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Blue Origin Building DC-X Lookalike

rrohbeck writes "The New York Times is running an article on what Blue Origin (Amazon.com founder Jeff Bezos' space company) is up to after his Texas land grab. A couple of Flash videos show a short successful test hop of the 'Goddard' test vehicle. From the article: 'The Goddard has a science-fiction sleekness. Videos show the craft taking off and landing again with a loud whooshing sound. In one view, one of the nine rocket nozzles jitters as it maintains the ship's attitude. Goddard resembles the DC-X, another vertical-takeoff-and-landing craft under development in the 1990s by McDonnell Douglas for the Defense Department and NASA until the government pulled the plug.' And in case you're an aerospace engineer, they're hiring."

106 comments

  1. that's better by macadamia_harold · · Score: 4, Funny

    Videos show the craft taking off and landing again with a loud whooshing sound.

    I suppose that's better than taking off and landing again with a crashing sound.

    1. Re:that's better by Anonymous Coward · · Score: 0

      Is it the same whooshing sound as the doors on the enterprise?

    2. Re:that's better by Thansal · · Score: 1

      very true.

      The device just does not look like it should work the way it does. Sure, the take off looks normal, put at the apex it looks like it should flip over and come down nose first!

      I don't have any sound on this computer so I have a hard time telling, are they ussing some sortta propulssion in the entire flight (something to keep them stable?).

      --
      Do Or Do Not, There Is No Spoon, There Is Only Zuul. Everything in the above post is probably opinion.
    3. Re:that's better by reklusband · · Score: 1

      Well, even a crash landing would be better than...Take off BOOM, or coming in for a landing BOOM... So no matter what they do they've got a 50% chance of being better off than NASA.

    4. Re:that's better by fifedrum · · Score: 2, Insightful

      the thrust is applied throughout the flight, the sound is pretty interesting, wooshing like too much air coming out of a too small nozzle. They don't coast during this test flight at all, it seems, if the sound indicates relative thrust, it's pretty constant, with maybe a few % reduction throughout the flight and a small increase at the end.

      the nozzles adjust during the flight to maintain attitude, I believe the DCx did the same thing. IIRC the DCx also had a series of manuvering thrusters spaced around the ship.

    5. Re:that's better by Rei · · Score: 2, Funny

      You know what? Every time I get out of bed, I don't explode. I guess this makes me 100% better than NASA.

      What's that? I'm comparing apples and oranges by comparing "getting out of bed" with "getting many tonnes of payload to a low-earth orbit"? You don't say...

      --
      Dear Lord: I don't want to go back to college, so please help me be sexy. Amen.
    6. Re:that's better by Anonymous Coward · · Score: 0

      The big difference is you're not a rocket, and 'Goddard' is. HTH.

    7. Re:that's better by Rei · · Score: 1

      My mistake. All rockets are the same. Silly me. So, given that I'm almost always successful when launching bottle rockets...

      --
      Dear Lord: I don't want to go back to college, so please help me be sexy. Amen.
  2. It made me think of... by d3m0nCr4t · · Score: 3, Funny

    Douglas Adams: "I love deadlines. I like the whooshing sound they make as they fly by." :D

    1. Re:It made me think of... by Anonymous Coward · · Score: 1, Funny

      Jeff Bezos finally gave the world a peek at his rocket.

      Bezos sex tape?

  3. slow on the uptake by neurostar · · Score: 0

    Wow, slashdot is kinda slow on the uptake. I read about this a few days ago.

    1. Re:slow on the uptake by Bucc5062 · · Score: 3, Informative

      Actually, slashdot is true toform and dup'ing the news. This http://science.slashdot.org/article.pl?sid=07/01/0 3/2344241 was posted on Jan 3. Even repeated it is a cool story.

      --
      Life is a great ride, the vehicle doesn't matter
    2. Re:slow on the uptake by Thansal · · Score: 3, Informative

      well, it is a dupe (and hey, the /. story is actualy earlier then the pythom one):
      http://science.slashdot.org/article.pl?sid=07/01/0 3/2344241

      --
      Do Or Do Not, There Is No Spoon, There Is Only Zuul. Everything in the above post is probably opinion.
  4. Quick, somebody call Mork; by The_REAL_DZA · · Score: 2, Funny

    I think we've found his egg!

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    This space intentionally left (almost) blank.
  5. Makes sense by tsotha · · Score: 3, Interesting

    DC-X was a very successful program. It had many successful flights until the Air Force turned it over to NASA and NASA crashed it on the first flight. Then they cancelled it.

    1. Re:Makes sense by Anonymous Coward · · Score: 0

      How hard can it be not to crash on its maiden voyage?

      Its not rocket science.

    2. Re:Makes sense by Richard_at_work · · Score: 3, Informative

      NASA flew the DC-X four times, with it being lost on the fourth flight. The US Airforce programme damanged the DC-X on its last flight with them and refused to spend funds on repairs, which was why NASA stepped in - they offered the funding to repair the vehicle and resume testing.

  6. Dang, what am I still doing QA work for? by StefanJ · · Score: 1

    I AM a rocket scientist!

    Well, actually, seriously, I'd hate to get a job at one of these places and then end up finding it tedious and hating it, the way I end up hating everything once I get into Type-A workaholic mode.

  7. A little optomistic by Silver+Sloth · · Score: 2, Interesting
    From TFA

    That craft, as the site says, will be "designed to take a small number of astronauts on a suborbital journey into space." The pace is deliberate, with commercial trips starting as early as 2010 285 ft today, commercial sub orbital space in three years time. That doesn't sound like a deliberate pace, it sounds a bit rushed to me.
    --
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    1. Re:A little optomistic by mianne · · Score: 1

      285 ft today, commercial sub orbital space in three years time. That doesn't sound like a deliberate pace, it sounds a bit rushed to me.

