not asking for scientists to alchemically create unobtanium from oil impregnated sea water.

    11. Re:Engineering Culture by Anonymous Coward · · Score: 0

      The way I read it, I believe his point isn't so much that we have those technologies now and that some sort of 'engineering culture' is ignoring them, rather that a great deal of money was spent on what, then, was just as infeasible a pursuit as our 'better' alternatives now, but it was done because of a specific set of circumstances overcame the initial resistance and allowed that development to begin. Now that we've used that money climbing the hill we're on, we (not engineers, but the complex that drives this development of technology forwards including investment, etc.) feel obliged to continue with incremental upgrades that we can justify as 'only a little bit more' rather than find a way to eat the upfront cost (something of a disadvantage to begin with) to achieve the benefits down the track. To me, it's no different from the gambler's fallacy of being pot-committed. You've spent this much money already and it's just a little bit more, right? If you quit now you'll lose all that investment. It focuses on the near-term at the expense of the long-term and therefore shoots itself in the foot in the process.

      I am painfully aware, just as you are, that reality does not marry with dreams. Every day I have to face this in an engineering role also. We're bound by the shackles of what investment funding is willing to contribute to a new, unproven approach rather than 'just a little more' on what is a proven approach, to milk increasingly miniscule improvements out of it. For the investor, that's more attractive, as they're far more readily guaranteed a return on their investment. Sure, we see a committal to 'new technologies' in science budgets, but compared with the scale of what it takes to produce something like the Manhattan project, it is almost nothing.

      I think that's his point, however - without the unique set of circumstances surrounding the requirement to lob big, inaccurate bombs at communists halfway across the world, there was no significant pressure to drive the development of rockets at the rate and extent that they were. It took that seed of exceptional circumstances to get the ball rolling but once you overcome that inertia, investment comes far more readily as investors see a fairly good level of risk vs reward in sinking just a bit more money into milking an incremental improvement out of what is now an existing technology. Without that mammoth investment in what is quite possibly a dead-end by someone willing to take the risk, the seeds of such a technology cannot be planted. In this case, it was the US government driven to develop technology against a threat they could not even readily see, and therefore were making guesses from increasingly active imaginations as to what they were trying to outrun. Only in those circumstances can you really get such a great initial investment to get the ball rolling.

      The same thing manifests itself in clean energy production today, as just one example. We see far more willingness to throw money at 'clean coal' than different, relatively immature technologies that will work out better in the end if they prove successful. Why? Because coal energy production is already proven and therefore it's only a small incremental investment to take it that next, ever-diminishing step forwards. If we threw the same resources as the Manhattan project at clean energy production, I have no doubt we'd see amazing progress but the fact remains that there is not that incredible pressure there to drive such investment. Certainly, I don't know any Engineers who'd turn down a blank check to develop envelope-pushing technologies and ideas to solve existing problems (in any field), but it's not the Engineers who decide where the money gets spent. Sadly, it feels like the pressure required for explloring these radical, new approaches - ways to cross the valley to 'higher mountains' - will only come once people like US Congress find themselves having to wade through a metre of sea-water to enter parliament.

    12. Re:Engineering Culture by Anonymous Coward · · Score: 0

      To be fair, Neal has (at Blue Origin at the very least) worked side-by-side with groups of engineers and has, I suspect, developed some of those opinions about "engineering culture" practically, via that exposure. Aero-astro engineers in my experience tend to be rather conservative in nature.

    13. Re:Engineering Culture by mcswell · · Score: 1

      ...which is a nice segue to a comment I'd like to make. It's time we consider "rocket science" to have become "rocket engineering," and tell NASA to leave the engineering to commercial companies. Let NASA do the next science thing, which (IMO) ought to be to get us out of low earth orbit, in fact to get us away from the Earth entirely. That will take some new technology. Maybe it's ion propulsion, maybe some kind of atomic rocket; or maybe ion propulsion with the energy coming from a nuclear plant of some sort. If we had large ion engines that could propel a human-carrying spacecraft reliably for a period of weeks or months, then we could move around the Solar System at reasonable speeds, possibly even with reasonable accelerations (meaning the astronauts might not suffer from the effects of 0g).

    14. Re:Engineering Culture by theNAM666 · · Score: 1

      Have you, perhaps, taken a glance a Goddard's posthumous patents?

    15. Re:Engineering Culture by Anonymous Coward · · Score: 0

      For some of us it's more than that, unfortunately:

      Take an example of another culture, similar/related,
      so as to get a bit of distance:
      Medical culture.

      How many times have I come across a doctor disallowing healing/recovery because "that can't happen"?
      Lots.

