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SpaceShipOne Completes Second Test Flight

waynegoode writes "According to an article at Space.com, Scaled Composites' SpaceShipOne suborbital rocket plane made its second powered flight today. The piloted vehicle was powered by a hybrid rocket motor to over 105,000 feet. The engine burned for 40 seconds, zipping to Mach 2. SpaceShipOne is one of several projects competing for the $10 million X Prize. Slashdot mentioned yesterday that it received a license from the FAA, the first license for a suborbital rocket."

194 comments

  1. Good luck to them! by erick99 · · Score: 5, Insightful
    This is a very exciting project to watch. Clearly Rutan and company are not entirely doing this for the money as they have easily spent more than the $10M prize already. They must be pretty serious as they have applied for DOT/FAA permits, according to the article:

    Just yesterday, the U.S. Department of Transportation (DOT) announced it had issued the world's first license for a sub-orbital manned rocket flight.

    The license was issued April 1 by the DOT's Federal Aviation Administration's Office of Commercial Space Transportation to Scaled Composites. This federal paperwork green-lighted a sequence of sub-orbital flights by Scaled Composites for a one-year period.

    The license to Scaled Composites is the first to authorize piloted flight on a sub-orbital trajectory, the DOT statement noted.

    I hope we are able to witness this "...piloted flight on a sub-orbital trajector.."this year!

    Happy Trails!

    Erick

    --
    http://www.busyweather.com/
    1. Re:Good luck to them! by RedWizzard · · Score: 3, Insightful
      Clearly Rutan and company are not entirely doing this for the money as they have easily spent more than the $10M prize already.
      You are right that Scaled Composites will have spent more than $10M. I've heard that their budget is $30-40M. But they are trying to develop a commercial venture so they are certainly "in it for the money", not the X-Prize (although that will obviously help), but the money to be made in space tourism.
    2. Re:Good luck to them! by Bobdoer · · Score: 4, Funny

      Personally, I hope that SpaceShipOne does much better than RealPlayerOne.

    3. Re:Good luck to them! by quantaman · · Score: 2, Insightful

      Clearly Rutan and company are not entirely doing this for the money as they have easily spent more than the $10M prize already.

      They indeed might not be doing it entirely for the money but that is hardly evidence. From the start I've considered the $10 million to be more of a publicity stunt, an incentive to speed the projects along a little bit, and some startup cash so some company doesn't win and go bankrupt before they start selling tickets. Who ever gets there first is going to get huge publicity and they will be the first to sell tickets to all the hollywood superstars who want to go into orbit. The $10 mil is good for startup but they, and a lot of the other X-prize competitors who make a sucessful ship, will be raking in way more than that once they start carrying paid passengers.

      --
      I stole this Sig
    4. Re:Good luck to them! by Gropo · · Score: 2, Funny

      This would be the RealOne equivalent...

      --
      I hate Grammar Nazi's
    5. Re:Good luck to them! by WindBourne · · Score: 1
      I suspect that they will
      1. Start selling tourists packages to millionare +.
      2. scale the 2 ships up so that they can get to orbit.
      --
      I prefer the "u" in honour as it seems to be missing these days.
    6. Re:Good luck to them! by sponge_absorbent · · Score: 1

      The current round of X-prize entrants wont be sending anyone into orbit for a while. Just a little over 100km up then down again.
      However, one could argue that hollywood superstars wouldnt know the difference, as long as the 'special effects' were good enough ;)

    7. Re:Good luck to them! by Anonymous Coward · · Score: 0

      Are you sure it's space tourism? Low-altitude surveillance, weather and scientific satellites present a much bigger market.

    8. Re:Good luck to them! by 3waygeek · · Score: 1

      Well, American Express is already offering a suborbital flight as a membership reward (only 20,000,000 points!) through Space Adventures. Neither Rutan nor Scaled Composites appear to be involved in this venture.

    9. Re:Good luck to them! by pfdietz · · Score: 1

      Scaling up the vehicle won't change the fact that it doesn't have anywhere near the delta-V needed to reach orbit, or the thermal protection to survive reentry at orbital speeds.

    10. Re:Good luck to them! by DerekLyons · · Score: 1
      You are right that Scaled Composites will have spent more than $10M. I've heard that their budget is $30-40M. But they are trying to develop a commercial venture so they are certainly "in it for the money", not the X-Prize (although that will obviously help), but the money to be made in space tourism.
      Nope. Burt Rutan has stated on many occasions that he is not building SS1 as a commercial venture, but because someone (Paul Allen mostly) paid him to do so. He has no interest in running a commercial or tourist program whatsoever. Now Mr. Allen and his fellow investors may have other plans, but Mr. Rutan isn't in them.
  2. Anybody else still in the running? by LostCluster · · Score: 4, Interesting

    As only a casual X-Prize follower, SpaceShipOne is the only X-Prize contestant team name I can come up with off the top of my head now.

    Is there any other team that's anywhere close to keeping SpaceShipOne's pace, or are they now the presumed winner of the X-Prize unless they really stumble?

    1. Re:Anybody else still in the running? by SpyPlane · · Score: 5, Informative

      How about our favorite FPS gaming programmer turned rocketman John Carmack's Armadillo Aerospace?

      http://www.armadilloaerospace.com

      Wow, that was a big possesive noun.

      --
      "We need a fourth law of Robotics: Stop Fingering My Wife"
    2. Re:Anybody else still in the running? by Carnildo · · Score: 4, Informative

      SpaceShipOne is the most likely winner, but Armadillo Aerospace is also trying for a launch this year, and could potentially beat SpaceShipOne.

      --
      "They redundantly repeated themselves over and over again incessantly without end ad infinitum" -- ibid.
    3. Re:Anybody else still in the running? by JT27278 · · Score: 2, Insightful

      www.armadilloaerospace.com

    4. Re:Anybody else still in the running? by MrBlue+VT · · Score: 5, Informative

      I've been following Armadillo about every week on their news page for the past year. I like their dedication and method of building a ship.

      They have however spent a lot of time dealing with engine issues. They've already had to go from a 90% peroxide monopropellent design to a 50% peroxide/methanol mixed-monoprop because FNC (one of the few companies that make 90% peroxide) wasn't willing to sell it to them. They've spent a lot more time dealing with designing the engines than they anticipated. Just goes to show, rocket engine design is not simple!

      Other issues include how to get the thing back on the ground safely. They initally planned to use a big ass parachute to land it, but they found out that this really restricts them in terms of getting a launch license. Because there is a possiblity for such huge range drift with the parachute design (thus endangering public safety since it can land in a huge footprint) that they've now had to think about doing a powered landing using the engines. This of course, leaves much less room for error on landing. An alternative would be to have the pilot bail out and parachute down while the ship lands by itself, but again this adds complexity.

      Although I'd love to see them win, the fact is, Rutan is way ahead of them in terms of testing and having a working prototype ship. Basically SS1 is the favorite by quite a bit as of now.

    5. Re:Anybody else still in the running? by guile*fr · · Score: 3, Funny

      blast that!!! I want doomIII NOW!!!

    6. Re:Anybody else still in the running? by Drakin · · Score: 2, Informative

      Yes. The da Vinci project looks to be making an announcement on the date of their attempt (the launch site has already been stated) on the 16th.

    7. Re:Anybody else still in the running? by Mark_Uplanguage · · Score: 5, Insightful

      The real trick to the X prize, if you read the whole article, is that everyone has to get the FAA approval. So if there are any thoughts to other teams forgoing safety to try and beat the clock, think again. Indeed as a long time fan of Rutan, he's been the only real contender in my mind, due to his ability to solve any challenge presented because he thinks completely out of the box. That tail fin which flips up to control descent is a mark of true genius.

      --
      "The difference between stupidity and genius is that genius has its limits." -- Albert Einstein
    8. Re:Anybody else still in the running? by budgenator · · Score: 3, Interesting

      The FAA sub-orbital space flight license is required for U.S. contenders in the X Prize competition.
      The impression I got was that Americans teams needed FAA license, and probably foreign teams opperating in the US. I'd suppose that a Russian team opperating inside Russia would have their own licenses or permits from appropriate Russian agencies. I'm unsure if the X-prise rules specify where the opperation has to take place.

      --
      Apocalypse Cancelled, Sorry, No Ticket Refunds
    9. Re:Anybody else still in the running? by nyquility · · Score: 1

      I don't care if they (Armadillo) win, the news posts, their page and the pictures are an instant winner with me.

      Somewhere between extreme professionalism and tongue in cheek science.... add to that the disintegrating shed and the sight of geeks arc welding and you have a winner.

      I'll gladly wait for Doom 3 a little longer, this may be more entertaining in the long run.

    10. Re:Anybody else still in the running? by MrBlue+VT · · Score: 1

      I agree. Love the updates each week. I'm thinking about getting one of the T-shirts too, they're pretty cool.

    11. Re:Anybody else still in the running? by forkazoo · · Score: 1

      Goes to show you once again -- Rocket Science is Easy!. Rocket Engineering is Hard!. :)

    12. Re:Anybody else still in the running? by bluGill · · Score: 2, Insightful

      Fortunately US pilots have a tradition of experimental planes, and a regulation to place them under. Not everything needed to get into space, but you can work under those rules to do a lot of test flights before you have to get into untested regulatory waters.

      Mind you would be a fool to start with an experimental plane classification and give no hints that you intend to reach farther. Regulators do not like it when you surprise them. However you can work with them in well understood areas, while making it clear you intend to go farther.

      Still if you are in the US and interested you should write your congressmen. (all 3, house and senate) Nothing greases the wheels for those doing better than congress leaning on the regulators to make it easy.

    13. Re:Anybody else still in the running? by red+floyd · · Score: 1

      An alternative would be to have the pilot bail out and parachute down while the ship lands by itself,

      I believe this is what the Vostok cosmonauts did.

      --
      The only reason we have the rights we have is that people just like us died to gain those rights. -- Cheerio Boy
    14. Re:Anybody else still in the running? by MrBlue+VT · · Score: 1

      Yep, if it was good enough for Yuri Gagarin, it should be good enough for the X-Prize.