      Three years was once a considerable amount of time when it came to rocket science.

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      Javascript, cookies, flash, and ActiveX must be enabled in order to view this sig.
    2. Re:A little optomistic by camperdave · · Score: 3, Insightful

      Taking off and landing safely are the two biggest obstacles to suborbital flight. They seem to be doing those two well enough. The only remaining obstacle seems to be altitude, which is simply a matter of working out the payload/fuel constraints. The Scaled Composites team took only three years from start of development to taking the X-Prize. 2010 is not an unreasonable goal for going from fully functional testbed to production vehicle.

      --
      When our name is on the back of your car, we're behind you all the way!
    3. Re:A little optomistic by FleaPlus · · Score: 2, Informative

      285 ft today, commercial sub orbital space in three years time. That doesn't sound like a deliberate pace, it sounds a bit rushed to me.

      As another commenter mentioned, taking off and landing (which they've just demonstrated) are the most difficult parts of a launch. Additionally, SpaceShipOne went from starting full development in 2001, to their first test flight in 2003, to their first suborbital flight in 2004.

    4. Re:A little optomistic by Anonymous Coward · · Score: 0

      This first flight actually shows me that Blue Origin is much further along than I had realized, but they have even further to go. To put 285 feet in perspective, their Goddard capsule reached almost as high as an Apollo capsule atop a Saturn V, sitting on the ground.

      Unfortunately, their "only remaining obstacle" is a much bigger one than your post belies. The current capsule is sub-scale, which means it doesn't yet have the payload they will need, and they don't yet have engines capable of reaching space. 2010 is not unrealistic, but it is ambitious.

  8. They're hiring? by Overzeetop · · Score: 0, Flamebait

    That looks like fun. Too bad I'm on the wrong coast and don't want to move. 9 years with NASA designing and building flight hardware, 6 in industry, MS in structures plus courses in Space Veh Prop, Guidance and Nav, and have owned my own 4 person SE firm for 4 years. GD&T and Pro/E is probably a hair on the rusty side, but it's like riding a bike. Built my own small-scale solid fuel rocket engines.

    I wonder what they pay?

    --
    Is it just my observation, or are there way too many stupid people in the world?
    1. Re:They're hiring? by kfg · · Score: 3, Funny

      I wonder what they pay?

      Money.

      KFG

    2. Re:They're hiring? by Anonymous Coward · · Score: 0

      Actually, I'll bet they pay "dollars", as opposed to actual "money".

    3. Re:They're hiring? by kfg · · Score: 1

      I'll have you know that "dollars" are completely supported by futures in unsecured bad debt; the most sophisticated financial instrument yet devised by man.

      KFG

    4. Re:They're hiring? by Anonymous Coward · · Score: 0

      and an endless supply of Hot Pockets

    5. Re:They're hiring? by Gramie2 · · Score: 1

      So you don't want a job with them and it's entirely irrelevant, but you felt like telling us why you are such a hardware stud. Thanks for sharing.

    6. Re:They're hiring? by Overzeetop · · Score: 1

      Yeah, I'm in that kind of mood today.

      C'mon - when I was in college we used to joke that there was a senior aero course called "Advanced Unemployment Line Mechanics." It's not often a company likely to do cool things happens to fit my background. Let me crow a little. Ignore me if you like. Eveybody else does.

      --
      Is it just my observation, or are there way too many stupid people in the world?
    7. Re:They're hiring? by Gramie2 · · Score: 1

      Then apply to that company. Call them up and see if what they are doing fits what you are doing. Just offer to take their engineers out for a beer when they're in town, because you know their pain and they know yours.

      But the feigned insouciance: "oh, I'm not interested..." seems a bit prima donna-ish

    8. Re:They're hiring? by Forbman · · Score: 1

      free shipping on Amazon.com orders over $14.92

    9. Re:They're hiring? by Overzeetop · · Score: 1

      Actually, I am interested in what it would be like 'cause it does sound cool, but it turns out I really don't have a desire to move to the west coast. Been there, done that, bought the T-shirt.

      We all have our moments...yesterday I had mine.

      --
      Is it just my observation, or are there way too many stupid people in the world?
    10. Re:They're hiring? by Media+Withdrawal · · Score: 1

      But the feigned insouciance: "oh, I'm not interested..." seems a bit prima donna-ish

      Boy did you ever hit the nail on the head! The bane of any rocket company's existence is prima donna rocket scientists. You must never hire these guys, they'll sink your program and they're everywhere. Space attracts that personality type. I worked at a rocket company once, and we had 4 prima donna engineers each presenting their own redundant, slightly different designs as the "final" design to the customer. They routinely went over their manager's head to the company owner. Of course their rockets always crashed, though they swore that never happened in previous jobs.

    11. Re:They're hiring? by Anonymous Coward · · Score: 0

      How serious can it be? -- they're using C for goodness' sake!
      Even Britain's Embedded C for autos report says don't do it - use Ada instead.

  9. Who needs spaceships? by Non-CleverNickName · · Score: 1

    I, for one, will just wait for Willy Wonka to finish the Phase III testing of his fizzy lifting drinks

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    1. Re:Who needs spaceships? by sentientbeing · · Score: 1

      Coke and Mentos works equally well as a propellant.

      The tricky part is dealing with the ants and wasps on the launchpad..

      --

      ------
      beware he who would deny you access to information, for in his mind he dreams himself your master
    2. Re:Who needs spaceships? by Moofie · · Score: 1

      Hmm. Most insects don't seem to care too much about NutraSweet, and diet soda is the preferred working fluid.