      How many times have doctors harmed people because they COULD NOT ALLOW that someone's biology
      didn't obey Authorized Knowledge?
      Lots.

      Read the brain researcher V.S. Ramachandran's book "Phantoms in the Brain"
      and you'll read him railing against doctors REdoing a proceedure that DIDN'T WORK,
      because Universe MUST OBEY...

      He calls it insanity, btw...

      This is something both you & I have probably hit with medically conditioned professionals,
      but I've encountered it with business,
      with engineering,
      with medical culture, &
      with bureaucracy culture, too.

      Stuckness of mind is something that whole-meditation undoes,
      but just TRY getting meditation into the head of science or engineering culture:
      ~IT *CAN'T* WORK~ is the shove back.

      Have they done the experiment?

      Of course not!

      They DON'T NEED TO, because
      ~IT CAN'T WORK~...
      ( tautology being the basis of science, OR establishment, of course... )

      Perhaps you see a Pattern here...

      To understand what is being got at,
      WORK THROUGH, not just read,
      "The New Drawing on the Right Side of the Brain",
      and EXPERIENCE brain-dominance-shift, from
      linear/object
      dominance to
      at-once/totality
      dominance,
      and when you SEE how huge the other dimension of our knowing is, readily available,
      THEN you will begin hitting the mind-stuckness of the culture, & whole world, you/everyone live in.

      I hope you try it, because the other dimension of our knowing,
      that "education" snuffs to protect its importance, is HUGE!

      BTW, progress is huger & faster if one uses charcoals & toothy paper, instead of pencil.

      BTW2, R-Mind/L-Mind isn't mere BS, it's a result of EEG measurement:
      grandmaster chess players are different from run of the mill chess players by using both hemispheres.
      Leonardo da Vinci was the greatest engineer in the last thousands of years, and a painter.
      Miyamoto Musashi one of 2 ultimate level samurai was a painter.
      Winston Churchill was a painter.
      Even Adolf Hitler was an artist ( don't know if he painted, or if his stuff was all pastels/pencils, but I've seen some of his stuff ).

      Every science/engineering culture person I've challenged to do the experiment has told me they DON'T NEED TO do the experiment,
      because results aren't possible outside the dimension they know to be the ONLY valid dimension.

      Pathetic "science" they wear/commit, if you ask me...

      -shrug-

      I did it, though it took years to gain what non-autistics gain in days, and it eventually gave me the key to healing my own brain...

      which, of course, "isn't possible" according to the countless life-destroying doctors who reject that anyone can get better...

      how utterly fed-up with the intellectual belligerent-dishonesty our "meritocracy" is stuffed with...

      Anyway, give it a shot & you'll discover what I discovered,
      or don't & know what established ( stuck ) minds "know":
      the data's RIGHT THERE, for the having, for anyone who's got the mental guts to taste it...

      http://www.drawright.com/
      there should be a Before/After gallery there,
      SHOWING the mind-healing that happens in normals within 5 days...

      Cheers,

      Captain Obvious ( :

    16. Re:Engineering Culture by Anonymous Coward · · Score: 0

      Indeed, the main goal of every scientist or engineer (that I've ever met anyway and it certainly was my goal when I worked in the field) is to come up with something that would create a revolution. Unfortunately all the easy revolutionary ideas that work have already been thought up. There are tons of magic ideas and many scientists try them out as they get older just in case every other scientist before them was wrong. Turns out, they weren't wrong.

      There is no magic anywhere in the Universe, only ignorance.

      By the by, you probably don't want a small power plant that can produce a metric fuckton of thrust, because if you did have one, so would that crazy guy down the street that just got dumped by his girlfriend and wants to make a statement. The only thing that has kept humans around for this long is that they've been limited in the amount of energy that any single stray person has access to.

    17. Re:Engineering Culture by dr.newton · · Score: 2

      ...engineers working in the space launch industry are resistant to change just for the shits...

      You have an excellent rant, and I know there are many people who should read it.

      However, it seems like a straw man argument here, as TFA did not say that "engineering culture" is resistant to change without good reason, just that it's resistant to change. You seem to agree with this assessment since your post gives many very good reasons why engineering culture should be resistant to change. Change is hard, and you need to do it right.

      --
      Just another proletarian malcontent.
    18. Re:Engineering Culture by JSlope · · Score: 1

      May be if only more women were in engineering by now we would have flying saucers.

      --
      ResoMail - the alternative secure e-mail system
  31. Re:A nice addition to Jacob's (and Smolin's) Thesi by Anonymous Coward · · Score: 0

    You have just described Nietzsche's "Last Man".

