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Blimps... In... Space...

LandGator writes "MSNBC reports a California company with an alternate launch site in Texas, JP Aerospace, is on their third test of a blimp system specifically designed to fly to space. Blimps. To Space. At payload costs around a dollar a ton to LEO. Their concept, first unveiled at the Space Access '04 conference in Phoenix last month (with a blog report here, include the Ascender, a ground-to-near-space blimp, which docks to a helium-inflated two-mile-long station at the edge of space, over 20 miles up. Another ship, also a blimp but specifically designed to reach orbit, takes the payload from there to LEO, using well-proven electric propulsion (AKA 'ion drive'). That trip to LEO would take up to nine days, but that's a good thing; for, what goes up fast, must come down fast, and speed is energy which must be bled off by either massive amounts of expensive and explosive rocket fuel, or through ablative heat transfer which has its own problems (as we have seen before). JP Aerospace has flown many PongSats -- micropayloads the size of a ping-pong ball -- for balloon or rocket-launch. Over 1,500 PongSats have flown to date, which demonstrates a track record in near-space few of the X-Prize contenders can approach. Oh, yes, the Air Force is interested."

59 of 511 comments (clear)

  1. Cost to orbit by BWJones · · Score: 3, Interesting

    Well, if they can truly get cargo to space at a single US dollar/ton, this is orders of magnitude cheaper than current costs which run approx $10k/kg. Which could very well result in a total destabilization of the space launch business. (a little chaos now and then is a good thing.....yes?). Of course we also have maglev and space elevators which could also provide this a run for the money, but I suspect maglev would be more expensive and due to helium costs, space elevators might be cheaper still.

    --
    Visit Jonesblog and say hello.
    1. Re:Cost to orbit by confused+one · · Score: 3, Insightful

      ahhhh Helium... Why oh why must we always use Helium... Hydrogen is 1/4 the weight & therefor would have close to 4 times the buoyancy. Hydrogen is good...

    2. Re:Cost to orbit by the_mad_poster · · Score: 3, Informative

      Yea, good and explosive. While it may not be particularly dangerous to people, losing payloads to accidents involving hydrogen explosions in the atmosphere would jack the potential cost up.

      --
      Alito: A vote for Alito is a punch in the eye to put that bitch back in her place!
    3. Re:Cost to orbit by Sparr0 · · Score: 4, Informative

      uhm... no. hydrogen is 1/4 the weight and therefore has ((airdensity)-(heliumdensity))/((airdensity)-(heli umdensity/4)) the buoyancy. In this case the density of air is so much higher that the increase in buoyancy isnt even 25%, let alone the 300% you say.

    4. Re:Cost to orbit by kmac06 · · Score: 4, Informative

      Half the weight. Hydrogen is diatomic.

    5. Re:Cost to orbit by kpansky · · Score: 3, Insightful

      Right... because ROCKET FUEL is much more stable...

      --

      --Kevin
    6. Re:Cost to orbit by MrNovember · · Score: 4, Insightful

      Really. It's not like sitting on top of many tons of pressurized, igniting liquid oxygen and hydrogen is any more dangerous than sitting under a hydrogen blimp.

      I bet people just keep thinking of the Hindenberg.

    7. Re:Cost to orbit by angst_ridden_hipster · · Score: 4, Informative

      Although the Hindenburg is often perceived as an advertisement against hydrogen, it was, in reality, more of an advertisement against using cellulose nitrate or cellulose acetate to add rigidity to the skin of a dirigible.

      In all likelihood, it was the flammable nature of the skin that led to the ignition. Sure, having all that hydrogen there didn't help once the fire started, but there were a lot of successful hydrogen-filled blimps and dirigibles up to that point (the survival ratio was at least as good, if not better, than that of hydrazine or solid-propellant rockets).

      --
      Eloi, Eloi, lema sabachtani?
      www.fogbound.net
    8. Re:Cost to orbit by another_henry · · Score: 5, Interesting
      Actually I thought that, but when you run the numbers you find that helium is very close in terms of buoyancy for a couple of reasons.

      Firstly, helium gas goes round as a single atom, He, because it's a noble gas. Hydrogen goes as pairs, H2. This means that in a given volume at fixed pressure, you would have twice as many hydrogen atoms as you would heliums, so that brings the difference in weight down to 1/2.