      --
      Why yes, I AM a rocket scientist!
  10. Not like DC-X by J05H · · Score: 5, Informative

    The Blue Origin's vehicle isn't anything like DC-X, except that they are both VTVL. The Goddard/New Shepard vehicles are axisymetric, base-first reentry and use hydrogen peroxide/kerosene. DC-X (and follow-ons) were biconic, used a side-first reentry with body flaps and were LOX/LH2 powered. Very different machines, both these test vehicles and any further versions. DC-X was based on the classified AMARV test article, the Goddard is more like the old "mega capsule" heavy lift concepts from the 60's and 70's, such as Boeing's LEO.

    All the best to Bezos and Blue Origin! The flight video is excellent!

    Josh

    --
    gigantino.tv - Heavy but weighs nothing.
    1. Re:Not like DC-X by Anonymous Coward · · Score: 0

      Why is it that nearly all of these upstart aerospace wannabe companies ignore basic concepts like escape velocity? You can't get more than a few hundred feet off the ground without a massive rocket propelling you up to speed to escape Earth's gravity....

    2. Re:Not like DC-X by Rei · · Score: 1

      Apparently you've forgotten that you're on Slashdot, where:

      1) A minimally suborbital vehicle is only a hop, skip, and a jump from being an orbital vehicle.
      2) A heavy, low ISP vehicle without a TPS is a stepping stone (or even "an upper stage") to an orbital craft.
      3) A rocket that carries a few hundred kg up 100 km is somehow something new, and is somehow a significant force to advancing rocketry technology, simply because the payload is humans instead of sounding rocket insturmentation.
      4) If two spacecraft look alike, they *are* alike.

      Oh, heck, lets throw "5) NASA does nothing useful and messes up disproportionately often" and "6) Corporations are the answer to reducing launch costs" in there too, for good measure.

      --
      Dear Lord: I don't want to go back to college, so please help me be sexy. Amen.
    3. Re:Not like DC-X by 'nother+poster · · Score: 1

      1) I don't think anyone said it was.

      2) H2O2/Kerosene isn't LOX/LH2, but at an ISP of 319 in vacuum (273 at sea level) it's no slouch and can be handled and stored much easier. (no cryogenic storage needed)

      3) Yep, it is. This and the other X Prize ships are made on shoestring budgets and are getting experimental "manned" ratings. I assume you understand what that means, but are ignoring it.

      4) Nobody said they were alike beyond looks. You didn't, the grandparent didn't, and rrohbeck, the submitter, didn't. They do resemble each other. They are both sort of cone shaped with rounded bottoms, although Goddard is shorter and broader.

      5) Nobody in this thread said that as far as I can tell.

      6) Well, you brought it up, but I don't see how corporations can make it worse. I'm sure it was faster and cheaper to go from NYC to LA by air before corporations got into the airline business.

    4. Re:Not like DC-X by Anonymous Coward · · Score: 0

      'Escape velocity' is only relevant for unpowered devices, please don't talk about that which you don't know so that others who do will be more easily heard.

    5. Re:Not like DC-X by Rei · · Score: 2, Informative

      1) People *always* say that on rocketry forums on Slashdot. It's a tradition.

      2) Stored much easier? Apparently you've never dealt with high-test peroxide. It's not like the stuff you find in your medicine cabinet. Ask the crews of the Sidon and the Kursk what they think of this "easy" to store material.

      3) Okay, lets pick one -- SS1. Budget ~25 million. Payload -- ~300kg to 100km. Per-launch cost undisclosed, but believed to be about half a million dollars. Lets compare this to, say, the SR-S sounding rocket: ~100kg to 200km, which should be a roughly equivalent challenge. Price: $95,000/launch (one launch to date). Total program budget at time of initial launch: $1.7 million (which developed and tested two scorpius designs, and initial work on the upcoming, larger variants). The entire Scorpius project (leading up to multiple orbital variants) is expected to be $20-25 million.

      Yes, they didn't have to make it man-rated ("experimental" man-rated, that is ;) ). And if you want a sounding rocket with more launches under its belt, the development costs are generally several million more. But if you want to call projects like SS1 "shoestring budgets", I'm just going to laugh. Sounding rockets are trivial compared to orbital rockets. SS1 serves the same role as a payload-recovery sounding rocket. Don't expect "oohs" and "aahs" just because some companies add a cockpit/cabin and charge an arm and a leg for people to ride. Heck, for the price of a SS1 launch, you could launch twice the payload nearly to orbit on a Black Brant XII.

      4) It was implied, and see #1.

      5) See #1.

      6) That's the thing: the space industry currently *is* run by corporations. While development is generally (but not always**) government subsidized, corporations usually (but not always**) bear the operating costs, compete for launch contracts, and gain the profit from the launches -- just like in any other industry.

      ** -- For example, the Orbital's Pegasus, SeaLaunch's Zenit, and SpaceX's Falcon.
      *** -- For example, everyone's favorite punching bag, the Space Shuttle.

      --
      Dear Lord: I don't want to go back to college, so please help me be sexy. Amen.
  11. Can't get to orbit that way by Animats · · Score: 4, Insightful

    It looks impressive, but you can't get to orbit that way.

    Single stage to orbit craft have to be somewhere above 97% fuel, with the best chemical fuels possible. People have tried to build SSTO craft, Rotary Rocket being a good example, but when your weight budget is that tight, it's next to impossible, and even if it works, the payloads are dinky.