  32. Re:I don't think his premises support his conclusi by amliebsch · · Score: 1

    I also agree with your "demonstrably." It's more like, we're standing on a hilltop. We think we can see - barely - higher hilltops through the mist. But we can't be sure it's not just a cloud.

    --
    If you don't know where you are going, you will wind up somewhere else.
  33. There is more effective fuel - 8 times payload by SergeyKurdakov · · Score: 1

    Rockets are no nearly perfect - given new fuel http://nextbigfuture.com/2010/12/swedish-researchers-have-discover.html shuttles could have 4-8 times more payload. And this is actually huge step. Next - launch could be performed from towers few kilometers hight or even mountains - it will take money - but still will make quite a change. There are other possibilities such as quad airship launch (walrus was designed for 500 -1000 tonnes - so the rocket could be 4000 tonnes of weight and could be launched, say from 15000 meters hight ), there are other, non rocket ways to launch things into space - but even rockets could be times more effective, than now.

  34. Re:Why aren't we trying something new? No unobtani by Overzeetop · · Score: 1

    A couple of decades before WW2, Robert Goddard suggested all of the rocket propulsion ideas to the US military, and they decided not to pursue it because they didn't believe the basic science which underlay his work. The Germans realized that he had, in fact, proven some basic concepts and expanded on his work.

    $4T has mostly gone into production and reuse of a great deal of the original innovation, not the innovation itself, and it's still dicey to send a person into orbit, all things considered.

    Technology has advanced an many areas surrounding the "other" options far more than rocket technology in the past 40 years. The problem is that there are limits to what we can do without radical advances which - based on our current knowledge - would likely violate some basic physical principles.

    --
    Is it just my observation, or are there way too many stupid people in the world?
  35. Re:Why aren't we trying something new? No unobtani by Xylantiel · · Score: 1

    Actually a launch loop seems pretty do-able to me, it just required a tremendous amount of investment. It would make access to space almost "free" as a result. This is the kind of thing he is referring to as prohibited less by physics and more by accounting.

  36. Re:Why aren't we trying something new? No unobtani by BJ_Covert_Action · · Score: 1

    The point of the article is that alternative launch methods may be beyond today's technology, but developing the technology of tomorrow would be a more worthwhile use of the resources that would otherwise go towards milking that last couple tenths of a percent of efficiency out of the technology of yesterday.

    See the funny part is that we are developing the technology of tomorrow. NASA is throwing money into contests designed to lay the groundwork for building a space elevator. The Air Force is currently testing hypersonic propulsion methods that could one day be utilized on an alternative launch platform. NASA and the Navy are both dumping money into tech like rail guns and mass accelerator cannons to see what can and cannot be achieved with them. Virgin, SpaceDev, and half a dozen other companies are looking into building space planes, eventually.

    Anyone who says that we aren't attempting to develop alternative space access methods currently is not looking hard enough. We are working, across the globe, to lower the cost of access to space by whatever means necessary. The problem is, getting out of our gravity well is hard. So developing this technology takes time, decades even, like rockets. Do we have space elevators, space planes, and orbital cannons? No. Are we working to get there one day? Yes. So I really don't understand what the complaint is, other than impatience.

  37. Re:He's right on how it started, wrong on why stuc by Cytotoxic · · Score: 1

    I thought the "space balloon" idea was pretty cool. The idea is to use a series of balloons to lift very large payloads to the edge of space. The final balloon would be very fragile and huge (to handle the super-thin atmosphere) and shaped as a lifting body. Ion thrusters would slowly accelerate the craft (and payload) to orbital speed. I don't know how much unobtainium is involved in the construction of the balloons, but it sounds pretty cool any way. I don't know that anyone has ever spent any real money on testing the idea.

  38. Re:A nice addition to Jacob's (and Smolin's) Thesi by sznupi · · Score: 1

    Said article is based upon bunk proposal of somebody who wishes for current working systems to be replaced by his system. Do you expect us to grant every such wish (when looking closer at engineering, even at physics, tells us they can't work...)

    From what I see, some people also tend to belittle all of current science and scientists mostly when too many of its aspects run counter to some "opinions" of said people... while the humanity is doing quite good (there is nothing wrong with "inertia" in such case). You can't know if we're not approaching relative stability of practically possible technology ... what is indeed the normal state for our species (interspersed with very few short bursts of progress). At the least, logic dictates that wishful thinking has limits.

    (medicine has social problems BTW - people, the patients care about their lives too much to simply trust evidence)

    --
    One that hath name thou can not otter
  39. We do have an alternative by Anonymous Coward · · Score: 1

    There is an alternative technology that Neal is probably thinking of. All studies of it done to date suggest it is better in every possible respect than rockets. Interestingly, it requires technology that was not developed until the 1990s - which means that even if history had gone differently we might not have it today.