    15. Re:Anybody else still in the running? by Anonymous Coward · · Score: 0

      Just goes to show, rocket engine design is not simple!

      Yeah, dude, it's, like...umm, rocket science.

    16. Re:Anybody else still in the running? by Anonymous Coward · · Score: 0

      www.davinciproject.com they are a Canadian team which has had better success than the Rutan team. All hot engine tests have been successful, the ship has been built and models have undergone structural and finite element analysis tests. The engine uses Hydroxyl-Terminated Poly-Butadiene (HTPB) for fuel with nitrus oxide (N20) as an oxidizer (a very reliable, safe, common propellant). The flights are scheduled for this summer, but no exact date has been set although the announcement will be made from Long Beach California just prior to the Champ Car World Series car race April 18 (so we will know when they plan to launch in 9 days). A lot of the design was done using Ansys Finite Element Analysis software being fed back to Autocad (and the following structural changes re-tested with Ansys again to Autocad and so on). The craft has an aluminum block for mounting the rocket, with a fiberglass/composite construction. They also spent quite a bit of money on the project, but not as much as the Rutan team. Where Rutan is sponsored by Bill Gates, DaVinci is (partially) sponsored by Sun Microsystems of Canada.

    17. Re:Anybody else still in the running? by mcraig · · Score: 1

      Well as you obviously haven't noticed I thought I'd point out that us brits have a good contender in Steve Bennet who founded starchaser industries they've had lots of succesful launches and I would say they are a lot further along than Carmack though perhaps not quite as far as Rutan check it out www.starchaser.co.uk I believe they are scheduled to make an x-prize attempt this year.

    18. Re:Anybody else still in the running? by ColaMan · · Score: 1

      I point you to Legal Issues for Commercial Reusable Launch Vehicles

      If I recall correctly, I saw a NASA image of one of the shuttles with a small "Experimental" designation on it.

      I can imagine NASA talking to the FAA going "oh yah, we're working on a new er, aircraft, yeah, aircraft... we need a experimental type certificate for it... no,no, nothing fancy really, just a pretty standard glider design... in the post by tuesday afternoon? Ok, thanks!"

      --

      You are in a twisty maze of processor lines, all alike.
      There is a lot of hype here.
    19. Re:Anybody else still in the running? by ColaMan · · Score: 1

      I also like one of the sentences in the first few paragraphs :
      In the near future, reusable launch vehicles will routinely take off and land (intact) from just about anywhere there's a prepared surface

      The "(intact)" suggesting that perhaps it's not quite the case at the moment ;-)

      --

      You are in a twisty maze of processor lines, all alike.
      There is a lot of hype here.
    20. Re:Anybody else still in the running? by weglian · · Score: 1

      NASA does not need FAA approval to do anything, except getting airspace clearance. NASA and the military operate under their own rules.

    21. Re:Anybody else still in the running? by weglian · · Score: 1

      The X Prize requires teams to obey all applicable laws. An FAA launch license is required by American citizens/companies (where every they launch from) or foreign citizens/companies launching from the U.S. The Canadian, Russian, Romanian, etc. teams will not need an FAA license, although they will need whatever approval their country comes up with. Many of those companies look to the FAA to see how we do it, since the FAA is the only one to have any published rules for launching RLVs.

    22. Re:Anybody else still in the running? by LWATCDR · · Score: 1

      Maybe not. The FIA requires that the pilot land in the vehical for the flight to count as a record. The Russians like about the bail out for years because they where worried that the US would claim the "offical" title of first man in orbit. Of course the X-prize people may not follow that rule.

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    23. Re:Anybody else still in the running? by PeelBoy · · Score: 1

      I agree. I wish they would make some coffee mugs or something instead of just the shirt.

  3. I 100% agree with this story by Anonymous Coward · · Score: 3, Funny

    please moderate this comment up for that factor alone.

  4. 1/3 of the way there... by MBAFK · · Score: 5, Informative

    They have to get to 328,000 feet, seems like they are looking pretty good.

    1. Re:1/3 of the way there... by Neil+Blender · · Score: 1

      They have to get to 328,000 feet, seems like they are looking pretty good.

      If I understand the X-Prize correctly, they have to take 3 people to that altitude. Just getting there is not enough. I might be wrong about actually taking people, but if they at least have to account for weight and life support, just attaining the altitude would not win it. An attaining it with an extra 500-1000 pounds of cargo might take as much work as getting there in the first place.

    2. Re:1/3 of the way there... by cmeans · · Score: 1
      Are the X-Prize rules specific enough about the resulting health of the 3 people upon returning to the ground?

    3. Re:1/3 of the way there... by Neil+Blender · · Score: 2, Insightful

      Are the X-Prize rules specific enough about the resulting health of the 3 people upon returning to the ground?

      By 'safely return to earth', I would assume they mean more or less in excellent health. Another thing to note is that the same craft has to repeat the journey within two weeks. I would say getting the ship to 100K feet is closer to 1/10 of the way there than to 1/3 of the way. But then again, what do I know?

    4. Re:1/3 of the way there... by JesseL · · Score: 2, Interesting

      According to the rules they only have to have one person actually go up. They have to have accomodation for 3 passengers, but they can substitute an equivalent mass of inert payload instead. Since the ship has to fly twice in two weeks there is a strong incentive for it to make at least the first landing intact.

      --
      "Prefiero morir de pie que vivir siempre arrodillado!"
  5. Um by Neil+Blender · · Score: 2, Insightful

    "Scaled Composites has its eyes on snagging the X Prize, a high-stakes international race to fly a reusable private vehicle to the edge of space and return safely to Earth."

    There is no way in hell anyone is going to accomplish this feat for under $10 Million. What is this going to buy them? Bragging rights? Certainly not a spot next to Lockhead or Boeing.

    1. Re:Um by Anonymous Coward · · Score: 2

      You're a dumbass. It's not the money, its the goal.

    2. Re:Um by lostchicken · · Score: 5, Informative

      Scaled has a huge reputation in the industry. They're sort of the outsource Skunk Works. Companies like Boeing and Lockheed go to Scaled when they need something bizarre built and tested. Scaled isn't ever going to have a spot next to Boeing and Lockheed because Boeing and Lockheed are their customers.

      --
      -twb
    3. Re:Um by pokeyburro · · Score: 5, Insightful

      Pretty much bragging rights, yes.

      Or you could look at it this way: sub-orbital flight can potentially yield returns far beyond the investment. And I don't mean just the ability to fly at sub-orbital altitudes; getting this far proves you've got the brains and cojones to achieve this feat, which attracts other investors, which can fund bigger projects.

      But if you can't bear the investment, the X-Prize may soften that blow to the point that a company may give it a try. Think of it as a carrot that will feed you long enough to get to the BIG carrot farther on.

      --
      Lately democracy seems to be based on the skybox, the Happy Meal box, the X-box, and the idiot box.
    4. Re:Um by e9th · · Score: 1

      Maybe SC is betting that Lockheed & Boeing are too tied into meeting NASA's requirements to make commercially successful vehicles

    5. Re:Um by moltar77 · · Score: 1

      ...until they successfully go sub-orbital and people are willing to pay a few million to go up. Then I would think Boeing and Lockheed might be interested in some R&D, or maybe even try to buy Scaled. If Scaled starts to turn up some profit in space tourism, I'm sure that will turn some heads. (here's hoping!)

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

      Do you think Lindberg made money on his flight when he won the prize? Nope. It's about prestige and fame. And those are huge. Even if you boil it down to pure money it's still a win because X-Prize bragging rights go a long way toward convincing investors you are serious, you know your business, and you're a leader in it. No small things those.

  6. A Little Questionable Article? by slakr · · Score: 3, Insightful

    This is a really interesting development, and best of luck to these guys. But this quote from the article: "The engine burned for 40 seconds, zipping to Mach 2, or two times the speed of sound, according to a source that witnessed the test flight high above Mojave, California skies." is a little wierd. An unnamed source, who is just credited as a "witness" doesn't sound like the right person to make these sorts of claims.

    1. Re:A Little Questionable Article? by SpyPlane · · Score: 1

      I found that wierd as well. I mean, that'd have to be a pretty hefty radar gun to pick up Mach 2!

      --
      "We need a fourth law of Robotics: Stop Fingering My Wife"
    2. Re:A Little Questionable Article? by mrright · · Score: 1

      There is no official information on the scaled site yet. But there are many people in mojave who are very interested in space, and launching a spacecraft is not exactly something you can hide that easily.

      So probably there was a guy with a telescope and a stopwatch watching this. From the data it is quite easy to estimate altitude and velocity. We will get much better and more accurate data from scaled soon.

      --
      Private property is the central institution of a free society (David Friedman)
    3. Re:A Little Questionable Article? by SB9876 · · Score: 2, Informative

      According to the article, *COUGH COUGH RTFA COUGH*, Scaled has been keeping largely mum so far but has admitted that the flight did occur and that post flight handling analysis is going on. Expect a website update in a day or two.

    4. Re:A Little Questionable Article? by kidgenius · · Score: 1

      You must not have ever taken trig in high school. To estimate heights and velocity, you need to know how far away you are from it. You also need to know one of the vectors that it is traveling along. Just b/c you can point a telescope at it, and bust out a stopwatch, won't tell you a darn thing.

    5. Re:A Little Questionable Article? by Anonymous Coward · · Score: 1, Insightful

      You know how big it is.

      You know your telescope.

      You know it's apparent size
      in your telescope.

      Therefore, you know the distance
      to the object!

      You know which end of the
      thing is the front.

      You know that it flies forward.

      Therefore, you know which
      direction it is moving in!

      Amazing, huh?

      Simple high school geometry is all
      that's involved. And a wee bit of
      logic. And knowing that rockets
      fly in the direction which is
      opposite the engine exhaust.

      You must not have ever taken
      high school geometry.

    6. Re:A Little Questionable Article? by kidgenius · · Score: 1

      So tell me this. If it is moving up, and towards you, and it's size does not change at all, then how are you going to time that and know how fast it is going? Yes, this is possible. Is it possible to determine the speed? yes. But NOT in every case, and it is at best a guess. I'm not denying how fast it went, but the way in which you are trying to determine it's speed is extremely crude.