    Two stages work. The Shuttle is two stages; the solid boosters and the external tank are dropped off. To get to orbit on chemical fuels and have any useful payload, you have to dump some mass during lift. Even with two stages, the weight reduction efforts result in fragile spacecraft.

    Now if we had nuclear rockets, we could get somewhere.

    1. Re:Can't get to orbit that way by jandrese · · Score: 1

      Of all of the possible uses of Nuclear power, using it to power a rocket out of the atmosphere is perhaps the last one I'd want to see actually implemented. It is hard to think of a better way of spreading radioactive particles all over a huge landscape, not to mention what happens when you crash.

      --

      I read the internet for the articles.
    2. Re:Can't get to orbit that way by Cassini2 · · Score: 1
      Now if we had nuclear rockets, we could get somewhere.
      Would we get there in one piece?
    3. Re:Can't get to orbit that way by Anonymous Coward · · Score: 0

      Nuclear lift rocket designs don't spray radiation out the back. They use the nuclear reaction to generate heat that warms air that is sucked through the system. The reaction chamber is sealed and is a black surface. It is more like a nuclear "jet" than rocket. Nuclear rockets for space use the straight radiation for propulsion, or a mix of radiation and heated gasses, but those don't have the power to lift anything from earth's gravity, and you probably don't want to be around them if they come back down.

    4. Re:Can't get to orbit that way by inviolet · · Score: 1
      Of all of the possible uses of Nuclear power, using it to power a rocket out of the atmosphere is perhaps the last one I'd want to see actually implemented. It is hard to think of a better way of spreading radioactive particles all over a huge landscape, not to mention what happens when you crash.

      Yes, what a disaster that would be -- we would get trace amounts of radioactive particles on the Earth's surface! Oh teh noes!!!11!

      Been down in any good basements lately? :P

      But seriously, spreading radioactivity "all over a huge landscape" is exactly the safe and optimal way to deal with an exploding nuclear rocket.

      --
      FATMOUSE + YOU = FATMOUSE
    5. Re:Can't get to orbit that way by Rei · · Score: 1

      Space Shuttle is a bit harder to classify into stages, but I'd list it as "2 1/2". The first stage (SRBs) and second stage (SSMEs fuelled by the ET) burn at the same time. The SRBs jetisson relatively early. The ET remains with it almost all of the way, but not quite. The shuttle ditches it (often using the OMS to help deorbit it), and then uses the OMS to get to their final altitude.

      The shuttle could take the ET all the way to LEO, which would make it a true 2-stage rocket, but it could carry little payload if it did that.

      --
      Dear Lord: I don't want to go back to college, so please help me be sexy. Amen.
    6. Re:Can't get to orbit that way by mikeee · · Score: 1

      It could be the top stage of a two-stage SSTO, though.

    7. Re:Can't get to orbit that way by Moofie · · Score: 2, Funny

      Sure! And we wouldn't even need flashlights when we get there!

      --
      Why yes, I AM a rocket scientist!
    8. Re:Can't get to orbit that way by rbanffy · · Score: 1

      I wouldn't want to go through the nightmare of approvals required to fly a fission-thermal rocket.

      I hope someday we could build a fusion-thermal engine. That would make a very interesting SSTO vehicle. Imagine re-entry without need for atmospheric braking.

      In the meantime, I still expect somehow Brukhard Heim's ideas to bring some interesting ideas for propulsion once we reach LEO.

      What could be sweeter than that?

    9. Re:Can't get to orbit that way by rrohbeck · · Score: 4, Informative

      Jerry Pournelle has some data that make it sound feasible.
      A mass ratio of 17 (5.9% payload) with RL-10 engines doesn't sound too bad for a start.

    10. Re:Can't get to orbit that way by FleaPlus · · Score: 4, Informative

      Of all of the possible uses of Nuclear power, using it to power a rocket out of the atmosphere is perhaps the last one I'd want to see actually implemented. It is hard to think of a better way of spreading radioactive particles all over a huge landscape, not to mention what happens when you crash.

      I'm sure it'd be trivial compared to the spread of radioactive particles from coal power plants.

      http://www.ornl.gov/info/ornlreview/rev26-34/text/ colmain.html

    11. Re:Can't get to orbit that way by 'nother+poster · · Score: 1

      Um, ah?!?! SSTO is Single Stage To Orbit. You can't have a "two stage" single stage rocket.

    12. Re:Can't get to orbit that way by Artifakt · · Score: 1

      I think the parent poster was referring to an Orion-like design, which would produce substantial fallout. Some Nuclear lift rocket designs don't spray radiation out the back. Some designs heat external air as a working fluid, some heat H2, water or some other carried mass, some (ion drives) toss electrons, which can be beta particles produced directly in a reaction, or otherwise, but are low acceleration devices (at least for the current generation).
              Unless we get invaded by the Fithp, we probably don't really need an Orion design, but a 1,000 person lunar colony, with quarters, labs, machine shops, vehicles and five years life support supplies, all in one shot, might be worth setting off a few very clean nukes in atmosphere. Still, if you're fussy about that (as I am), sealed pile designs can give us, at the very least, human access to all exploitable worlds and moons as far out as Saturn. Fusion and a patient economic system can probably give us this arm of the galaxy, if it's not already occupied.

      --
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    13. Re:Can't get to orbit that way by powerlord · · Score: 1

      I think you may be on to something. All of the people here keep talking about how you can't get to orbit ... if you start on the ground.

      This things seems to have really good handling, and is probably has less Kinetic energy than most other Launch Vehicles. What if you launched it/recovered it off a stable suborbital platform (say a structure suspended between to dirigibles? (although I suppose that would make this a second stage) ... Or recovered it through the use of a deployed parachute and a ground landing with maneuvering jets used to steer to the Landing Zone.