      Secondly and more importantly, it's not actually the weight that counts. (Please if I've got this wrong, correct me, this is just from me thinking about it) The important thing is the difference in weight between e.g. a liter of air and a liter of helium/hydrogen.

      Air is mostly nitrogen which has mass no. 14. This means that 1 mole of N2 molecules weighs 28g. A mole of any gas occupies 24 liters at STP so air weighs about 1.17 g per liter. Running the numbers for He and H2 gives 0.16 and 0.08 respectively.

      Now, looking at the difference in weight, which is what determines buoyancy, helium gives about 1.01 g per liter while hydrogen gives 1.09 g per liter. Not such a big difference after all! I think that the advantage of non-flammability probably outweighs this minor difference in buoyancy. On the other hand, it may very well be easier and cheaper to produce hydrogen in bulk than helium.

      --
      "Studies have shown that people who eat peanuts live longer than those who do not eat."
    9. Re:Cost to orbit by afidel · · Score: 4, Informative

      Thank you. The stupid Hindenburg was the begining of bad science in the media. Due to the radio reports and the worldwide viewing of the recorded images of the disaster no formal inqury into the cause of the disaster was done. As we know now the skin of the Hindenburg was painted with what was essentially ROCKET FUEL. A small static discharge along a seam is the most likely cause of the disaster, the skin almost exploded and it wasn't until much later in the disaster when the envelopes tore open due to loss of internal structure that the Hydrogen had any affect on the fire. Not only that but no people were hurt by the hydrogen fire because due to hydrogens boyancy it would have risen to the top of the structure and burnt there.

      --
      There are 4 boxes to use in the defense of liberty: soap, ballot, jury, ammo. Use in that order. Starting now.
    10. Re:Cost to orbit by georgewilliamherbert · · Score: 4, Insightful
      Space Elevators == folly.
      The problem is, you have to keep it up and stable. Major danger given the forces involved.
      I wish ignorant people would stop saying that.

      They're almost certainly dynamically stable in position and tension.

      And when it fails, it's a total catastrophe.

      I wish ignorant people would stop saying that, too.

      It's going to be a thin ribbon of probably carbon nanotube fibers. How much ribbon do you need to drop on someone to hurt them?

      Common retort: Oh, but it's falling from orbit

      What is the terminal velocity of a strand of ribbon? Do you have a one story building's roof available to demonstrate this to yourself?

      Most of it, falling down, will burn up in the upper atmosphere. That which does not, will fall so slowly by the time it reaches ground level as to pose no threat to anyone on the ground, unless you tangle yourself up in it after it lands or it happens to catch an airplane on the way down.

      Screaming terror scenarios of huge swaths of land ruined by explosive impact are bad science fiction not fact. No competent professional has ever said such a thing. It just plain will not happen.

    11. Re:Cost to orbit by Coz · · Score: 3, Informative

      Yes. Atomic oxygen (O1), standard diatomic oxygen (O2, the kind we breathe), and ozone (O3, the kind the blocks UV and gets eaten by fluorocarbons). O1 and O3 are very reactive, but nothing that a hydrogen balloon should have to worry about, so long as it contains most of its hydrogen.

      Of course, one of the other great benefits of helium over hydrogen is that helium is MUCH more containable - He stays inside Mylar envelopes a lot longer than H, which has been known to burrow its way out of multi-layer metal/ceramic containers thanks to its small atomic size.

      --
      I love vegetarians - some of my favorite foods are vegetarians.
    12. Re:Cost to orbit by portforward · · Score: 5, Insightful

      Actually the Hindenburg probably wouldn't have blown up or burnt nearly so quickly IF THEY DIDN'T PAINT IT WITH ROCKET FUEL. (oh the irony) Hydrogen will burn with a flame that travels upwards.

      No, the only safety concern that I have with Hydrogen is that it tends to escape from a confined space much more quickly than does Helium.

    13. Re:Cost to orbit by Greedo · · Score: 4, Insightful

      Also, I remember reading a while ago that the earth's helium resources are pretty limited. Any helium that escapes into the atmosphere isn't coming back. Ever.