    7. Re:A Little Questionable Article? by cosmo7 · · Score: 1

      So tell me this. If it is moving up, and towards you, and it's size does not change at all, then how are you going to time that and know how fast it is going?

      You could count sonic booms.

    8. Re:A Little Questionable Article? by kidgenius · · Score: 1

      I believe their is only one boom when the sound barrier is broken. Anything above that creates only the first boom. You don't get another for going 2, 3, 5,....etc times the speed of sound.

  7. Slashdot in space... by RedPhoenix · · Score: 3, Funny
    Slashdot mentioned yesterday that it received a license from the FAA, the first license for a suborbital rocket.

    Woohoo.. interplanetary takeover. If 'News limited' can have their own satellites, so can we.

    Slashdot, your official lunar news source.

    1. Re:Slashdot in space... by red+floyd · · Score: 1

      Well, Slashdot did have the "Geeks in Space" feature....

      --
      The only reason we have the rights we have is that people just like us died to gain those rights. -- Cheerio Boy
  8. Curses, foiled again! by SB9876 · · Score: 5, Interesting

    Drat, someone beat me on the article submission. At least this time, the editors will finally have a decent reason to reject my submission, though.

    Unless something goes seriously wrong with Scaled's program, it looks they've got the thing pretty much sewn up. The only serious competitors to Scaled right now are Carmack's Armadillo and those craaazy Canucks on the Da Vinci project. Given that this is almost exactly 1/3 of the way to the X Prize and that they already have broken the red tape barrier, I have trouble seeing anyone catching up to Rutan and crew at this point.

    1. Re:Curses, foiled again! by JT27278 · · Score: 1

      The first rocekt powered flight of Spaceship one ended with some damage to the craft from a collapsed landing gear. This set them back months. While it's clear that they are a front runner, it's way too early to call it over. With this type of endevor, any time before it's done is way too early.

    2. Re:Curses, foiled again! by SB9876 · · Score: 3, Interesting

      True, it's basically a test of designs at this point. Rutan and company could probably go for the X Prize tomorrow is they felt like it but at great risk to the pilots. Conversely, they might find out that at mach 3, SpaceShipOne has unfixable stability problems. Basically, that's back to the drawing board and all chances for a win are gone then.

      However, sing as how no other team has even tested a full scale demonstrator yet, Rutan is firmly in the lead. Armadillo hasn't even figured out their entire landing proceedure yet. It's hard to figure out where Da Vinci is at since they're site is somewhat short on details. It took a while to even figure out that they had physical components ready. Unless something goes wrong, it's hard to see anyone passing Scaled at this point.

  9. wait by weekendwarrior1980 · · Score: 1

    didn't the first one clock mach 7 (7 times the speed of sound? Or am I talking about the some other vehicle?

    1. Re:wait by goretexguy · · Score: 3, Informative

      I believe you are thinking of the X-43A Scramjet test vehicle.

    2. Re:wait by fredrik70 · · Score: 1

      yup, another vehicle. You're thinking of NASA's scramjet plane which did a nippy mach 7.

      --
      if (!signature) { throw std::runtime_error("No sig!"); }
    3. Re:wait by Anonymous Coward · · Score: 0

      You're thinking of NASA's scramjet project that was recently tested.

    4. Re:wait by rusty0101 · · Score: 1

      Sounds like the scramjet, not the x-prise.

      Though I could be wrong.

      -Rusty

      --
      You never know...
    5. Re:wait by weekendwarrior1980 · · Score: 1

      Sorry, yes that's the one.

  10. I hope they get there, but what next? by skywolf · · Score: 4, Insightful
    Although this team have spent more than the prize money, it seems incredible that they have designed, built and flight tested a prototype for less than the cost of any off-the-shelf space-launch I have ever heard of.

    Is this 'cos they're good, or is it the case that the two tasks (suborbital flight, orbital flight) really don't bear any comparison? Five years from now, will Slashdot be covering the Y prize (orbital flight) or ultimately even the Z-prize (presumably an amateur moonshot)

    1. Re:I hope they get there, but what next? by Xolotl · · Score: 1

      Suborbital flight is much easier to achieve, which is why the X-Prize specified it. The velocities required are much lower, which means less fuel needs to be carried, the aerodynamics are simpler and the return journey doesn't require nearly as much heat shielding to protect the passengers while the ship burns off the excess velocity.

    2. Re:I hope they get there, but what next? by mrright · · Score: 4, Interesting

      There is a very logical upgrade path from a suborbital to an orbital vehicle.

      A manned suborbital vehicle going to 100km altitude needs a reaction control system to orient itself in a vacuum. It needs to be pressurized. And it needs a (small) heat shield.

      So it really is a space craft that just does not have enough delta-v to make orbit.

      By increasing the available delta-v incrementally you can work out the bugs much easier than if you had to do it all in one big step like they did with the shuttle.

      A suborbital craft is also very interesting as a reusable first stage for a microsattelite launch vehicle. For example with the payload of the spaceship one and an expendable upper stage it should be possible to get about 10kg into low earth orbit. This would be very interesting for universities and radio amateurs that can not affor d a large launch vehicle.

      The DOD has also shown some interest in microsattelites. This is a nice way to make some money while developing a real reusable orbital space craft.

      --
      Private property is the central institution of a free society (David Friedman)
    3. Re:I hope they get there, but what next? by fredrik70 · · Score: 1

      it's not really comparable suborbit flight is all going straight up and then you just fall down, no big problems with heat shielding, etc, etc (even if they apparently got some shielding). To go orbital you not only doesn't need to get up high, but also very, very fast sideways (around mach 25 IIRC) so you go into orbit. the speed and the stress on the craft are far higher than a suborbital flight.
      but hey, it's a very good step in the right direction!

      --
      if (!signature) { throw std::runtime_error("No sig!"); }
    4. Re:I hope they get there, but what next? by DerekLyons · · Score: 1
      Although this team have spent more than the prize money, it seems incredible that they have designed, built and flight tested a prototype for less than the cost of any off-the-shelf space-launch I have ever heard of.
      That's not surprising when you consider that SpaceShip One isn't a space launch system. If the Shuttle is an 18 wheeler, SS1 is somewhere around a Segway. Impressive as hell in it's own right, but decidely at the precise bottom of the scale.
      Is this 'cos they're good, or is it the case that the two tasks (suborbital flight, orbital flight) really don't bear any comparison?
      It's a difference of degree as well as of kind. An orbital ship has to re-enter, SS1 doesnt. An orbital ship requires a far higher velocity (read: a much more powerful engine) than a sub orbital ship. An orbital ship requires much more precise navigation and control than an suborbital ship. Etc. Etc.

      There are evolutionary paths from the X-Prize vehicles to orbital vehicles, but the paths are steep, slippery, and strewn with landmines.

    5. Re:I hope they get there, but what next? by cmowire · · Score: 1

      Better analogy: The shuttle is an 18 wheeler built by Ferrari. The SS1 is a custom touring motorcycle made out of fancy materials.

      Neither one's going to be practical for dropping off a cake at grandma's, but they are both neat toys. It's just that the touring motorcycle is a lot cheaper to take out for a joyride.

    6. Re:I hope they get there, but what next? by Keebler71 · · Score: 2, Informative
      I have to respectfully disagree. Your statement:

      So it really is a space craft that just does not have enough delta-v to make orbit.

      ...Has to be the understatement of the year. Yes, sub-orbital spaceflight addresses many of the technical challenges of orbital spaceflight, however it doesn't address the only hard one. Reaction control and the aerodynamics are really rather straight forward. This project does not address the thermal control issues of orbital flight, as the heat loads are no where near what would be encountered during re-entry from orbital velocity. Moreover, they are using a solid propellant rocket motor. They would have to switch to liquid engine to go suborbital, and that implies a heck of a lot more mass (tankage, cryo, pumps, much more complex engine, etc...) I don't mean to belittle the monumental achievements of Scaled Composites' with this project, however IMHO the real advances they have made are programatic... being able to accomplish this on a shoe-string budget, with few leaks, not to mention cutting through the beurocratic red tape necessary to DEFINE THE PROCESS of granting a civilian permit for space flight.

      BTW, I just ran the calculations, and agree with you on the microsat point. Figuring a 10kg payload, and about 20kg for engine and tankage (pretty optimistic) requires about 160 kg of propellant to get to Vcirc at 100 km. I think a 200 kg 'payload stage' would be quite reasonable.

      --
      "It takes considerable knowledge just to realize the extent of your own ignorance." - Thomas Sowell
    7. Re:I hope they get there, but what next? by gd2shoe · · Score: 1
      Is this 'cos they're good, or is it the case that the two tasks (suborbital flight, orbital flight) really don't bear any comparison? Five years from now, will Slashdot be covering the Y prize (orbital flight) or ultimately even the Z-prize (presumably an amateur moonshot)
      Is there anything "amateur" about a moonshot?
      (but yes, it would be awesome)
      --
      I won't join Slashcott. OTOH, If Beta goes live, I just won't be back until it's fixed. Sorry Dice.
    8. Re:I hope they get there, but what next? by Anonymous Coward · · Score: 0

      Perhaps, but I think you might be underestimating (by quite a lot) the difference between orbit, and merely achieving the altitude. You get get away with a lot in the later case which you simply couldn't in the former, so there are fundamental and unavoidable differences in many of the technologies (engines, heat shielding, and more).

    9. Re:I hope they get there, but what next? by Thagg · · Score: 1

      SpaceX is probably the most advanced of the new low-cost launchers. Interestingly, the man behind SpaceX is the founder of PayPal, who got out while the getting was good.

      SpaceX is dedicated to creating a pair of low-cost extremely simple launchers. They've created their own engines based on a very simple design, and their own turbopump. The engines are LOX/RP1 (basically kerosene) engines, which are extremely well known, inexpensive and available.

      There was a nice writeup on SpaceX in Aviation Week two weeks ago. They have been testing their engines and plan to launch their first orbital mission within a year or so.

      It's always a longshot betting on any of these small rocket companies actually launching a rocket successfully. It's even harder to make money doing it. Lockheed built a small, solid fueled rocket of about the same class as the smaller of the SpaceX rockets about 10 years ago. The first one blew up, but the second and third ones succeeded. Unfortunately, the market for small launchers just didn't exist.