      Heck, this thing is a VTOL Launch Craft, what makes people think all the answers are going to be what we are used to?

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    14. Re:Can't get to orbit that way by Moofie · · Score: 1

      "two-stage SSTO"

      You're going to need to run that by me again. A two-stage, single stage to orbit rocket? Pretty sure that you've run into a little glitch in your acronym parser there, buddy.

      --
      Why yes, I AM a rocket scientist!
    15. Re:Can't get to orbit that way by Moofie · · Score: 1

      "what makes people think all the answers are going to be what we are used to?"

      Dunno. What makes you think that the people who are thinking about this problem think all the answers are going to be what you think some people are used to?

      --
      Why yes, I AM a rocket scientist!
    16. Re:Can't get to orbit that way by nuckfuts · · Score: 1

      They're not trying to get into orbit. If you had bothered to RTFA, it states that the craft is "designed to take a small number of astronauts on a suborbital journey into space".

    17. Re:Can't get to orbit that way by Cerebus · · Score: 1

      Read this if you haven't already:

      http://www.amazon.com/Project-Orion-Story-Atomic-S paceship/dp/0805059857

      Very interesting book. One of the interesting tidbits was they figured out that an Orion burning out of *orbit* would result in significant fallout at ground level--enough so that they could estimate the additional number of cancer deaths--and this was one reason among many why the thing never got built. To be safe to Earth-bound life, Orion would have be launched from the Moon (how to build one *on* the Moon is left as an exercise for the reader :).

      --
      -- Cerebus
    18. Re:Can't get to orbit that way by mikeee · · Score: 1

      er, so I did. Let me rephrase:

      Yes, but you could put something much like this rocket as a second stage on top of a big dumb booster and maybe get to orbit that way.

    19. Re:Can't get to orbit that way by powerlord · · Score: 1

      Thanks interesting article.

      The really interesting part was where he talked about building a 'near orbital' SSTO craft as a testbed and learning tool for a true SSTO craft.

      Comparing that to the Blue Origin craft, makes me wonder if they aren't aiming for true SSTO while using sub-orbital space tourism as a way of defraying the development costs (perhaps with suborbital travel as a future business plan?).

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    20. Re:Can't get to orbit that way by Moofie · · Score: 1

      Now you're talkin'. : )

      --
      Why yes, I AM a rocket scientist!
    21. Re:Can't get to orbit that way by powerlord · · Score: 1

      Good point. I stand corrected. I'm just tired of people saying "that can't be done", because they haven't thought of a way to do. :)

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    22. Re:Can't get to orbit that way by Moofie · · Score: 1

      The bottom line is, altitude doesn't really matter that much. The "kinetic energy" you mention is the killer. There is a big, big difference between a sub-orbital shot to a certain altitude, and orbiting at that altitude. All the notions about flying launch platforms only address the altitude problem, not the kinetic energy one.

      Rocket science is kinda funny. It's governed by a fairly straightforward set of equations, and until there's some sort of radical change in the way we accelerate reaction mass, those equations select for a certain sort of solution. SSTO is a tough problem to solve, and vertical landing makes it even tougher.

      Apparently, some really smart people think it will work. I'm a bit of a doubting Thomas, but I'm eager to be proved too pessimistic. I'm still grouchy that VentureStar got canned, because that's a real spaceship! : )

      --
      Why yes, I AM a rocket scientist!
    23. Re:Can't get to orbit that way by powerlord · · Score: 1

      But isn't part of the equation the air resistance that the vehicle has to move through, so wouldn't launching at a higher latitude help minimize that?
      (Of course I bet this is probably negligible relative to the whole equation so I can see where the reduced atmosphere wouldn't make a difference :) )

      I was grouchy over VentureStar getting canned also, thats why I'm somewhat optimistic about this. :)

      This seems like a Corporate take on a similar approach:

            Step 1) Build a test vehicle X

            Step 2) Use the information from X to help build Y, a sub-orbital testbed/passenger vehicle. The use as a passenger vehicle can help underwrite the R&D and maintenance costs (and if you can get sub-orbital flight going well enough, you might be able to make a decent profit as a quick "space-line".

            Step 3) Use the information from Y to help refine what it would take to get SSTO vehicle Z built.

      I realize I'm trivializing a large part of it, mostly through my own ignorance (I am a Software Engineer, not a Rocket Scientist :) ), but it just seems like a plausible progression.

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    24. Re:Can't get to orbit that way by Moofie · · Score: 1

      "But isn't part of the equation the air resistance that the vehicle has to move through"

      That's not accounted for in the simple statement of "The Rocket Equation", but you're absolutely right: Atmospheric drag is significant. Getting out of the atmosphere is a good idea, and that's why SpaceShip 2 and Pegasus and all those systems use an air-breathing carrier aircraft as a first stage.

      That's not a bad idea, by any means, but it's not a panacea. (Few things are.) My off-the-cuff guess would be that a zeppelin-borne high altitude launch platform would make spacecraft integration a challenge. (Problem 1: How do you get the spacecraft to the platform?) Insoluble problem? Certainly not. But a non-trivial problem, certainly.

      The progression you outline is, indeed, precisely what Blue Origin seems to be doing (along with all the other private firms) and they have produced more flying hardware than LMCO did with VentureStar. Heck, Blue Origin is not too terribly far from where DC-X was, and that's quite an accomplishment.

      So, yeah, I'm optimistic. I'm certainly willing to proceed from the assumption that these folks have done a better design study than my back-of-the-napkin one, and they've got what they think to be a good solution. I can't wait to see it.