      So, once we use the helium we have, we aren't getting any more. One source says this may happen by 2030.

      Found some googled info here and here and here.

      --
      Tuus crepidae innexilis sunt.
    14. Re:Cost to orbit by Thuktun · · Score: 4, Interesting

      What is the terminal velocity of a strand of ribbon? Do you have a one story building's roof available to demonstrate this to yourself?

      While I tend to agree with your overall claim, this particular comparison doesn't seem all that straightforward. That's the terminal velocity of an infinitesimal fragment of the overall tether.

      Small pieces tend to flutter in the breeze. Would a mile's length of tether also flutter? Much less so, at least in the middle, since any given small length of the tether would need to pull on the parts above and below it to move out of position. I'd be interesting to see a computer simulation of this.

    15. Re:Cost to orbit by mindstrm · · Score: 3, Interesting

      Seems not to be a problem.

      When the blimp is staying up via buoyancy, it's still in atmosphere by definition. If there is atmosphere of any sort, it's rather unlikely you will find high velocity paint chips or other things.. they would quickly slow down, burn up, etc.

      When the blimp is OUT of the atmosphere, at orbital velocity, it is no longer staying up there via buoyancy, and puncturing it's gasbags would not really be an issue as far as staying up there goes.

    16. Re:Cost to orbit by Spoticus · · Score: 3, Funny

      What is the terminal velocity of a strand of ribbon?

      African or European ribbon?

    17. Re:Cost to orbit by ahfoo · · Score: 4, Informative
      WElp, I did a bit of research as well and you're right that it does leave the Earth, but your tone of urgency, which I'm assuming, may be a bit displaced.

      Helium makes up about 0.0005% of the earth's atmosphere. This trace amount of helium is not gravitationally bound to the earth and is constantly lost to space. The earth's atmospheric helium is replaced by the decay of radioactive elements in the earth's crust. Alpha decay, one type of radioactive decay, produces particles called alpha particles. An alpha particle can become a helium atom once it captures two electrons from its surroundings. This newly formed helium can eventually work its way to the atmosphere through cracks in the crust.
      Quoted from education.jlab.org

      So, yeah, you're right it's leaving, but it's also being replaced by natural radioactivity so that even after all the hydrocarbons are used up, natural gas wells will still be producing helium for millions of years.

      According to Praxair, fifty percent of current natural gas consists of helium. So, it's not all that rare which helps to explain why it's not all that expensive.

  2. Only since 2002? by Mz6 · · Score: 5, Interesting

    What's even more amazing is they have only been around since 2002. Going from start-up company to your 3rd test flight in that amount of time is.. well.. impressive.

    --
    Hmmm.
  3. x-prize by Capt'n+Hector · · Score: 4, Interesting

    Eh? That's the coolest thing I've seen in a while, if it's at all possible. Kinda blows the x-prize away.

    --
    Quid festinatio swallonis est aetherfuga inonusti?
    Africus aut Europaeus?
  4. Oh the humanity by daeley · · Score: 3, Funny

    on their third test of a blimp system specifically designed to fly to space

    "Now, the object of this expedition is to see if we can find any traces of last year's expedition."

    --
    I watched C-beams glitter in the dark near the Tannhauser gate.
    1. Re:Oh the humanity by daeley · · Score: 4, Funny

      I am imagining this thing getting a hole from a micrometeorite and going fllurruurpptpppthhh around the globe like a punctured balloon in your living room, whacking into San Francisco, slobbering over Addis Ababa, sliming Machu Picchu, bouncing off Sidney before coming to rest sadly draped over the Eiffel Tower. Of course.

      --
      I watched C-beams glitter in the dark near the Tannhauser gate.
  5. NOT a dollar/ton by SeanTobin · · Score: 4, Informative
    The price is NOT a doller/ton. It is a dollar per ton/mile.

    Incase there are actually people not reading the linked article, the interesting part is quoted here:
    Blimps into space looks insane but they have flown some of the parts of a 3 stage to orbit system and they are talking about costs to space of a dollar a ton/mile.
    --
    Karma: SELECT `karma` FROM `users` WHERE `userid`=138474;
    1. Re:NOT a dollar/ton by rmohr02 · · Score: 4, Insightful
      The price is NOT a doller/ton. It is a dollar per ton/mile.
      Correct. However, it is still an order of magnitude cheaper than conventional ways of getting cargo into orbit.
    2. Re:NOT a dollar/ton by Capt'n+Hector · · Score: 4, Informative

      So that makes it ~$1,000 per ton to LEO. That's still WAY cheaper than current rates.