      SpaceX has a government payload signed up for their first rocket. If it is successful, and they can really launch rockets for the rediculously small price that they quote, then perhaps they will be successful. More power to them!

      thad

      --
      I love Mondays. On a Monday, anything is possible.
    10. Re:I hope they get there, but what next? by pfdietz · · Score: 1

      SpaceX is perhaps the most promising space launch startup ever. Compared to some of their predecessors, they just ooze business and engineering sense.

      They've worked hard to keep things simple and cheap, and that means their breakeven launch rate is not excessive. I give them a good chance of succeeding, and eventually beating even the Russians and Chinese on launch costs.

  11. Absolutely awesome! by csoto · · Score: 0, Redundant

    Way to go, guys! Burt and the rest of the team embody what this country can produce, when we put our minds to it.

    --
    There exists no way of exchanging information without making judgments. --Bene Gesserit Axiom
  12. Okay, you guys... by Faust7 · · Score: 4, Insightful

    Enough with the "I'll believe it when I see them fly at xxxx feet" or "Rutan's an aviator, not an aerospace engineer" or "Only 15 seconds? Bah!' comments. Just suppress the generalizations and childishness for a little while... and watch Burt Rutan, Scaled Composites, and SpaceShipOne. Watch them as if you were waiting for the curtain to be raised for an opening act, because that's exactly what this is. This is rocket plane history unfolding.

    Rutan and his company aren't doing this for the prize. They're doing it to make a point about certain types of aviation and engineering that have been long derided by NASA and other naysayers as being unrealistic, impossible, et cetera.

    Look at Rutan's track record, which includes the development of composites--an absolute breakthrough that the FAA is just now getting around to accepting--and the Long-EZ craft. Look at everything the guy has done, and the company he has, and tell me he doesn't have one hell of a chance at making this thing work.

    1. Re:Okay, you guys... by Rorschach1 · · Score: 1

      I'm not doubting that they'll pull it off. But can someone remind me how this gets us closer to affordable access to space? After all, isn't this pretty much the same technology as the X-15 that first flew in 1959? Just scaled up a bit to hold three passengers.

      Reaching 100km at no particular speed is a loooong way from attaining orbit.

      How about someone funding a space elevator competition? Be the first to demonstrate a 100km cable of a certain strength and win $XX million.

    2. Re:Okay, you guys... by SB9876 · · Score: 2, Insightful

      True, 100 km is old stuff for NASA but it's still quite useful. There's the whole space tourism for 1/10th the cost angle which does have appeal. The Russians are building a space plane (another X Prize contestant, BTW) for that very purpose. I don't know what the maximum downrange for SpaceShipOne is but it has great potential for moving small numbers of people and freight at high speeds. Need to send someone or something from LA to New York in 1.5 hours for $100K a pop? There's a solid, profitable business right there.

    3. Re:Okay, you guys... by BCW2 · · Score: 1

      Ruttans record is sectacular. The nay sayers here forget that all the supposed experts thought he couldn't fly aroubd the world non-stop and without refueling. He succeeded, with a good team that won't believe you can't do it.

      Remember Alan Shepards Mercury flight was about the same as this one.

      --
      Professional Politicians are not the solution, they ARE the problem.
    4. Re:Okay, you guys... by ckaminski · · Score: 2, Insightful

      I wish you people would shut up about the damn space elevator already. Please tell me how you're going to build a 20,000km space tether out of unobtanium WITHOUT FUCKING CHEAP ACCESS TO SPACE?!

      Thank you. ;-)

    5. Re:Okay, you guys... by MindStalker · · Score: 1

      Actually there are several viable plans that involve dropping a very thin single line, and then using that to install new lines through small robot climbers. Its more the materials that are the problem and not the access to space.

    6. Re:Okay, you guys... by bluGill · · Score: 2, Insightful

      Why do I need cheap access to space? If you gave me a cable that worked for a space elevator, but the only material that would work resulted in a cable that required something with twice the power of the Saturn V, I'd jump at it despite having to hire rocket scientists to design and build the thing. (Assume that the plan of dropping a small cable to pull the big one up turns out not to work for whatever reason).

      Once I get a cable in place, all launches are cheap. I can undercut anyone with a conventional rocket, and still make money, despite my high initial costs. I'll just spread those costs out over 50 years.

      Mind I will be very careful to make sure that if you want to compete with me, you have to build your own rocket because there is no way I could compete with you taking your cable up on my elevator.

      Just get me a cable. The rest is easy. (Easy as in we already have the technical know-how to do it. Not as in any fool can do it)

    7. Re:Okay, you guys... by Anonymous Coward · · Score: 0

      You dumbass this is not the pilot Dick Rutan who flew the voyager plane but his brother the super genius aerospace engineer who designed the damned plane.

  13. Poway California? by Audacious · · Score: 0, Flamebait

    When I first read the article I mentally converted Poway to PovRay and found myself thinking "What the heck are those guys doing now!? And where is this city located?"

    (Working on too many graphic projects!) :-)

    --
    Someone put a black hole in my pocket and now I'm broke. :-)
    1. Re:Poway California? by Anonymous Coward · · Score: 0

      The fact that this has been modded as flamebait makes me question whether some of these moderators should even be given access oxygen nevermind mod points.

    2. Re:Poway California? by Audacious · · Score: 1

      Yes, well - some people just don't like Audacious. *Shrug* Takes all kinds.

      I just finished dealing with someone who said I was a hate monger. I've never thought of myself as a hate monger - but who knows? Maybe I should look in the mirror more often? I thought once a day, when I shaved, was enough but ya just never know.

      Ah well, since joking around must now be flamebait I'm expecting this to draw quite a bit of flack. The funny thing is - the e-mail I received said my post was moderated to funny (+1). Which is what I thought it was - funny I mean. In the normal sense of the word. So imagine my surprise when I check it and it is no longer listed as funny but as flamebait. My thoughts are that Slashdot's e-mailing system must be mucked up a bit. Otherwise, why would it tell me it was moderated as funny?

      You know - I think there's a joke in there somewhere but I just can't quite see it. :-) Besides - why would I want to entice whomever it was that marked my last message as flamebait to do so again? *nudge-nudge-wink-wink*

      Later!

      --
      Someone put a black hole in my pocket and now I'm broke. :-)
  14. Bet this one only went 1/3 of the way because... by Ungrounded+Lightning · · Score: 5, Informative

    They have to get to 328,000 feet, seems like they are looking pretty good.

    I bet this one only went a third of the way because that's about as far up as they can go while still controlling the craft's attitude with control surfaces.

    Power for the rest of the altitude should be no problem, since their engine seems to be working just fine. But they'll need also need their attitude control and reentry heat shielding working to go extra-atmospheric - where they can't just glide down the whole way.

    So first some tests where the limits of the aircraft mode are demonstrated and debugged, followed by tests where the additonal functions are also used.

    One step at a time wins the race. B-)

    --
    Bantam Dominique roosters crow a four-note song. Once you've heard it as "Happy BIRTHday" you can't NOT hear it that way
  15. how long now? by bwy · · Score: 4, Insightful

    Something is getting ready to happen real soon. Days after an FAA launch permit, a second powered test all the way to over 100K feet. The burning question is, how many more test launches before they go the distance? Surely, the history of test piloting experimental aircraft can yield a little input? What are the things left to verify and confirm before going the full 300K+ feet? I'm guessing not a whole lot if performance was good on the spacecraft and the engine burn went well. Is the cabin of SpaceShipOne fully pressurized, or do they depend exclusively on the pilot wearing a pressure suit?

    This is very exciting to watch. I wish these guys all the luck and safety in the world.

    1. Re:how long now? by SB9876 · · Score: 3, Insightful

      As another poster pointed out, 100K feet is about the maximum altitude where flaps still give aerodynamic control. Above that, they're going to have to depend upon the attitude control system. My guess is that the next flight will go to slightly over 100K feet and test those systems out.

      After that, there will probably be a series of flights progressively going higher and faster to test out the high speed handling of the craft. Rutan is known for being very methodical about testing new designs.

      After that, they'll probably start doing a few flights to 300K+ feet to make sure that everything works correctly. After that, they'll load on the two extra passengers and prepare to make the two flights in one week necessary to get the prize. (just hitting the altitude doesn't get you the prize) Knowing Rutan, he'll probably throw in a couple more flights in that first week just to show off.

    2. Re:how long now? by SB9876 · · Score: 1

      Oh yeah, almost forgot, the cabin is pressurized. So no pressure suits are required.

    3. Re:how long now? by Thagg · · Score: 4, Interesting

      Actually, SpaceShip One is a shirtsleeve environment. The pilots don't wear pressure suits. I believe all the windows are double-paned, each of which would hold pressure by themselves. The environmental controls on the ship are pretty simple, there are scrubbers to remove CO2 and water vapor, and they have an oxygen bottle to bleed some oxygen into the cabin.

      Pressure suits are a real pain, and they restrict the pilot's vision, hearing, and motion so much that it's really good if you can avoid them. SpaceShip One is no walk in the park to fly, the pilot really needs all the help he can get to fly it.

      Godspeed, Burt.

      thad

      --
      I love Mondays. On a Monday, anything is possible.
    4. Re:how long now? by beauzo · · Score: 1

      ...and no heater. IIRC, aside from the blue jump-suits, the avionics under the seat are suppose to help keep the pilot warm during the short ride. It's going to get cold real fast.

      -B

    5. Re:how long now? by Teancum · · Score: 1

      Keep in mind that the X-Prize requirements are that you only have to carry "ballast" equivalent of two extra passengers... not the passengers themselves. Still, it would be a nice "plus" if they could do a full commercial-capable flight of three people, two passengers + pilot.

      I would have to agree that Rutan does follow a very methodical and incremental testing regime... indeed this is exactly the benefit of going the route that he has been taking. Carmack has been struggling with engine design, but it appears as though they are going to be ready to launch a test vehicle real soon as well. It is going to be an exciting year this year in terms of private space programs.

      I'm expecting a stealth group to "suddenly" appear on the scene as well if these groups get real close to reaching the goal.