      --
      Why yes, I AM a rocket scientist!
    25. Re:Can't get to orbit that way by dthx1138 · · Score: 1

      Uhhh.... no.

      Assuming we're talking about the Nuclear Salt Water Rocket, the engine literally ejects the contaminated fuel out the exhaust nozzle. From the wiki on Nuclear Thermal Rocket:

      An alternative liquid-core design, the nuclear salt-water rocket has been proposed by Robert Zubrin. In this design, the working fluid is water, which serves as neutron moderator as well. The nuclear fuel is not retained, drastically simplifying the design. However, by its very design, the rocket would discharge massive quantities of extremely radioactive waste and could only be safely operated well outside the earth's atmosphere and perhaps even entirely outside earth's magnetosphere.

      In other words, it would be like if your local nuclear plant was spraying the surrounding area with heavy water. Not good. Yes, a few km up the exhaust would be spread out over a few km, but how about radius you're affecting from the ground up until then?

      If nuclear rockets are ever to be used on launch vehicles they would definitely have to be a closed-system design.

      --
      I just found the box to change my sig. Um.... [timeless witticism].
    26. Re:Can't get to orbit that way by waveclaw · · Score: 1
      Of all of the possible uses of Nuclear power, using it to power a rocket out of the atmosphere is perhaps the last one I'd want to see actually implemented.


      Let's see:
      1. Throium Nuclear reactor to make the hot parts safer than your car's gasoline engine.
      2. Hydrogen as the reaction mass (yes, you still need reaction mass) so no secondary active radionuclides get made.
      3. ????
      4. Orbit?


      Don't skimp on that hyrdogen, though. The difference between a clean single-to-orbit nuclear spacecraft and a planet-sterilizing cruise missile (non-nuclear link) is in the reaction mass, not the energy source.

      I'm sure it'd be trivial compared to the spread of radioactive particles from coal power plants.


      But people usually worry about that violent cause of death that happens really flashy and to 1% of the population. They tend to focus on labels (NMR anyone?) and ignore that they are dying slooooowly from their McDonald's lunch like most of the 1st world.
      --

      "You cannot have a General Will unless you have shared experiences. You cannot be fair to people you don't know."
    27. Re:Can't get to orbit that way by jandrese · · Score: 1

      The problem is that the ISP from "use nuclear reactions to heat up some other fuel" tends to be too low to be useful. It's a lot easier/safer/cheaper/lighter to just use a reactant that expands on its own (conventional rocket fuel). That's why I specified ground-to-orbit in my post. Once you're in space there are a lot of uses for nuclear propulsion that actually make sense (Nuclear powered Ion drives for instance), but for getting out of the atmosphere you're options are a lot more limited.

      --

      I read the internet for the articles.
    28. Re:Can't get to orbit that way by Jonathan_S · · Score: 1
      was grouchy over VentureStar getting canned also, thats why I'm somewhat optimistic about this. :)
      That's ok, I'm grouchy that VentureStar got the DC-Y canned. (Which actually sounds like you might have been thinking of)

      The DC-X -> DC-Y -> Delta Clipper was exactly the kind of evolving path you described as making sense. And the DC-X part was already built and doing flight testing.

      But NASA picked the super hi-tech, long shot, all or nothing choice of Lockheed's VentureStar over McDonald Douglas's Delta Clipper. And the VentureStar, fairly predictably, was trickier to build and more expensive than forecast and NASA ended up with the "nothing" side of that bet.
  12. Blue Origin Design by amightywind · · Score: 3, Funny

    Powered ascent and descent results in a craft that is 4 times more massive than one that would reach the same altitude but land using a ballistic reentry and a parachute. You would not see Burt Rutan embrace an inefficient design like that.

    --
    an ill wind that blows no good
    1. Re:Blue Origin Design by UtilityFog · · Score: 2, Informative
      It's not that simple. The basic design of the SSTO as a cone-shaped capsule uses ballistic re-entry. The powered landing needs only the delta-V of terminal velocity, not orbital. We're talking on the order of 100 m/s instead of 8000 (probably more like 10k if you account for air resistance on the way up).

      good backgrounder: Harry Stine's Halfway to Anywhere.

    2. Re:Blue Origin Design by FleaPlus · · Score: 1

      Powered ascent and descent results in a craft that is 4 times more massive than one that would reach the same altitude but land using a ballistic reentry and a parachute. You would not see Burt Rutan embrace an inefficient design like that.

      Keep in mind that cost-effectiveness is the goal, not efficiency. Many slashdotters seem to get the two confused with each other. Considering that your main cost is paying employees, which method results in fewer employees to pay? If you use a ballistic landing it tends to be a much harder landing, so you have to spend more on quality control to ensure that your craft is still structurally ok after each landing.

      That said, it looks like the Blue Origin craft will actually use powered descent primarily, with parachute descent as a fail-safe.

    3. Re:Blue Origin Design by amightywind · · Score: 1
      If you use a ballistic landing it tends to be a much harder landing, so you have to spend more on quality control to ensure that your craft is still structurally ok after each landing.

      Parachutes and skids are chosen for spacecraft because they are light and reliable. A stall landing of a craft with a square chute on skids is pretty benign. The DC-X experience (explosion) shows that high thrust landings on retractable legs is a needlessly unreliable and unsafe.

      --
      an ill wind that blows no good
    4. Re:Blue Origin Design by FleaPlus · · Score: 1

      The impression I get is that the failure modes are worse for a controlled landing, but for a "normal" landing a parachute can only slow you down to some minimum velocity, while a powered landing can touch down at an arbitrarily small velocity. This is particularly critical if you want to fly your craft on a daily basis, like Blue Origin probably wants to do.