      --
      Quid festinatio swallonis est aetherfuga inonusti?
      Africus aut Europaeus?
    3. Re:NOT a dollar/ton by Bingo+Foo · · Score: 3, Funny

      Which is pretty close to an order of magnitude of orders of magnitude.

      --
      taken! (by Davidleeroth) Thanks Bingo Foo!
    4. Re:NOT a dollar/ton by NoMoreNicksLeft · · Score: 4, Funny

      Wow. Here I was, ready to put a 1 ton satellite into orbit for $1. Instead, I find out it costs nearly $200. You've dashed my hopes of becoming a private space power. Damn you.

  6. Can I have a Giraffe? by g0nk · · Score: 5, Funny

    I would love to see huge balloon animals in the night sky..

  7. It... is... BALLOON! by pedantic+bore · · Score: 3, Insightful

    Or maybe I'm the only person who remembers F-troop. Seriously, this is going to be a bit weird, because at that size, it's going to be quite visible all the way up, even in orbit.

    --
    Am I part of the core demographic for Swedish Fish?
  8. Couple of things... by Skyshadow · · Score: 5, Interesting
    First, an error I noticed: It's not $1/ton to LEO, it's $1 per ton/mile. It's still really low, but it's a pretty significant difference.

    Second, LEO isn't just *up*, it's also speed that keeps you falling back to earth. That kills the up-fast-down-fast idea. Are these space blimps (inflatible tech! Dr. Schlock would be proud) going to manage to accelerate a load from a relative standstill to LEO speeds using an ion engine (which has very weak acceleration) in just a few days? Unless I'm missing something, that doesn't seem very likely.

    That aside: Cool idea. This sort of infrastructure wouldn't be as awesome as a space elevator would be, but it sure seems a hell of a lot more likely (cheaper, safer, possible without huge leaps in materials, etc). Once you're moving tons of material to orbit for a very small price (costs more to ship something across the ocean!), it seems like space exploration is ready to take off (no pun inte... oh, who am I kidding?) in a very real way.

    --
    Every year during my review, I just pray the words "slashdot.org" aren't mentioned.
    1. Re:Couple of things... by Tyler+Eaves · · Score: 5, Informative

      Well, let's work it out. Assuming an ion Drive can produce a net thrust of 0.01g (.0931 m/s). LEO is around 7600m/s. That gives 81362 seconds, or 22 hours. Obviously they're planning on much lower accelerations than even that, but low forces build up over time.

      --
      TODO: Something witty here...
  9. Blimp Cruises by ChowyChow · · Score: 5, Interesting

    I can't way until they offer nine day cruises to near-space.

    Imagine the view...

    Seriously, this is a good stepping stone to space tourism.

  10. Re:LEO? by apraetor · · Score: 3, Informative

    Low Earth Orbit.

  11. Probably not X Prize contenders. by mr_mischief · · Score: 3, Insightful

    This is neat, but too bad it wouldn't work for the X Prize. If it takes 9 days to get up there, then comes back slowly too, they wouldn't be able to relaunch the same craft in time. That's a shame, as this sound promising and could really use the extra funding from the prize itself and that the prize's notoriety would help it get.

    Hopefully this solution will be developed and used commonly when fats times to orbit aren't a must.

    1. Re:Probably not X Prize contenders. by g0nk · · Score: 5, Funny

      just carry a saftey pin with you on the way up, that'll get you down quicker... ;)

  12. Re:LEO? by Anonymous Coward · · Score: 4, Funny

    It's like a Sagittarius, only friskier.

  13. Great... by Faust7 · · Score: 5, Funny

    So the first word visiting aliens will see will be "Goodyear."

  14. WTF? by wwest4 · · Score: 4, Interesting

    I'm sure they have thought this out, but:

    Can you really accelerate a big inflated condom to escape velocity with an ion drive? I mean, it can only get so high on He, and I'm assuming that at its apogee there will still be an appreciable amount of atmosphere. Would an ion drive be able to overcome the drag force? Anyone willing to do the math?