    6. Re:how long now? by Suidae · · Score: 1

      Maybe they can sell the three extra seats on the two flights to the highest bidder. I dunno what it costs to launch that thing, but I'll bet they could easily cover the costs with a few rich passengers.

      If I were a millionare I'd sure drop a few hundred thousand to be on that flight.

  16. Can't wait by nizo · · Score: 0, Offtopic

    Hopefully someone will be offering affordable "zero-g" sex flights before all of my parts (and partner's parts) stop working.

    1. Re:Can't wait by homer_ca · · Score: 1, Informative

      If you can finish in 25 seconds, you can always rent out the Vomit Comet, an airliner built for weightlessness training that flies alternating climbs and dives.

    2. Re:Can't wait by nizo · · Score: 2, Interesting

      Bah the prudes can rate me into oblivion, but I'm telling ya the average joe going into space is what will change everything.

  17. No mention of the feat at the web site?! by fygment · · Score: 1

    Debrief or not, one would have expected some mention on the Scaled Composites homepage that the test had taken place. The last announcement came out the same day. No doubt they got the licence but maybe the rest is just a hoax by someone to shake up the competition.

    --
    "Consensus" in science is _always_ a political construct.
    1. Re:No mention of the feat at the web site?! by mrright · · Score: 2, Informative

      There are some images on RLV News . And there is also a story on space.com. Everybody in mojave must have seen and heard this.

      --
      Private property is the central institution of a free society (David Friedman)
  18. R.U. Serious? by poptones · · Score: 1
    Rutan, a guy who has been a pioneer for as ong as I can remember (and I can remember quite a long time back now). Then you got a guy who helped startup the largest software company in the history of the world. They're well on the way to launching a space vehicle that not only represents a huge step up for private space ventures, but does so in a craft that looks and operates substantially unlike anything the largest government in space has ever made operable.

    Ten Million is just the beginning. those "bragging rights" are worth Billions nowdays - assuming everything goes well and the prize gets awarded this year, the sportswear licensing alone will probably be worth a Billion dollars next year...

  19. Lindbergh wasn't trying to be a transatlantic taxi by TigerNut · · Score: 5, Insightful

    A lot of the aviation 'firsts' had nothing to do with commercial interests on the part of the participants. They just wanted to DO it, because they thought they could. On that note, Carmack's efforts are closer in spirit to those of the Wrights, Lindbergh, et al, than Rutan (since Burt and Dick are well known in the experimental aircraft business) but it looks like that within a couple of years there will be a number of private organizations capable of doing Low-Earth-Orbit vehicle insertion. What that is going to do for society? I dunno. The suborbital capability alone basically gives Rutan etc. the ability to deliver people or cargo partway around the world in half an hour. That would be one hell of a courier service.

    --

    Less is more.

  20. X.43 by sofakingon · · Score: 0

    That was the NASA X.43 ScramJet. Something totally different.

    This competition just goes to prove that with a couple million in capital you can do anything!
    Once again, mod +1 for capitalism!

  21. What's that I smell... by Anonymous Coward · · Score: 0

    Given that Rutan has a PhD in aerospace engineering + a decade of doing stuff with planes other people couldn't.

    I think it might be the bleached bones of a billy goat. Maybe the grass is green enough where I'm at.

  22. sub-orbital != orbital by close_wait · · Score: 5, Informative
    I'd just like to remind everyone that putting an object into a low-earth orbit requires about 25 times the energy of just raising it vertically to that height and letting it fall back to earth. That's why the commercial rockets that put satellites into orbit will continue to be big expensive beasts, X-prize or no X-Prize.

    1. Re:sub-orbital != orbital by mrright · · Score: 4, Interesting

      The X-Price vehicles itself will not compete with orbital launch vehicles. But they are a good way to learn how to build a real reusable space vehicle instead of just converted ICBMs like we have been doing for the last 50 years.

      And there is a commercial rocket in production that is small compared to its competitors and has a reusable first stage. It will be used to launch satellites for the DOD, among others.

      There are already plans to scale this vehicle up to a much larger size. And the first stage will still be reusable.

      --
      Private property is the central institution of a free society (David Friedman)
    2. Re:sub-orbital != orbital by SB9876 · · Score: 4, Informative

      I'd seen figures closer to 12 times as much energy but the difference is largely academic. Either way, geting to LEO is expensive. However, I'd expect to see an X2 prize being offered to get to LEO after this. Remember that a lot of the high costs of LEO launchers are artificial. The fuel is usually about 2% of the total launch cost. The rest is all those launch technicians and the cost of all those non-reusable rocket parts.

      Boeing has managed to capitalize on reducing the launch technician side of things along with using cheaper Ukranian parts to get launch costs down to about $5000/kg to LEO with Sea Launch. That's half the cost of their own Delta launchers. The DC-X several years ago had real promise of beinga practical SSTO, massively cutting launch costs. Unfortunately, NASA axed it, seeing it as a competitor. The hope is that the rise of private companies that aren't tied to NASA politics will be able to eventually replicate the work done on the DC-X and actually get some real progress on cheap orbital launches rather than the technology of the month approach NASA's been dumping money down the last 20 years.

    3. Re:sub-orbital != orbital by Anonymous Coward · · Score: 0

      At first I didn't believe you, but since I am a physicist I went ahead and worked it out.

      You are probably right, although the exact figure depends on the height you are going to. The higher you go, the energy for orbital flight becomes a smaller multiple of the energy for a straight up shot. The virial theorem gives the limit at 1.5x the energy for a straight up shot.

      Ignoring air friction, I did a simple calculation and found that for 300,000 feet the energy for orbital flight is 35x greater than the energy required for going straight up. If I took air friction into account it would reduce this ratio. So the 25x greater figure seems reasonable.

    4. Re:sub-orbital != orbital by AeroIllini · · Score: 2, Informative

      However, I'd expect to see an X2 prize being offered to get to LEO after this.

      Actually, the next project Peter Diamandis is working on related to this is called the X-Prize Cup, i.e., the Rocket Races. Every year there will be an airshow (spaceshow?) in a yet-to-be-determined city where people who have built X-Prize-style suborbital craft can compete. Prizes will likely be in several categories, like Most Altitude, Longest Downrange Distance, Most Velocity, Largest Payload to 100km, etc. And since the competition will happen every year, this will give the crafts' designers and builders a chance to improve their designs.

      The X-Prize was designed to foster a space tourism industry. The X-Prize Cup is designed to create innovation and growth in the private space arena. It will eventually lead to orbital flights.

      The hope is that the rise of private companies that aren't tied to NASA politics will be able to eventually replicate the work done on the DC-X and actually get some real progress on cheap orbital launches rather than the technology of the month approach NASA's been dumping money down the last 20 years.

      Don't get me wrong, I am very excited about the things NASA has accomplished and can still accomplish. They are doing great things. But the problem with their approach is that every new vehicle is a revolution, not an evolution. The best way to develop new technologies has always been to take a design that already works and tweak it slightly for your own purposes, making it a little better in the process. Unfortunately, NASA can't do that because their funding has the lifespan of a politician's term in office.

      --
      For security, the MD5 hash of this message and sig is 09f911029d74e35bd84156c5635688c0.
    5. Re:sub-orbital != orbital by Anonymous Coward · · Score: 0

      I'd seen figures closer to 12 times as much energy but the difference is largely academic.

      It depends on the height. If you can define what radius you call LEO, it's easy to calculate. If you want to do this yourself, try it first without the Earth rotating. Adding in rotation of the earth and orbital inclination is computationally easy, but you may need to do a little head-scratching if you haven't thought through it before.

  23. Re:Bet this one only went 1/3 of the way because.. by PhantomHarlock · · Score: 2, Informative

    They have reaction control and heat shielding on the craft as of present. The heat shielding was recently added.

  24. Re:Lindbergh wasn't trying to be a transatlantic t by PhantomHarlock · · Score: 3, Informative
    > Carmack's efforts are closer in spirit to those of the Wrights, Lindbergh, et al, than Rutan (since Burt and Dick are well known in the experimental aircraft business)

    Except that the wrights spent most of the rest of their career suing other people over patents. Everyone else continued innovating despite them. But I am sure you are referring to the good part where they were building aircraft out of their bicycle shop. :)

  25. One-third of the way there by Anonymous Coward · · Score: 0

    In terms of height, at least. That's 32 km. Now comes the hard part.

  26. Re:Lindbergh wasn't trying to be a transatlantic t by corngrower · · Score: 4, Informative

    You realize that the first nonstop transatlantic flight was made by a couple of Brits, not Lindbergh. He was first to solo. I think the flight by the British really was more important historically, but you won't find it in any American textbooks.

  27. No rocket engine design is not hard by codepunk · · Score: 1, Informative

    No it is easy to build rocket engines, dealing with all of the retarded govt regulations is hard.

    I have what I think is a innovative design for a new engine but I cannot try it. It requires aluminum powder and you have to sell your soul to the govt and jump through a thousand hoops just to get something simple like aluminum powder. If I even attempted to build a test engine the damn feds would probably be all over me accusing me of attempted terrorism.

    --


    Got Code?
    1. Re:No rocket engine design is not hard by bluGill · · Score: 2, Funny

      If you need powered aluminum, I can get you plenty. All my neighbors drink pop from cans (I'm the strange one on the block who can't stand soda) and most throw them away. Cans are about as pure aluminum as you can get, so I'll just powder them, and then sell to you.

      Okay, so I'll burn the paint off too, and if you like I will use electrolysis to get rid of the Al oxide.

    2. Re:No rocket engine design is not hard by qualico · · Score: 1

      How about fertilzer? Has lots of oxygen.

    3. Re:No rocket engine design is not hard by Anonymous Coward · · Score: 0

      Er...oooookaaaay. Hope you know what you're doing.... Powdered aluminium explodes readily, and "burning the paint off" will also burn the aluminium....

  28. IS This Design A Dead End? by reallocate · · Score: 4, Interesting

    My understanding is that the Rutan craft will accelerate to a few times the speed of sound and then coast to 60 kilometers.