    It's called laser launch. The vehicle still works like a rocket - there's propellant on board, and it gets superheated and escaping propellant generates thrust. However, since the energy source and nearly all of the technical complexity of the launch system stays ON THE GROUND where it can be as big and cheap and redundant as it needs to be, it reduces the cost of the system by orders of magnitude. The easiest and simplest laser launch system is a spacecraft with a block of metal bolted to the bottom.

    The lasers fire in pulses that create planar shockwaves acting like a rocket nozzle without the nozzle. Spacecraft lifts off. Technically the spacecraft could work without any onboard electronics or control systems of any sort. That is to say, no aerospace hardware AT ALL. Nothing made in a cleanroom with reams of paperwork speccing every part. Independent laser moduules would be made by whichver cut rate contractor offers the best price this week...a few errant beams or failed modules would not affect the launch.

    Since concentrated light can increase the temperature of the exhaust more, the rocket would be much more efficient and need less propellant for the same payload.

  40. The lock-in is physics. by blair1q · · Score: 2

    Everyone in the rocket business thinks of the alternatives all the time.

    And then looks at the laws of physics, and the laws of economics, and goes for the solution that gets the job done with minimal waste and effort.

    This isn't to say there's no waste or extraneous effort, but the main theme of the project isn't based on a fantastic boondoggle.

    And if there's more than one way to skin a cat, it will get tried eventually as someone realizes they do have the resources to attempt it.

    But while it may work for a niche, eventually you come back to the science of rocketry and the equations of motion and you decide that your rocket is going to look and act like a lot of others before it.

  41. advid.net: Better at snarky comments than physics by Weedhopper · · Score: 1

    I was going to write a snarky comment myself, but I decided to just do an obligatory snarky reference to a comic instead:

    http://xkcd.com/123/

  42. Canadians by DarthVain · · Score: 1

    tried to follow a different path and innovate using polar bears as rocket fuel, but as it turns out harvesting the critters is a really technical problem.

    We then figured out that we could piggy back arms on other space programs and did that instead.

    We were experiencing some problems shutting down our submarine thermal generator we used to limit the polar bear habitat, making them easier to catch, but we just blamed it in "Climate Change" and that seems to have solved the problem.

    Our scientists are off shoveling their driveways now and are unavailable for comment at this time.

  43. Stephenson's Rocket by Anonymous Coward · · Score: 0

    Seeing "Stephenson" and "Rocket" in the same headline, I couldn't help assuming it's about a steam locomotive...

  44. Re:He's right on how it started, wrong on why stuc by Animats · · Score: 1

    That's called a "rockoon". First tried in 1949. Works OK, payload rather limited.

    Back in 2004, JP Aerospace was pushing the idea of a permanent station at the edge of space which was really a balloon.They're still sending up balloons, but they're basically repeating what the USAF did in the late 1940s.

    Accelerating a fragile airship to orbital velocity at the edge of the atmosphere is a fantasy. If there's enough air to get lift, there's enough air to get drag.

  45. Re:Why aren't we trying something new? No unobtani by Intrepid+imaginaut · · Score: 0

    • Big gun? Workable, but you can't send anything fragile, including people

    Aha, that's simply because your gun isn't big enough. Consider an 11km high pylon tower, quite doable, with maglev tunnels in them to accelerate a vessel at 7g, quite acceptable again. The savings you make in fuel consumption and atmospheric density/turbulence are quite significant enough to lower the cost of launches to LEO to justify the initial expenditure, assuming you had a long term path to profitability in mind, like siting medical facilities in orbit for the rapid drop of transplant organs or something.

  46. Rockets not a "random pick" by Sinical · · Score: 2

    This is the crux of it, I think:

    To employ a commonly used metaphor, our current proficiency in rocket-building is the result of a hill-climbing approach; we started at one place on the technological landscape—which must be considered a random pick, given that it was chosen for dubious reasons by a maniac

    I don't agree that Hitler choice of rocketry for the V2 was random. I think he went to his not-yet-rocket scientists and said, "How do I deliver X kilograms of payload to England with such and such circular error probability, and oh yeah, it can't be intercepted?" And rockets were the answer. And for good reasons. I'm not sure what other technologies of the 1930s and 1940s could have performed the task: submarines with huge artillery built-in (susceptible to torpedo planes unless you could do some kind of shoot and scoot); they did try the bomber thing but that wasn't a winner; balloons don't seem like a possibility. We *still* don't have something better than rockets and missiles for mass producing corpses (whether you agree its a good idea or not): perhaps the Navy's upcoming railguns are different enough to be considered a "change".