    1. Re:WTF? by Froze · · Score: 4, Informative

      Your question begs multiple misconceptions.

      First, escape velocity is about getting you permantly out of earths gravity well. Not something you want if your destination is a stable orbit around the earth.

      Second, escape velicity is a ballistic value, ie. the speed required to kick your butt off the planet from ground level going straight up.

      Third, pushing "a big inflated condom" around in the upper atmosphere is not really a problem since there isn't much air to create drag.

      Further, the higher you go, the less drag you feel, hence the "launch" of the orbiter from a platform already 20 miles up.

      --
      -- The morphemes of your disquisition are ascertainable, but they have eschewed an ambit of transpicuous exposition.
  15. Re:Potential for a disaster by apraetor · · Score: 5, Informative

    The Hindenburg was filled with hydrogen, not helium. Hydrogen burns, helium does not. Besides, the Hindenburg was painted with some rather flammable compounds..

  16. I'm a bit confused by this statement: by Vellmont · · Score: 4, Interesting


    That trip to LEO would take up to nine days, but that's a good thing; for, what goes up fast, must come down fast


    What goes up fast must come down fast? Unless I'm missing something, low earth orbit still means going several thousand miles an hour. The rate you ascend at has nothing to do with how quickly you'd come down at.

    --
    AccountKiller
  17. Up-fast-down-fast? by Syberghost · · Score: 4, Insightful

    Whether you reach orbital velocity in 9 days or 9 minutes, you're still travelling at orbital velocity.

  18. Pong Stats by proudlyindian · · Score: 3, Funny

    Pong statistics for leo.space.com:
    Balls: Sent = 2002, Received = 1001, Lost = 1001 (50% loss)

    Striving to be common

  19. Helium vs. Hydrogen by mbessey · · Score: 3, Interesting

    Hydrogen is half the density of Helium, not 1/4. And it wouldn't give anything like twice the buoyancy, either. If you're confused as to why this should be so, I recommend doing a little web research on the following terms: "monatomic gas", "chemical mole", "ideal gas law". "density of air".

    -Mark

  20. Re:Altitude != orbit -- The beginning of the end by stripe · · Score: 5, Informative

    That is what the ion engine is for. They calculate it will take 9 days to acclerate the craft to 8km/s.

  21. Blimps do not necesarily crash due to leaks by tarranp · · Score: 3, Informative

    People have a misconception that if you put a hole in a blimp, that it crashes. If properly designed it will not.

    It all comes down to the pressure difference between the insides and the outsides of the blimp.

    Reading their promotional literature, they do not maintain much of a pressure difference between the insides of the blimp and the outsides. Thus, a hole will not really result in the helium being replaced with the heavier atmospheric gases.

    Most blimps can manage a safe emergency landing if even significantly damaged.

    Last but not least, I suspect that their choice of helium was more due to the dramatic reduction in safety precautions they have to take with the stuff on the ground. There are real advantages to using diatomic gases over monotomic gases (for example, they leak much more slowly through micro-pores). But the advantages do not make up for the disadvantage of the risk of explosion on the ground or at low altitudes.

    1. Re:Blimps do not necesarily crash due to leaks by Oculus+Habent · · Score: 3, Informative

      I suppose that once you get to LEO, it's not so much of an issue, as whatever the blimp is carrying may be able to propel itself into higher orbit.

      My understanding of blimps is that they use equivalent pressure - hence the airsacs that allow pressure changes as they rise - and rely on the buoyancy of lower weight at the same pressure.

      I'm just thinking of a blimp on the edge of space suddenly getting hit with a small projectile traveling 1000+ miles per hour. That could do some serious damage. Aside from making a hole, the force of impact might well deform the ballon, rapidly forcing gas from it. This is unlike most damage that occurs with conventional blimps. And, the additional height exacerbates the issues with blimps, giving them more time to slowly leak as they descend and more time to accelerate.

      --
      That what was all this school was for... to teach us how to solve our own problems. -- janeowit
  22. RTFM... by TheSync · · Score: 3, Informative

    http://www.jpaerospace.com/atohandout.pdf

    Here are the details:

    Atmospheric airship with crew of three takes payload to 140,000 ft. Airship uses lift and buoyancy, and driven by propellers designed to operate in near vacuum.