    Remembering that achieving orbit is a matter of velocity, not altitude, is the Rutan design a dead end? I.e., could this design achieve orbit with the addition of a more powerful engine? (I know the easy answer is "Yes", but I'm asking if this particular design is capable of orbital flight.) If so, would the Rutan's rather unusual reentry approach work in a return from orbit?

    --
    -- Slashdot: When Public Access TV Says "No"
    1. Re:IS This Design A Dead End? by SB9876 · · Score: 2, Insightful

      Getting SpaceShipOne up to LEO just requires a larger carrier arcraft and more powerful, higher Isp boosters. (About 12 times bigger but at least that's something that can be attacked with standard aerospace engineering) The reentry is where the problem is at. 17,000 mph is a lot of speed to bleed off. The current SpaceShipOne design isn't capable of mounting the heat shielding necessary to survive those kinds of thermal loads.

    2. Re:IS This Design A Dead End? by mrright · · Score: 4, Insightful

      It will coast to 100km, which is the official edge of space. And the design is not a dead end. It does exactly what it is designed to do: fly to 100km.

      The overall concept which rutan is using is staging at high altitude and low speed with a more or less conventional aircraft as a first stage.

      This is most definitely not a dead end. There are existing launchers such as pegasus that do it that way, and there are also some very serious proposals for orbital two stage space transports with a large, rocket assisted transport aircraft as a first stage.

      Give rutan a price of 100 million $ and he will come up with a concept for an orbital two stage space transport. It will probably look completely different (no two rutan aircraft look alike), but I would bet that it will use subsonic staging at high altitude.

      --
      Private property is the central institution of a free society (David Friedman)
    3. Re:IS This Design A Dead End? by Anonymous Coward · · Score: 0
      I think that saying SpaceShipOne being a dead-end akin to saying Charle's Lindbergh's 'Spirit of St. Louis' was a dead end.

      The 'Spirit of St. Louis' did what it was designed to do, namely cross the Atlantic. It was never designed to provide passenger service, or deliver weapons onto targets. Subsequent aircraft were designed for those purposes. But the designs of those subsequent aircraft owe a great deal to creation and successful flight of the 'Spirit of St. Louis.'

      I think the same will be true of SpaceShipOne. While this design won't get you orbital, it will greatly influence how private industry will go about creating orbital vehicles.

      As Newton once said:

      "If I have seen further it is by standing on the shoulders of Giants."

      If it succeeds, Scaled Composite's SpaceShipOne will be one of the giants upon which the privitization of access to space stands.

    4. Re:IS This Design A Dead End? by Suidae · · Score: 1

      Perhaps this is a stupid question, but I don't know anything about orbital mechanics or reentry, so I'll ask anyway.

      Why does all the orbital speed have to be discarded so quickly? Could an orbiter reduce its altitude more slowly to reduce the amount of heat generated?

      Obviously it would take longer and require more fuel, but could it be done this way?

    5. Re:IS This Design A Dead End? by pfdietz · · Score: 1

      It's not a dead end for reaching orbit. You'd just have to redesign the engine, the propellant tanks, fuselage, wings, thermal control, and probably most of the rest of the vehicle. :)

    6. Re:IS This Design A Dead End? by HeyLaughingBoy · · Score: 1
      Why does all the orbital speed have to be discarded so quickly?

      I was wondering the same thing. Wouldn't it be possible to come back into thin atmosphere and decelerate slowly by essentially being a high altitude glider? At LEO speeds, you're still below escape velocity, so even if you skipped off the atmosphere a few times, you're still going to be coming back to Earth. It would take an airframe configuration that allowed controllable lift over a large envelope, but I don't see anything that makes it impossible.

      The issue I see is that you need to both maintain a low enough altitude where control surfaces work but which is high (Read: thin) enough that heating isn't excessive.
    7. Re:IS This Design A Dead End? by Bill+Barth · · Score: 1
      Here's the thing: The slowest you can go in space occurs at the _highest_ point in your orbit. You can't simultaneously be at the highest point in your orbit and significantly decelerating without serious retrorocket fire. Also, skipping off the atmosphere, at best, corresponds to making your orbit more elliptical (and less circular) which means that you are in the atmosphere at the lowest point in your orbit. Which means that you are in the fastest part of your orbit inside the atmosphere (bad). In fact, you may be going faster than in your previously circular orbit even though you've reduced your overall energy (potential + kenetic).

      The thermally optimal way to get out of orbit is to retro burn to an instant dead stop and then retro burn against gravity at a rate that doesn't heat you up :) Of course this requires more fuel than you can get to space!

      --
      Yes...I am a rocket scientist.
    8. Re:IS This Design A Dead End? by Suidae · · Score: 1

      Could you adjust the shape of the orbit (which I presume takes less energy than getting into a lower orbit) such that at the lowest altitude (and highest speed) you are passing through atmosphere and loosing velocity?

      It seems like you could choose the altitude (and therefore atmospheric density) so that you'd always be keeping the heat load down to a level that didn't require exotic materials or ablative sheilding.

      Each pass through the atmosphere would make the apogee a bit lower until you had discarded all that extra velocity and were continiously in the atmosphere.

  29. turns out that they can glide down the whole way by Anonymous Coward · · Score: 0

    Read the design documents on space.com and scaled.com and such.

    Because it doesn't reach orbital velocity, the shuttlecock system keeps the speeds down to a reasonable level and heat shielding is minimal.

  30. FedEx to the 32nd floor... by firewood · · Score: 1
    That would be one hell of a courier service.

    I can just see it now. Boss says to newbie secretary "send this letter to Singapore by the fastest means possible". A weeks later, the accounting dept. inquires why the company received a shipping bill from $35M from UnitedScaledCompositesExpress.

    1. Re:FedEx to the 32nd floor... by kalidasa · · Score: 1

      ScaledComposites: when you absolutely, positively have to get there in an hour.

    2. Re:FedEx to the 32nd floor... by Drooling+Iguana · · Score: 2, Funny

      Serves them right for not buying a fax machine like the rest of the world.

      --
      ... I'm addicted to placebos
  31. distance? by orn · · Score: 1

    I'd like to see what this thing could do for distance travel. I know that it's really only designed to go up and down in a very narrow parabola, but being at 300K feet means there is very little atmosphere. You should be able to really book with relatively little fuel cost.

    How long until the first business jet/rocket appears?

    I could just see Paul Allen going to shareholder meetings in one of these (or the business jet equivalent).

    --
    1. 2.
  32. Looks friendly to me by Anonymous Coward · · Score: 0

    I like the idea it seems pretty environmentally friendly, not requiring a first stage launch. Plus I would get to board at a nearby airport. Instead of having to travel to a spaceport first.

  33. Re:turns out that they can glide down the whole wa by Ungrounded+Lightning · · Score: 4, Informative

    Because it doesn't reach orbital velocity, the shuttlecock system keeps the speeds down to a reasonable level and heat shielding is minimal.

    Right. Falling into the atmosphere from just above it at a moderate speed is much less heating than hitting it sideways at nearly orbital velocity.

    But while you're still doing atmospheric flight you only have to deal with the friction from the airspeed you need to get your lift - and you have an atmosphere around you to dump it into continuously.

    Once you "pop out" you have the additional energy of your fall back from your peak altitude to flight altitude to deal with. That's a LOT. Any excess of that over the kinetic energy of your flight speed shows up as heat in your skin, mostly in the very short time near the end of the transition from "air might as well not be there" to "thick enough to fly in". This is in ADDITION to the continuous heating of the skin by flight friction - which didn't get much chance to cool by conduction in the near-vacuum of the hump flight.

    If you weren't firing your engines while up in the near-vacuum it's close to a wash - you converted flight kinetic energy to altitude, then back. So it's similar to just the air friction from cruising at the high altitude and speed. If you fired your engines in the near vacuum, the portion of that energy that went into accellerating you comes back as extra heat.

    So it's not as big a problem as with a shuttle (which dumps most of its orbital energy as a couple thousand mile streak of purple ionized ceramic vapor). But it's not trivial either. (Especially since you'll be flying pretty darned fast just before you leave the effective atmosphere if you want to get very far above it.) Thus the recently added heat shielding.

    --
    Bantam Dominique roosters crow a four-note song. Once you've heard it as "Happy BIRTHday" you can't NOT hear it that way
  34. First FAA license by Eric+Smith · · Score: 4, Informative
    received a license from the FAA, the first license for a suborbital rocket."
    No, it's the first commercial license issued for a MANNED suborbital rocket, which is much more significant.
    1. Re:First FAA license by weglian · · Score: 1

      Actually, it's the first license for a reusable launch vehicle. (It just happens to be suborbital) The FAA has had regulations on the books for RLVs since about 1999, but no one had applied for a license until the past year. They still have 2 more applications in the works.

  35. Re:Bet this one only went 1/3 of the way because.. by Ungrounded+Lightning · · Score: 1

    They have reaction control and heat shielding on the craft as of present. The heat shielding was recently added.

    Right.

    This flight would be to check the airworthyness of the craft with all systems installed (but some not yet required to be operational for mission success).

    If everything went well I'd expect the next flight to actually use the reaction attitude control in lieu of control surfaces (if they didn't check that this time around), or to go up high enough that they're actually needed for flight control (if they did check 'em out this time).

    --
    Bantam Dominique roosters crow a four-note song. Once you've heard it as "Happy BIRTHday" you can't NOT hear it that way
  36. Re:Bet this one only went 1/3 of the way because.. by Anonymous Coward · · Score: 3, Interesting
    A few months ago I got a behind-the-scenes tour of Scaled Composites facilities in Mojave. Of course the highlight of the day was getting to walk around the hangar where the Space Ship One and White Knight were stored. I can assure you that they have the thermal control and attitude control problems taken care of. Exoatmospheric, they use reaction jet thrusters to orient the spacecraft, just like any manned spacecraft. For the re-entry, the pilot really has to do nothing, just feather the wings and the spacecraft is inherently stable and will seek the desired re-entry attitude. Moreover, the re-entry attitude (seen in this page's banner (third of left at top)) presents a large surface area... to accomplish most of the decel in the higher, thinner atmosphere where heating is not as much of a problem. Of course, they can do this because, unlike the shuttle, they have no need to provide lift, which would require higher speeds in denser air and leads to temperature issues.