    1. Re:Rockets not a "random pick" by davidbofinger · · Score: 2

      What happened was that Hitler went to his scientists and said, "How do I turn London into rubble?" And the scientists who worked for the Luftwaffe said, "Pilotless planes!" because that was the sort of technology they had and if it was chosen they would be in charge. And the scientists who worked for the Army said either, "A giant rocket!" or "A giant gun!" for the same reasons. And Hitler said, "Good, good, do all of those things." So instead of focus on one solution the Germans built the V-1, the V-2 *and* the V-3. And they all worked, more or less, though maybe none of them was a really good idea.

  47. Re:A nice addition to Jacob's (and Smolin's) Thesi by Weedhopper · · Score: 1

    This argument is and always has been horse shit, informed only by the view of those who are too myopic or narrow minded to see the quickening pace of technological advancements beyond their own limited world views.

  48. Epiphyte Corp by Anonymous Coward · · Score: 0

    Nice to see Randy and Avi back with a little conversation about rocketry:

    Avi: We could make a preposterous amount of money from communications satellites.
    Randy: It will be expensive to build those, but even so, nothing compared to the cost of building the machines needed to launch them into orbit.
    Avi: Funny you should mention that. It so happens that our government has already put $4 trillion into building the rockets and supporting technology we need. There's only one catch.
    Randy: OK, I'll bite. What is the catch?
    Avi: Your communications satellite has to be the size, shape, and weight of a hydrogen bomb.

  49. Takes all the power of the Hoover Dam. by maillemaker · · Score: 1

    There is a post above yours that says in order to launch an Apollo-type mission with lasers it would take all the power of the Hoover dam and then some, plus they would have to burn much longer than the 70 milliseconds or so they currently do.

    --
    A work that expires before its copyright never enters the public domain and thus enjoys eternal copyright protection.
  50. In any case, color me unconvinced by sean.peters · · Score: 2

    It was an interesting article, but there were a couple of parts that I thought were really weak. One problem area:

    To recap, the existence of rockets big enough to hurl significant payloads into orbit was contingent on the following radically improbable series of events:

    1. World's most technically advanced nation under absolute control of superweapon-obsessed madman
    2. Astonishing advent of atomic bombs at exactly the same time
    3. ...

    What? Surely step 2 was more or less a direct result of step 1 - there's nothing improbable about that at all. I omitted the rest of the list, but the sequence didn't seem all that improbable to me. In fact, I really can't even figure out how the concept of probability even applies to historical events. They're all unique.

    Another problem:

    There is no shortage of proposals for radically innovative space launch schemes that, if they worked, would get us across the valley to other hilltops considerably higher than the one we are standing on now—high enough to bring the cost and risk of space launch down to the point where fundamentally new things could begin happening in outer space.

    *crickets*

    Ok, Neal, care to explain to us what these radically innovative schemes might be? In addition to the parent's theory that institutional inertia is the reason (which is probably a big part of the answer), there's also the very real possibility that none of these other "radically innovative" schemes have any chance of competing with rockets on the basis of cost-effectiveness - because all the R&D on rockets is essentially done and paid for, whereas to "cross those valleys" would be simply enormously expensive. And there's no guarantee your radical new technology would work. I think the risk factor here is even more important than the problems of inertia.

  51. Re:Why aren't we trying something new? No unobtani by Anonymous Coward · · Score: 0

    Big gun sounds pretty good to me. Especially at two dollars a pound.

    Good lord, imagine all the incredible things you could do with just the ability to send cheap loads of water into space. Let alone massive quantities of reflective foil!

    Of course this incredibly cheap technology would make it real easy for our enemies to launch stuff at us. I guess that's why it had never been developed, aside from one they pointed at the ground and one that was dismantled in the first gulf war without ever being used. (maybe I should use some of that foil to make a hat)

  52. Re:Why aren't we trying something new? No unobtani by Prof.Phreak · · Score: 1

    How about a maglev train in a large circular vaccuum tunnel, accelerated to very high speed,... and then shot out horizontally into orbit? (how fast would it have to be shot out for it to leave earth orbit, irrelevant of air resistance---can't maglev get it to that speed in a vaccuum tunnel?)

    or... how large would a trebouchet have to be to launch a capsule into orbit?

    or... how about a huge slingshot (with a whole lot of rubberbands?).

    or... how about launching rockets from air balloons, e.g. if amateurs can get a camera up 30miles for $500 to take pictures... why not get the whole rocket 30miles up... and avoid wasting energy in fighting densest 30 miles of atmosphere? (also can accelerate much slower---due to vastly reduced air resistance).

    or... how about launching off a high flying airplane (sorta like in that new superman movie?)

    or... how about using small nukes to propel things? ... a gazillion of such ideas are unworkable, but some of them, if given enough thought and research, might just be practical, and long term, cheaper than current methods. So... who knows what the alternatives are...