    Dark Sky Station (DSS) at 140,000 ft. Permanent, crewed facility.

    Airship that flies from DSS to orbit. Over a mile long. Uses buoyancy to climb to 200,000 ft. From there uses solar/electric propulsion to reach orbital velocity over several days.

    Continuing to use solar/electic propulsion, it can keep on going to anywhere in the solar system.

    Several "DSS" platforms have been flown. All equipment has been flown at 100,000 ft. and tested in the environment. Ion engine tests of the orbital airship at 120,000 ft. will occur in the next five months.

    Every segment of the plan has funding. DoD is funding the atmospheric airship for reconnaissance. Telecom companies are funding DSS.

  23. Re:Potential for a disaster by Mannerism · · Score: 4, Insightful

    Hindenburg, anyone?

    Man, I'd hate to be in the blimp industry. Give a dog a bad name, or what? One big accident almost seventy years ago and every time somebody suggests a blimp as a solution to anything, everybody assumes it's a fiery disaster waiting to happen. It's as if we'd all given up on ships after the Titanic.

  24. NOBODY'S SEEN THE IMPLICATIONS? by alizard · · Score: 4, Interesting
    From what I've seen here, what's left to do on the project is development, the proof of concept is already done.

    If enough money is put into the project, we can start space industrialization in a year or three, we don't have to wait until we find out if the space elevator is actually possible, we don't have to build giant rail guns for cheap space launches if the Elevator is unworkable.

    It's time to start work on actually building Space Power Satellites at the "proof of concept" level. For more info, click here

  25. Re:Advanced Materials by LaCosaNostradamus · · Score: 3, Interesting

    The blimp in Stephenson's The Diamond Age was filled with vacuum, and a cyberpunk author did something similar with tall buildings in one of his books (building tops were large balloons whose lift helped support the building weight so the thing could carry more floors).

    This is different than a gasbag put into a vacuum. Stephenson's blimps were under compression, and the proposed blimp-in-space is under tension.

    Compression's a bitch. Holding a 500-foot-dia sphere in enough equalized compression to avoid buckling and collapse is insanely difficult, which is why nanotech was the narrative used to justify it. But tension? Ha, tension's a walk in the park particularly for materials formed into skins.

    Just eyeballing it, we have more than enough common materials like mylar that can produce a gasbag of sufficient size (i.e. common Goodyear blimp). If the tension proves too much for mylar, then some strenghtening can be done like sail makers do all the time, with carbon-fiber thread wrappings, etc. But my rule-of-thumb gets hazy for things that are kilometers in size under the gas pressures they must contain, since tension rises appreciably with the radius of curvature.

    --
    [You have a stable society when some nut guns down a schoolyard and the law doesn't change.]
  26. Re:Helium non-renewable by Teahouse · · Score: 3, Informative

    Actually it is. Any Nuclear reactor can be tuned to produce Helium. I think they did this briefly at the Laurence Livermoor reactor for a short time before decomissioning it.

    --
    "Curiosity killed the cat, but for a while I was a suspect."- Steven Wright
  27. Re:Crap? by Anonymous Coward · · Score: 5, Informative

    This is stupid, I swear noone has any vision.

    First, they're talking about 20 miles up for this two-mile 'lily-pad'. At 20 miles, we still have atmosphere, so we still have buoyant(sp) forces acting. Since there's a buyoant(sp) force at work, orbital mechanics can be damned. Your airship doesn't fall back to Earth because it's lighter than air.

    Are you with me, then? You have a lovely two-mile long launch platform. From here, you launch another, smaller balloon with even less density and a few ion engines. This smaller balloon floats up as high as the remaining atmosphere allows. At this point, we'll say that the balloon is 'floating' on the very top of the Earth's atmosphere. It won't go down (buyoant[sp] force) and it won't go up (gravity). At this point, as long as the ion engines can beat the force of gravity, you have acceleration.