    WYIAARS.

  37. Providing some numbers... by Einer2 · · Score: 1

    The change of potential energy in going up 100 km (the X-Prize limit) is going to be approximately m*g*h = m*(980 cm/s^2)*(1E7 cm) ~ [m * 1E10] ergs.

    The amount of kinetic energy needed to kick into orbit once you're there is m*G*M_E/R_E = m*(6.67E-8)*(6E27 grams)/(6.5E8 cm) = [m * 6E11] ergs.

    Thus, the ratio of energies is approximately 1:60. Since you'll be doing a lot of that extra accelerating for orbital trajectory in atmosphere, it'll probably be an undetermined amount more to account for air friction.

    Interestingly enough, if the spaceship completely stops relative to the Earth at 100 km, then by the time it's dropped back down to 20 (neglecting air friction in between), it'll only have a velocity of 1.3E5 cm/s ~ 3000 mph. The air friction is going to be a lot less than for orbital craft that enter atmosphere at something like 17,000 mph.

    Barring math errors, of course. It's amazing how easy it is to lose decimal places when you didn't sleep the night before...

    --
    Microsoft delenda est!
    1. Re:Providing some numbers... by Anonymous Coward · · Score: 0

      You forgot the 1/2 in the kinetic energy calculation.

      The virial theorem for an inverse square force.
      K=-(1/2)*U

    2. Re:Providing some numbers... by Einer2 · · Score: 1

      And there we go, so the real factor is approximately 1:30. Thus, 1:25 is a lot more consistent with an Intro Physics reality than 1:12.

      Heh. Virial theorem? I wasn't going to do anything requiring so much thought.

      --
      Microsoft delenda est!
  38. July 4, 2004 by puzzled · · Score: 1



    I pick July 4, 2004 as the first private suborbital spaceflight date. Anyone else got a historically significant date they might pick?

    --
    I am very easy to get along with, but I don't have time to waste being nice to people who are being stupid. -Theo
    1. Re:July 4, 2004 by lommer · · Score: 1

      Yea, I'd pick July 1st - Canada's birthday! :-)

  39. More than bragging rights...? by Pi_0's+don't+shower · · Score: 1
    I find it very interesting that this is sponsored by Paul Allen:

    (Link to Article)

    Perhaps if there were some way of capturing people's imagination (i.e. capturing people like Paul Allen's or other bajillionaires imaginations), more private people would invest in natural science? Private corporations sure aren't going to do it anymore -- look at the demise of pure science at Bell Labs. This is perhaps something positive on multiple fronts... with the potential to grow the investment of wealthy individuals into research science, if it's advertised correctly.
  40. Why liquid? by RobM · · Score: 1

    > Moreover, they are using a solid propellant
    > rocket motor. They would have to switch to
    > liquid engine to go suborbital, and that
    > implies a heck of a lot more mass

    Why a liquid propellant engine is necessary for (sub?)orbital flight? From their webpages, I understand that their engine uses "hybrid" solid/liquid propellants and is restartable a certain number of times...

    Are there other things I should know regarding liquid engines features but I don't because I'm not a rocket engineer? :-)

    Ciao,
    Rob!

    --
    AniToolBox! An Open Source animation program!
  41. I don't know about 2 stage by Anonymous Coward · · Score: 0

    This design seems like it would be conducive to a 3 stage to orbit craft. Imagine a huge Whte Knightish craft and then a winged space shipe oneish craft with a another sub pod slung underneath that. Release that 3rd stage at 100km to orbit. Probably won't be a large payload, but imagine universities and small private oragnizations suddenly being able to launch ther own microsats, at very resonable prices.

    If Scaled does develop a modified version of Space Ship One (Space Ship 2?) for launching microsats, they could probably make mint selling launching services and pay for it's development, even if they don't get the $10 million of the x-prize

  42. Cannot be scaled to orbital by A+nonymous+Coward · · Score: 2, Informative

    These go pretty much straight up and back down. Probably don't need to go much over 5-10 times the speed of sound at most on the way up, and much less coming down, since they are made of composites. Orbital requires going real fast (17,000 mph) much closer to horizontal. The de-orbit is where the heat comes in. Unless you carry enough fuel up to slow down entirely by rocket power, you have to scrub that speed by friction with the astmosphere. Maybe real careful and slow and cautious aero braking would do it, but I doubt that's their game, and certainly not with anything based on SpaceShip One.

    However, the tourist angle (#1) might be reasonable. But who knows how much rich folk will pay for a few minutes of weightlessness and an astronaut badge?

    1. Re:Cannot be scaled to orbital by smartalix · · Score: 1

      You certainly underappreciate tourism. It already costs over $30,000 to "climb" Everest, and it's so popular the entire route has to constantly be swept for trash left by rich pampered tourists.

      A suborbital flight with official astronaut recognition (the Air Force only requires a pilot to go 50 miles up to be recognized) would sell like hot cakes for $50,000 a pop, and would be profitable for Rutan after a relatively small number of flights.

      Tourist income would also be supplemented by microsattelite launches, as Rutan anounced previously that the SSO will be able to fire rockets, much like a fighter plane, at the top of its arc to launch such devices.

      --
      Read a preview of my novel CYBERCHILD at www.smartalix.com/cyberchild
  43. are any of the teams.... by zogger · · Score: 1

    ...contemplating using a helium balloon as the "first stage" of a launch? Or is this allowed? Starting at 50-60 thou feet or above before it lights might be a nice edge....

    total aside, grew up watching "man in space". It's been nice, was sad to see them abandon the X series , then go back to it years later, badly...lost opportunity there.. anyway, as a kidm I, along with several million other people got stunned, and went outside and tried to see sputnik (didn't)(tell you, it weirded people out, scared them), although I did see ECHO later on. Chemical rockets ar... old news,I'm just not impressed or juiced over it any longer, except for this thing, but....... really... I'm holding out for a last minute dark-horse entry that sweeps the tourney, from some physics nerds, the release of the "civvie version" electrogravitic distortion propulsion craft.

    one can hope... I got ten clams that "da man" already got one, or several..

    1. Re:are any of the teams.... by merdark · · Score: 2, Informative

      are any of the teams contemplating using a helium balloon as the "first stage" of a launch? Or is this allowed? Starting at 50-60 thou feet or above before it lights might be a nice edge....

      Yup, the Da Vinci Project is. They are also supposedly good to go within a year. But no launch date has been set yet. And since they launch from Canada, I guess they don't need any license from the USA?

      http://www.davinciproject.com/beta/Technical/Tec hn icalMain.html

  44. July 2, 2004 by bluGill · · Score: 1

    The actual flight will take place on July 2nd, 2004, but they will wait to release that information until July 4th.

    For those outside the US: the U.S decleration of independance was adopted on July 2nd, 1776, but not actually ratified until the 4th. (It is slightly more complex than that, read the link)

  45. 100km flight on Monday? by Fenris+Ulf · · Score: 1

    The first supersonic test was on December 17th, the 100th anniversary of powered flight.

    This Monday will be April 12th, the anniversary of the first human spaceflight, and the first shuttle launch.

    Perhaps we can expect a major milestone next Monday?

    1. Re:100km flight on Monday? by Anonymous Coward · · Score: 0

      My bet is May 5th. May 5th, 1961 was when Alan Shepard made his suborbital flight, making him the first US astronaut in space.

  46. all right! by zogger · · Score: 1

    80,000 feet before first burn! that's thinking! I thought it might be a good idea! Thanks for the URL!

    There used to be some big start up space company that wanted to use expended fuel sections from other launches, link them together, and make cheap orbital platforms out of them. I think they were going to be supported by Hilton hotels, but I haven't followed it. I like off the wall thinking, turning expendable/waste stuff into useful products.

  47. Re:Lindbergh wasn't trying to be a transatlantic t by JohnsonWax · · Score: 2, Informative

    A lot of the aviation 'firsts' had nothing to do with commercial interests on the part of the participants. They just wanted to DO it, because they thought they could.

    Uh huh.

    While I won't argue that Lindbergh was interested in doing this, the $25,000 Raymond Orteig Prize was most certainly a driving force behind the actual attempt. Even the most noble person needs to eat, and unlike science, engineering advances almost always come with some reward, be it financial or strategic.

  48. Please learn how to use links. by Anonymous Coward · · Score: 0
    Please learn how to use links.
    <a href="http://www.armadilloaerospace.com">John's toy</a>
    yields: John's toy
  49. Please learn how to use links. by Anonymous Coward · · Score: 0
    Please learn how to use links.
    <a href="http://www.armadilloaerospace.com">John's toy</a>
    yields: John's toy
  50. yeah wtf by Anonymous Coward · · Score: 0

    i know the x prize is like 100k plus and i read the story title as 105km and was like damn! they beat everyone else!! now they just have to do it a second time...

    sadly i am disapointed by a stupid unit error. why oh why doesnt the USA use metric yet? is it just arrogance or what?

  51. Re:Lindbergh wasn't trying to be a transatlantic t by Anonymous Coward · · Score: 0

    Actually, you will find the Brit flight in American aviation books. Some of the better ones will have the Brit flight, but it involved a few stops along the way...

    Now, the British around-the-world flight is in the books, because it essentially was not repeated on the scale of Lindbergh until the Voyager flight a few years ago.

  52. Re:Lindbergh wasn't trying to be a transatlantic t by Anonymous Coward · · Score: 0

    You realize that the first nonstop transatlantic flight was made by a couple of Brits, not Lindbergh. He was first to solo. I think the flight by the British really was more important historically, but you won't find it in any American textbooks.

    It's good that you included "nonstop" because some guys in a flying boat made the trip a bit earlier.

    And anyway, these days you won't find Lindbergh in very many American textbooks either.

  53. Problems with Solid Rockets by Teancum · · Score: 2, Informative

    The Shuttle SRB's, the only man-rated solid rocket ever made, is indeed a rocket that once fired must get fully used, and ejected if you need to quit using it.

    Another benefit of using liquid fuels is that you can throttle (I.E. change the flow rate) of the rocket engine as it is fired.