    --

    "If anything can go wrong, it will." - Murphy

  53. You have your numbers backwards by sean.peters · · Score: 1

    Yeah, except your numbers are backwards. Rockets are nearly perfected technology - making little tweaks to them is not very expensive, and all the basic R&D is already paid off. However, developing entirely new technologies from scratch is very, very expensive. And you run the risk of them not working at all.

    So if your object is to get something into space in the relatively near future, are you going to go with a) the system that's already been extensively tested, has pretty good capability, and a known price? Or b) a system that hasn't even had basic R&D done (meaning you'll need to pay for that), might have either extremely good capability, about the same capability, or worse capability, and you have no idea what it will cost?

    I think the question answers itself.

  54. where "bang-for-the-buck"... by PaulBu · · Score: 1

    ... is to be taken quite literally for the first couple of attempts to launch an entirely new system! ;-/

    I was quite impressed that you can actually get launch insurance (but only for rocket launches, of course!).

    Paul B.

  55. I totally agree by sean.peters · · Score: 1

    He didn't so much as mention what these alternative technologies might be, and the only things I've seen have been pretty much pie-in-the-sky. It's far from a sure thing that there ARE any higher hills to climb, and even if there were, there's a good chance that getting from here to there would be cost-prohibitive.

  56. Dude, basic finance by sean.peters · · Score: 1

    If it requires a "tremendous amount of investment", then it can't be "almost 'free'". That investment would have to be paid off, and all the while, it would be competing with rocket technology that's ALREADY been paid off. Net result: rockets would be cheaper, so no one invests in the launch loop.

  57. Yes, but by sean.peters · · Score: 1

    ... dude, we've ALREADY SPENT the 4 trillion and ALREADY HAVE the rockets. What you're proposing is that we just dump all of that and spend another $4 trillion in the (not guaranteed) hope that you'll come up with something better? The GP is exactly right here.

  58. Right. by sean.peters · · Score: 1

    And amortized development costs for that will OBVIOUSLY be cheaper than our already paid for rocket technology.

    Your investment ideas intrigue me and I'd like a copy of your prospectus.

    1. Re:Right. by Intrepid+imaginaut · · Score: 1

      And amortized development costs for that will OBVIOUSLY be cheaper than our already paid for rocket technology.

      That was Stephenson's point - rockets are not cheap and they are pretty bad value with it. Better to spend some of that money on newer and better systems.

  59. Article Doesn't Make Much Sense by davidbofinger · · Score: 1

    The article illustrates why we don't love Stephenson for his engineering.

    These rockets, which were known as V-2s, were worse than useless from a military standpoint

    True enough, but rocket development doesn't depend on the V-2 alone. On the other side of Europe, for instance, we have the Russians hurling Katyushas. The V-2 was a direct development of German Army experience with rocket artillery.

    Atomic bombs turned out to be expensive, dirty, controversial, and of limited military use

    Really? There's no military use for an explosion in the kiloton range? How about, just as an example, dropping it on an enemy army headquarters?

    The rockets of the 1950s and 1960s were so expensive, and yet so inaccurate, that their only effective military use was lobbing bombs of inconceivably vast destructive power in the general direction of large urban areas.

    Katyusha again.

    because those bombs were so destructive (making it tricky to drop them out of a manned aircraft without killing the crew)

    Again, preposterous. Piston-engined propeller planes dropped atomic bombs without serious issue. Turbojets and turbofans just made it even easier.

    I love a lot of what Stephenson does, but societal and technological reasonableness isn't his focus. This article reads a lot like his books.

  60. Re:Why aren't we trying something new? No unobtani by Anonymous Coward · · Score: 0

    Lofstrom Loops and Space Fountains don't require unobtainium.

  61. Re:There is more effective fuel - 8 times payload by Anonymous Coward · · Score: 0

    A. There's a big gap between finding a new molecule and producing giant amounts of rocket fuel. They've only found tiny little bits of your magic fuel.

    B. Tall towers are structural nightmares. Tall towers meant to hold a massive beast of potential energy that will throw itself into orbit - lots more structural issues. Mountain locations are of limited use - you get more effective launches by moving closer to the equator. But moving closer to the equator means major political issues (noted in the article).

    C. Airship launch: possible, but complicated. More complicated = more ways to go wrong. There are several programs going on hybrid air-breathing/rocket combinations, Space Ship 2, etc for example.

    The article made a good point about us being near to the top of the conventional rocket curve, plus the amount of funding it takes to get new technologies built, scaled, certified, and commercialized.