    Acceleration, even small amounts of it, mean a lot in a vaccum. Give it a couple weeks and you'll find yourself speeding along at 8 km/s. Let go of the object you want in orbit and use the same ion engines to slow down. Physics being what they are, you should wind up back where you started with the same amount of velocity as when you left. At which point, you'll be 'floating' on the top of the Earth's atmosphere and you can manipulate your airship to get back down to the 20-mile-high 'lily-pad'.

  28. Space cruise? by MAXOMENOS · · Score: 3, Interesting
    $1/ton/mile for cargo.

    Figure a fully outfitted luxury passenger module, including oxygen and other facilities, is ten tons per passenger.

    That's $200 per passenger to get to the "edge of space", or $9000 per passenger for low earth orbit.

    Space cruises for civilians now become feasible.

    Pretty exciting.

  29. No way. Unfortunately. Way too much drag by Thagg · · Score: 3, Informative

    This blimp needs air for bouyant lift, so you are inevitably going to be in the atmosphere. Ion engines, unfortunately, only work in a vacuum. And even if they did work at that altitude, the drag would so high that they wouldn't accelerate the ship at all.

    If the ship was, say, 50 ft wide and had a rediculously low drag coefficient of .01, then the drag force at 5000 fps, 1/5 of orbital velocity, is: .5 rho Cd V^2 A

    where

    rho is density (about 1.7x10^-5 slugs/ft^3)
    Cd is .01
    V^2 is velocity squared. At 5000 fps, that's 2.5x10^7
    A is area, 50 ft

    This yeilds a drag of a little more than 100 lbf.

    The most powerful ion engine is Nasa's new HiPEP that has a thrust of about 1/10th of a pound.

    Now, I'm a big fan of JP Aerospace, and wish them all the luck in the world. Their program of launching sounding rockets from high-altitude balloon platforms was quite exciting. Hypersonic blimps, though, are just not going to happen.

    Thad

    --
    I love Mondays. On a Monday, anything is possible.
  30. Re:No way. Unfortunately. Way too much drag by wwest4 · · Score: 3, Funny

    I came up with a similar result. Maybe we should just shut up and short the stock later on. :)

  31. Re:Weight, profile and wind by barawn · · Score: 3, Insightful

    Does the name Tacoma Narrows ring a bell?

    Yes, it does. And it did to the people who looked at the space elevator as well. The Tacoma Narrows bridge fell because the period of its resonant frequency happened to be close to a naturally occurring oscillation.

    In order for resonance to be a serious problem, the induced oscillation has to occur over the entire object, and it has to be close in period to the natural frequency of the object.

    The fundamental period of the space elevator is 7 hours. There's nothing which occurs on the full scale of the elevator (hundreds of thousands of kilometers) which is near to 7 hours.

    So induced oscillations aren't a worry.

    (Wind oscillations are a non issue if they don't rip the ribbon. The ribbon is huge. The atmosphere is just a tiny sliver compared to its full length.)

  32. Re:No way. Unfortunately. Way too much drag by tsotha · · Score: 3, Informative
    You are assuming this thing is going to be a bigger, thinner Goodyear blimp. According to what I've read (and look at the picture), part of the idea here is the shape of the craft is supposed to generate lift. So by the time it's going 5000 fps it'll be far above its original altitude with very little drag.

    Yes, I know you won't get aerodynamic lift without air, so there will be some drag, but your back-of-envelope calculation doesn't tell enough of the story to know if it's a showstopper.

    My question is how the heat gets dumped on the way back. I guess it has so much surface are the heat load at any given point is small, but we're not talking about titanium here.

  33. Gravity in the blimp space station by w3woody · · Score: 4, Interesting

    I don't know if anyone has noticed this, but at the "dark sky station" stationed at 100,000 feet up, since the station is floating rather than orbiting, there is no issue with zero gravity. Weightlessness is caused by the fact that an object in orbit is "falling" to the earth--and missing. But the "dark sky station" is not in free-fall; it's held aloft via bouyancy, and so workers on the "dark sky station" will experience full gravity. No problems with muscle atrophy.

    Furthermore, it's not like poeple haven't flown up to 100,000 feet up in balloons; what becomes technically interesting is building a permanent or semi-permanent station as a balloon at that altitude.

    The best part is that the worlds record for the highest skydive is above that altitude. So theoretically in the case of a catestrophic emergency, people could simply get into their skydiving space suits, and jump.