      Also important for a repeated-flight company like Blue Origin is that a powered landing can touch down at a particular location, while a parachute landing would require some sort of transportation back to the launch site using a truck or helicopter. For a vehicle as big as the New Shephard, I don't think that will be easy to load and transport.

      I could be wrong, but I also suspect that it can be tricky to properly and safely load a parachute of that size.

    5. Re:Blue Origin Design by Moofie · · Score: 2, Insightful

      "but I also suspect that it can be tricky to properly and safely load a parachute of that size."

      It may be tricky, but the math of carrying all that propellant with you is pretty darn inflexible. I've done that math, and I don't know how Blue Origin (and/or Rotary Rocket and/or Armadillo) plans on making it work.

      I'm very, very eager to find out. : )

      --
      Why yes, I AM a rocket scientist!
    6. Re:Blue Origin Design by Media+Withdrawal · · Score: 1

      Powered ascent and descent results in a craft that is 4 times more massive...

      Than what? What alternative are you suggesting for POWERED ASCENT? A giant cannon? Some sort of sky-hook?

      As for descent, keep in mind that even the expendable Soyuz re-entry capsules have landing rockets. If you want a parachute system to be re-usable, you would need either landing gear or a structure and re-entry shield built strong and leak-proof enough to take repeated water landings. That adds mass, too. Parachutes are not enough.

      A LOX-H2 SSTO design such as SSX has an easier time descending than may at first be apparent. It has a low terminal velocity due to its large, empty tanks, and a hovering propellant consumption rate some 25-30x lower than during lift-off (10x because it already burned over 90% of its propellants on ascent, times another 2.5-3x because it only needs to achieve one gee to hover). So a 1-minute hover on landing (already a significant safety factor) adds about as much mass as a 2-second hold-down at launch, which is to say, not much at all. It does need efficient throttling, but I doubt that adds much mass.

  13. It's about time! by Anonymous Coward · · Score: 0

    It's here! My freakin' FLYING CAR, it's here!!

  14. DC-X? by locokamil · · Score: 1

    Like a development of the DC-8?

    If I didn't know better, I'd think they were planning on launching a "new and improved" scientology.

  15. In case you're an aerospace engineer by iamlucky13 · · Score: 4, Interesting

    Correction: In case you're a highly experience aerospace engineer.

    I already checked. They don't seem to be doing a Google style "young talent" hiring search or accepting those with marginally-related experience. If you look through the jobs page, they're generally asking for 10 years experience with some very specific skills (like direct experience with RS-68's or RL-10's). Your chances probably aren't very good if you're looking to break into aerospace, even with an advanced degree. *sigh*

    With good reason, I'd wager. I would attribute a large part of SpaceX's rapid pace of development of the Merlin engines to having recruited the same kind of talent directly off of Lockheed and Boeing. They didn't have to figure out many of the details of how to build a working rocket because they people they hired had already built them.

    This is probably critical for Blue Origin. Space.com's reported that their current test vehicle is powered by catalytically decomposed hydrogen peroxide. If they're going to achieve the payload and altitude they want, suborbital though it may be, I doubt they're going to get there without a bipropellant; fuel + oxidizer. Just switching to H2O2 + kerosene would double the theoretical specific impulse, or energy they can get per mass of fuel. On the downside, burning a bi-propellant increases the complexity of the engine significantly and complicates throttling, and if they're planning on using turbopumps instead of a pressure-fed system (a scheme their jobs page supports), it gets even more complicated.

  16. Next up for Blue Origin by sokoban · · Score: 3, Funny

    Building DC-9 Lookalikes, but with rocket engines in order to transport Thetans to Teegeeack in clusters (packaged by the thousands together), and thereafter drop them in two volcanic areas, one of which is Las Palmas, and the other Hawaii.

    (The preceding joke is based upon the writings of L. Ron Hubbard, which make up a core belief in Scientology (OT III, Incident 2))

    --
    09 F9 11 02 9D 74 E3 5B D8 41 56 C5 63 56 88 C0 is the magic number.
  17. Agreed, but still usefull. by Anonymous Coward · · Score: 0

    The biggest advantange of this type of craft is the fact that you need little to no ground support for launch or landing, and has a quick turn-around time with little to no maintaince between flights. This is most usefull in scenarios where there is no possibility of ground support other than the crew - namely a moon/mars lander.

    Bezos has a decent business plan here. Focus development on recreational sub-orbital flights, which VTL crafts are capable of, and which there is a market for, and in doing so put yourself in a very good position to get a contract from NASA for the new lander that is still up for bid.

  18. Testing VTL control... by bodland · · Score: 2, Insightful

    Vertical Take off and landing. Notice the lack of heat, that is simple escaping gas, notice the lake of "smoke" or product of a oxygen reaction, the liquid and frost?...Some compressed gas propellent in the form of pressurized liquid was used to propel this "pod". Probably a test of the computer controls required to do a vertical landing.

    The pod will probably be deployed atop a conventional rocket to shoot tourists into low earth orbit, take some snaps, puke in zero G then fall to earth, chute deploys then the last 5000 feet or so the landing "spray" take over with non-explosive propellent...for a safe, soft touch down.

    Makes perfect sense, it is safer than splatting craft on the ground like the Russians do, and craft recovery is much cheaper with a soft touch landing than a splash down. Aircraft carriers are expensive.

    I could be way off base...but don't expect any "secret amazing" drive technology out of commercial space vehicles. It is really about making space tourism, safe, repeatable and profitable.

    -=Space Pod=- coming to a Six Flags near you.....