    Think about it this way: When you are firing a rocket you are also throwing away mass (Newton's F=ma equation). At the same time, when you are using a typical rocket engine, the actual amount of energy being send out the nozzle stays roughly constant throughout the burn, assuming that you can't throttle the rocket. This means, working the equation backward, force stays constant, but the accelleration rises as the mass drops.

    Rockets like this are just fine for a nuclear warhead or for a solid well-built military satellite, but toward the end of the burn you can hit 20 G's or more. Even the Saturn V had this problem to some extent (the Apollo astronauts sometimes hit as high as 8 G's of accelation for brief moments). The Shuttle main engine has adjustable engines that fire at about 105% thrust rating on the launch pad and dropping to about 80% of the rating as it starts gaining altitude... in part to make the ride easier on the passengers.

    While there are other issues to follow through, this is something else to consider, and why especially with manned rocket they are almost always liquid rockets.

    In addition, the specific impulse (the amount of energy release by a pound of rocket fuel) is sometimes higher with liquid fuels. This is mainly a matter of chemestry, but several factors go into it. I'm sure, however, that some solid propellants have a higher specific impulse than LH2/LOX (the fuel typically used by NASA on the upper stages of most of the manned rockets... this is what caused the falling chunk of ice/foam that destroyed Columbia).

    1. Re:Problems with Solid Rockets by RobM · · Score: 1

      Thenks for the reply! :-)

      From the FAQ on Scaled website, they state that the engine can be stopped and restarted many times (even if it's not all that useful since the max burn is about 90 seconds IIRC).

      On SpaceShipOne however there's no provision for engine throttling. They don't state if this is because it has been considered not useful for SpaceShipOne mission profile, or if it can't be done with their tecnology.

      Their engine works (from their site) mixing liquid N2O with HTPB rubber at high temperature. it would be useful to know if in such reaction controllig N2O flow or temperature can achieve throttling or not.

      Ciao,
      Rob!

      --
      AniToolBox! An Open Source animation program!
  54. CEV Vs. SpaceShipOne by nixcha · · Score: 2, Insightful

    I recently read an article in the UK magasine "Focus" which outlined NASA's ditching of the shuttle over more Apollo style rocket+capsule launch systems. After all the effort they've put into the shuttle it looks like NASA has decided that "space plane" style vehicles just simply isn't economically feasible, and will never become the cheaply reusable vehicle they had hoped for.

    Yet at the same time the private sector is clearly getting close to achieving success at the 100km mark. I realise this is very different from the kind of application NASA will be needing out of their kit - but surely the shear potential of such space access would make it worth NASA pursuing further.

    It seems to be that all the advances that have been made by the shuttle will be lost when NASA takes a step back to using the capsule+rocket method.

    1. Re:CEV Vs. SpaceShipOne by pfdietz · · Score: 1

      I don't think NASA has concluded that winged launch vehicles will never be feasible.

      I think they have concluded that the shuttle is irremediably flawed, and that developing a winged Shuttle II would not make economic sense at this time.

    2. Re:CEV Vs. SpaceShipOne by Anonymous Coward · · Score: 0

      "...but surely the shear potential of such space access would make it worth NASA pursuing further"

      Shear potential? They can get wool from space?

      Oh, SHEER potential...

  55. Don't forget us brits ! by mcraig · · Score: 2, Informative

    Well as you obviously haven't noticed I thought I'd point out that us brits have a good contender in Steve Bennet who founded starchaser industries they've had lots of succesful launches and I would say they are a lot further along than Carmack though perhaps not quite as far as Rutan. Check it out www.starchaser.co.uk I believe they are scheduled to make an x-prize attempt this year.

  56. Re:turns out that they can glide down the whole wa by cheekyboy · · Score: 1

    TO reduce or get rid of heat from the air, you can generate a plasma field around you so the air never touches you, but that is hard. A simple way to do that is to have a rocket flame/jet burst out in front of you, not behind you, ironicly that speeds up re-entry since it heats up the air infront of you and causes a plasma to be made and all other air just moves around you and never touches you. Great trick, it has been tested once.

    --
    Liberty freedom are no1, not dicks in suits.
  57. rotary rocket by cheekyboy · · Score: 1

    pitty rottery rocket didnt get finished, it had high hopes

    http://www.airspacemag.com/asm/Web/Site/QT/RRock et .html

    --
    Liberty freedom are no1, not dicks in suits.
    1. Re:rotary rocket by pfdietz · · Score: 1

      I didn't have high hopes. Their approach was too exotic and their goals too radical for what they could afford to develop. Not surprisingly, they ran out of money before they got very far.

  58. TICKETS!!!! by Anonymous Coward · · Score: 0

    As soon as Scaled gets a stable ship, I got $10,000 cash for a chance to fly! Wonder if that will cover the costs for their hybrid fuel (pelletized rubber like the other hybrid engines?)

    I bet I am not the only one that would blow some money for a ride. Question is, what will the price of admission be? (and is there a booth at the end selling pictures, coffee mugs and T-shirts?)

  59. Re:Bet this one only went 1/3 of the way because.. by PhaseChange · · Score: 1

    They might be closer to that than you think. From Scaled's web site (describing unpowered test flight on 11 March):

    The twelfth flight of SpaceShipOne. Objectives included: pilot proficiency, reaction control system functionality check and stability and control and performance of the vehicle with the airframe thermal protection system installed. This was an unpowered glide test.
    Results:

    Launch conditions were 48,500 feet and 125 knots. All systems performed as expected and the vehicle landed successfully while demonstrating the maximum cross wind landing capability.

  60. Pity poor StarChaser by It'sYerMam · · Score: 1

    Unfortunately, because they can afford to spend more than the prize money, the UK's team (StarChaser) cannot really compete. We are, apparently, in second place behind Scaled Composites.
    The X-Prize cannot be entered by groups that have government funding to ensure that this doesn't happen, but unfortunately for us, there're people out there with lots and lots of cash. In the meantime we have to wait until someone gives us some :D

    --
    im in ur .sig, writin ur memes.
    1. Re:Pity poor StarChaser by cosmo7 · · Score: 1

      I understand your plan to use a cement mixer as your capsule kind of puts the ick on big sponsorship deals, people thinking you're insane, etc.

      Good luck anyway.

  61. how come all you geeks don't talk about by wtfu2 · · Score: 0, Troll

    the little company that built the engine for spaceship one? spdv.ob (spacedev). a couple weeks ago they got their biggest contract ever from the mda to build a bunch of satellites. one of them is supposed to have a laser??!! my buddy and i over beers were talking about how they will eventually combine the satellite laser technology with rfid and start zapping unprofitable demographics as a drag on the us economy (that is, if cigarettes haven't killed you already)

  62. Re:Lindbergh wasn't trying to be a transatlantic t by LWATCDR · · Score: 1

    As an American I would say you are wrong. I rember reading about the first nonstop flight. It was in a Vickers Vimy converted WWI bomber. The landed in bog In Ireland.
    The funny thing is that almost no one rembers what prize Lindbergh was going for. It was not a solo Atlantic crossing. Lindbergh's claim to fame was the first nonstop flight from New York to Paris. He did not have to do it solo at all. In fact most of the other teams where just that teams. Lindbergh figured he would rather have more fuel then a navigator. He was also the dark horse lacking any real fame or backing.

    --
    See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
  63. But it's not suborbital! by A+nonymous+Coward · · Score: 1

    I agree, suborbital flights for $50K would sell like hot cakes. But SpaceShip One does not make suborbital flights, it merely goes straight up and backdown, and how much will that bring in? Sure, some ... but enough to keep it busy and pay the bills?

    1. Re:But it's not suborbital! by Wyatt+Earp · · Score: 1

      But, one doesn't need to orbit to be an Astronaut.

      17 July 1962 X-15 Flight 62 Spacecraft: X-15A. Launch Site: Edwards . Launch Vehicle: X-15A. More details

      FAI world altitude record. Maximum Speed - 6166 kph. Maximum Altitude - 95940 m. First astronaut wings flight (USAF definition).

      17 January 1963 X-15 Flight 77 Spacecraft: X-15A. Launch Site: Edwards . Launch Vehicle: X-15A. More details

      First civilian flight above 80 km. Maximum Speed - 5917 kph. Maximum Altitude - 82810 m. Second astronaut wings flight (USAF definition).

      http://www.astronautix.com/project/x15.htm

      I'd throw down 50K to get civie astronaut wings.

    2. Re:But it's not suborbital! by smartalix · · Score: 1

      Straight up and straight down (actually an arc, but for argument's sake, let's assume it is a completely vertical path) to space (over 50 miles as defined by the USAF) IS a suborbital flight. What do you think the term means? A fraction of an orbit is a fraction of an orbit. How much of a fraction is moot, the point is getting up there with three people.

      --
      Read a preview of my novel CYBERCHILD at www.smartalix.com/cyberchild
  64. sub-orbital to orbital by XNormal · · Score: 1

    It should be relatively simple to modify any X-Prize class vehicle to be a reusable first stage for a nanosatellite launcher.

    The upper stage can be a cheap and reliable expendable like Dan Moser's Comp-L design. Staging is done in a very benign environment: vacuum and zero G. You can literally open the door and push it out with a spring loaded device. A rotating platform can spin the upper stage first for stabilization. The upper stage and payload need no aerodynamic fairing and are subjected to very low loads. In vacuum it is possible to use a high expansion ratio nozzle to get high Isp even from a low pressure engine with pressure fed propellants.

    --
    Stop worrying about the risks of nuclear power and start worrying about the risks of not using nuclear power.
  65. Simpsons quotage (can't resist) by Scrameustache · · Score: 1
    They have to have accomodation for 3 passengers, but they can substitute an equivalent mass of inert payload instead.

    Buzz: Mission Control, this is Corvair. Launch sequence initiated. All systems go.

    Homer: Are we there yet? I'm thirsty.

    Race: Mission Control, request permission to sedate cargo ahead of schedule.

    Controller: Permission denied.


    : )

    --

    You can't take the sky from me...

  66. Re:Lindbergh wasn't trying to be a transatlantic t by Anonymous Coward · · Score: 0

    And don't forget Lindbergh was a Nazi