  62. It's all true, but he left something out by SMACX+guy · · Score: 1

    I don't have planet busters until my scientists invent Orbital Spaceflight, and then that gets me these wonderful weapons deliverable only by rockets, never by needlejet or any other technology. And likewise, I don't have any other space tech until I have these rockets. Rockets are the key. You can't have planet busters or spaceflight without them.

    And trust me, no matter how hard you try to get along, there's always some pro-war nutcase who wants a vendetta. You must arm. That doesn't mean you have to nuke anyone, but you damn well better at least be trying to get the technology. He is so right about the evil genocidal leaders. Stuff just doesn't ever get done without these kind of people.

    One thing I was shocked to see Stephenson miss, though, is that you also need Pre-Sentient Algorithms. Orbital Spaceflight can't exist without it; it's a path dependency. (This is why, in the pseudo-reality (Earth simulations often played on the computers at the University) outside the true reality of SMACX, computer Science basically starts in the 1940s after you build something called Bletchley Park.) I cannot imagine how the author of Cryptonomicon, of all people, missed this.

  63. Re:Why aren't we trying something new? No unobtani by mosb1000 · · Score: 1

    I think the most realistic alternative launch technique is a rail gun like the one the navy recently demonstrated. You could use it at first to launch a scramjet vehicle up to the supersonic speeds it needs to begin working. Later as the technology develops you might be able to launch payloads at orbital velocities directly from the railgun. This would reduce the weight and size of the vehicles, and hopefully their cost along with it.

  64. He're one reason why that's party wrong by dbIII · · Score: 1

    In 1987 I was on the opposite side of the earth to Florida looking at a NASA funded scramjet that was being prepared to go into a NASA funded shock tunnel to be tested at mach 6. That team went to to do the Hyshot test a couple of years ago and the more recent US military scramjet test was also based on this work.
    I'm sure there are other promising leads that NASA is funding or others are working on elsewhere.

  65. Factually incorrect! by Cyberax · · Score: 1

    This article is factually incorrect.

    First, rockets were developed by the USSR before and during the war. http://en.wikipedia.org/wiki/Katyusha_rocket_launcher rocket launchers were used quite devastatingly on the Axis forces.

    Before the war USSR was experimenting with liquid rocket engines ( http://en.wikipedia.org/wiki/GIRD ) and later proceeded to develop the R-7 rocket which was used to launch the famous Sputnik-1. And no, it was done without significant contributions from the German engineers.

  66. Re:Why aren't we trying something new? No unobtani by badboy_tw2002 · · Score: 1

    "If anything can go wrong, it will." - Murphy

    Very nice contrast between post and sig :)

  67. NASA's Breakthrough Propulsion Project by Anonymous Coward · · Score: 0

    And yet for NASA's "Breakthrough Propulsion Project", NASA was only willing to part with $10,000.00 per suggestion. Where did the rest of the $1.6 million go. Surely, the website was not that complex. The message: "This society does not value the contributions of scientists and engineers."

  68. Re:Why aren't we trying something new? No unobtani by strack · · Score: 1

    you would think so, but thats because you havent put any thought into it whatsoever. do you know how difficult it would be to keep a cable going at mach 25, inside a flexible sheath, without it touching the sides? fucking impossible.

  69. Re:He's right on how it started, wrong on why stuc by nonguru · · Score: 1

    Didn't Arthur C. Clarke write about tethered space elevators as a substitute technology. (I think the original idea came from a Russian physicist.). I'm guessing the necessary materials or construction technology isn't available yet, not to mention the massive amount of capital to fund the infrastructure.

  70. Re:Why aren't we trying something new? No unobtani by strack · · Score: 1

    we need a rail assisted ssto rocket. the rail should give the extra boost needed to make ssto feasible.

  71. Re:Why aren't we trying something new? No unobtani by Anonymous Coward · · Score: 0

    Orion thermonuclear-pulse rocket?

  72. Re:Why aren't we trying something new? No unobtani by Bram+Stolk · · Score: 1

    I saw a documentary of a guy using lasers and plasma.
    The neat thing was that the engine, the laser, stayed on the ground, and kept shooting pulses at a metal cup. The result plasma pushed the cup higher and higher. He demonstrated it and it worked! Sure it was a small cup and the height was maybe 20m but the prinicple worked! Leave the heavy engine on the ground or in a low orbit, and you save the energy of having to launch it.

    --
    Bram Stolk http://stolk.org/tlctc/
  73. Re:Why aren't we trying something new? No unobtani by Anonymous Coward · · Score: 0

    modded down? really?