    1. Re:Testing VTL control... by rrohbeck · · Score: 1

      I read somewhere (can't remember where) that they're using H2O2 monopropellant for the demo and will use H2O2/kerosene for the real thing. That's why you only see steam in the demo.

    2. Re:Testing VTL control... by DerekLyons · · Score: 1
      Vertical Take off and landing. Notice the lack of heat, that is simple escaping gas, notice the lake of "smoke" or product of a oxygen reaction, the liquid and frost?...Some compressed gas propellent in the form of pressurized liquid was used to propel this "pod". Probably a test of the computer controls required to do a vertical landing.
       
      The pod will probably be deployed atop a conventional rocket to shoot tourists into low earth orbit, take some snaps, puke in zero G then fall to earth, chute deploys then the last 5000 feet or so the landing "spray" take over with non-explosive propellent...for a safe, soft touch down.
       
      I could be way off base

      You are so far off base that your post contains essentially no relation to reality.
    3. Re:Testing VTL control... by Anonymous Coward · · Score: 0

      I've heard conflicting reports about the current fuel (mono vs bi-propellant), but the more reliable sources (space.com vs. wikipedia) indicate the current capsule uses H2O2 monopropellant. The exhaust would be steam and O2. This is all consistent with the heavy interest in experienced propulsion engineers on their jobs page.

      I suspect, although I have no source for this, that the current engines are also fed fuel by either a pressurized tank or seperately powered pumps, as opposed to a turbopump powered by a small fraction of the fuel itself. This is much simpler, but means significantly increased tank weight. Since they're also looking to hire turbomachinery engineers, you can bet the final engines will be turbopump powered.

  19. Scifi by chord.wav · · Score: 1

    The Goddard has a science-fiction sleekness

    Damn right! The only thing missing from that pick are Tatooine's 2 suns and Luke kicking a rock right next to it.

    1. Re:Scifi by chord.wav · · Score: 1

      pick = pic as in picture

  20. My favortite part of the video... by Anonymous Coward · · Score: 2, Funny

    "10... 9... 8... 7,6..5... 4...... 3, 2... 1"

  21. Oh Please... by Anonymous Coward · · Score: 0

    That's totally fake. If you look close enough you can see the wire from the crane it's suspended from. The sound is just static to make it sound like it's actually doing something.

  22. H2O2 Rocket (s)? by Paracelcus · · Score: 1

    Sure did look like steam coming out of those engines, I thought that hydrogen peroxide just didn't have enough energy for a practical launch vehicle??

    --
    I killed da wabbit -Elmer Fudd
  23. Did they read Fallen Angels? by ibirman · · Score: 1
    This ship sounds suspiciously like the Phoenix from Larry Niven's Fallen Angels. Here is a passage from the book describing it:


    Phoenix stood in the center of the enormous room. It looked like a giant ice cream cone, sixty feet high, standing on its big end. At the slightly rounded base it was half as big across as it was high. It stood alone, with no scaffolding around it.


    The book is available online from the Baen Free Library at: http://www.baen.com/library/

    1. Re:Did they read Fallen Angels? by rrohbeck · · Score: 1

      This ship sounds suspiciously like the Phoenix from Larry Niven's Fallen Angels. No surprise. Larry Niven is part of the Citizen's Advisory Council, who pushed for DC-X style VTVL for a long time. See here.
  24. Would $100billion help? by cheekyboy · · Score: 1

    Look if these guys can do this under say $1billion, then why is nasa wasting 10s of billions or why is the navy/govt wasting 100s of billions in iraq!!!

    Seams like even 5% of the military spending could yield close to star trek technology, ie. 100 space ships with crews of 1000s, and 5 space stations.

    --
    Liberty freedom are no1, not dicks in suits.
  25. Blue Origin Design Confusion by amightywind · · Score: 1
    Than what? What alternative are you suggesting for POWERED ASCENT? A giant cannon? Some sort of sky-hook?

    Jackass. If you purposely misread a simple sentence I can't help you much.

    As for descent, keep in mind that even the expendable Soyuz re-entry capsules have landing rockets.

    Keep in mind that a Soyuz descends under parachute and uses the rocket firing briefly before impact to reduce landing shock. They have nothing to do with the rest of the descent. They stand in place of a landing bag.

    If you want a parachute system to be re-usable, you would need either landing gear or a structure and re-entry shield built strong and leak-proof enough to take repeated water landings. That adds mass, too. Parachutes are not enough.

    Yes, simple skids add a small fraction of the size and mass of the outsized tanks of the Blue Origin. No solution is free. But to most engineers the lighter simpler safer system is preferable. Not suprising Bezos embraced the sexy and discredited alternative

    A LOX-H2 SSTO design such as SSX has an easier time descending than may at first be apparent. It has a low terminal velocity due to its large, empty tanks, and a hovering propellant consumption rate some 25-30x lower than during lift-off (10x because it already burned over 90% of its propellants on ascent, times another 2.5-3x because it only needs to achieve one gee to hover). So a 1-minute hover on landing (already a significant safety factor) adds about as much mass as a 2-second hold-down at launch, which is to say, not much at all. It does need efficient throttling, but I doubt that adds much mass.

    Nice description of the problem, for an English major. Integrate dv = -u dm/m - g dt for the powered descent scenareo and you will see the point. Open any dynamics book to find a discussion of the problem. Also LH2 is utterly wasteful for flight in the atmosphere. High thrust not high Isp is the solution to air drag.

    --
    an ill wind that blows no good
    1. Re:Blue Origin Design Confusion by Media+Withdrawal · · Score: 1

      Heh, you really crack me up. OK, I'll integrate that equation. It's great for parachutes. Perfectly accurate...

      (wait for it...)

      ...on the Moon!