  74. Just tell the physics right and by advid.net · · Score: 1

    I was going to write a snarky comment myself, but I decided to just do an obligatory snarky reference to a comic instead:

    http://xkcd.com/123/

    This xkcd n123 is one of my favorites since a long time ! :D

    By the way : why do you imagine that I said there's nothing like a "centrifugal force" in a rotating system coordinates ?

    I kept it short but the long story is that :

    - The "centrifugal force" is not a force due to interaction of objects or fields but a correction term introduced to compensate the non-inertial frame choosen.
    - The author didn't mention any frame, he uses a non-inertial frame without thinking about it, and I'm not sure he knows what a non-inertial frame is and what using it implies.
    - Using the terrestrial reference frame for rocketry is terrible, not only you need the centrifugal pseudo-force but also the Coriolis effect. Instead of making things simple you dive in a nightmare.

    But this specific point isn't that much important, I think several other comments have pointed out what's wrong in his perspective, right from the begining of this /. story...

  75. Stephenson's Rocket by Dabido · · Score: 1

    Hmmm, wonder if we can get to the stars with steam engine power?

    --
    Sure enough, the cow costume was hanging up next to the superhero outfit and sailors uniform. (S,Spud)
  76. Pretty unimpressive by Anonymous Coward · · Score: 0

    Sure Neal, the accountants are to be blamed! Considering all your books I read, I'm pretty unimpressed with the article.

  77. Re:Why aren't we trying something new? No unobtani by Anonymous Coward · · Score: 0

    Launch Loop.

  78. Re:He's right on how it started, wrong on why stuc by HappyEngineer · · Score: 1

    Why isn't launching from an aircraft a big win? Rockets spend loads of fuel launching through the lower layers of atmosphere that planes can pass through with far less energy.

  79. Re:There is more effective fuel - 8 times payload by WildBlueYonder · · Score: 1

    According to this paper the specific impulse of this new fuel is actually lower than that of LOX and LH, and comparable to other rocket fuels, It is the density impulse which is 20-30% better. This means that the propellant mass wouldn't increase, although making a smaller, denser fuel source would lead to a smaller rocket overall, with mass and cost savings for the structure. Additionally it's lack of Chlorine would make it more environmentally (and worker) friendly than some of the propellant options, which is always nice. Unfortunately that paper doesn't go into production costs, or any possible issues with storing it (This paper looks like it may have more information along those lines, but I don't have a subscription). I don't know if it can sit in a tank at room temperature like Hydrazine, or needs special care like Oxygen (due to its molecular weight I'm guessing the former.) All in all it does seem like a nice stepping stone between the high functionality of LOX LH, and the economy and convenience of some of the other liquid fuels, but it doesn't appear to be a serious game changer in any way.

    As far as your suggestion to launch from buildings, mountains, or balloons, that doesn't actually offer substantial benefits either. While launching from high up would result in lower drag losses, that helps less than you'd expect because a ground launched rocket travels through the densest part of the atmosphere at it's slowest speeds. By the time a rocket is going fast enough that drag would really start to slow it down it is already at a pretty high altitude. If you are trying to make a cheaper rocket you really want to increase it's starting speed much more than its height. The math works out this way because of the fact that our starting radius is 6378 km. As big and impressive at Mount Everest seems to us it's really just a tiny pimple compared to the radius of the earth (brings you to 6386 km), and our entire atmosphere isn't much better.

  80. Re:There is more effective fuel - 8 times payload by SergeyKurdakov · · Score: 1

    and our entire atmosphere isn't much better. no, practically low earth transfer orbit starts at 150 km at this altitude a satellite will not decay into atmosphere for quite a while. and while at space station orbit there is also atmosphere - it does not change much - they just fix orbit every few days with quite a few amount of fuel. As for higher altitude start - it is actually already exploited in air launch. and building launch from mount will increase payload several times ( just check for existing projects ). the things I describe are not money wise - they really would require too much money to be spent relative to possible outcome - so currently it just make no sense. but not only rocket system are proposed - there are about a dozen of different future space launch proposals,

  81. Jules Verne was right...sorta by DanielRavenNest · · Score: 1

    Guns are an effective way to get things going, but not all the way to orbit, or escape velocity, as in his book. They are good for 50-75% of orbital speed, and the rest you do by some other method. Half orbital speed guns have already been built, decades ago, I got to visit several over the years. They just have not been built big enough to deliver useful payloads to space. That would require not trillions, not billions, but about the cost of one rocket launch (~100 M$).

    One big reason the major aerospace companies have not pursued things like this is that nobody ever got promoted by developing a scheme to launch stuff for 90% cheaper, which would cut your revenues by 90%. It has to be done by someone outside the current crop of vested interests whose *current* launch business would be decimated.