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SpaceX Landing Attempt Video Released

An anonymous reader writes: Last week, SpaceX attempted to land a Falcon 9 rocket on an autonomous ocean platform after successfully launching supplies to the ISS. It didn't work, but Elon Musk said they were close. Now, an amazing video has been recovered from an onboard camera, and it shows just how close it was. You can see the rocket hitting the platform while descending at an angle, then breaking up. Musk said a few days ago that not only do they know what the problem was, but they've already solved it. The rocket's guiding fins require hydraulic fluid to operate. They had enough fluid to operate for 4 minutes, but ran out just prior to landing. Their next launch already carries 50% more hydraulic fluid, so it shouldn't be an issue next time.

248 comments

  1. Wait a minute by Immerman · · Score: 4, Insightful

    It suddenly occurred to me that I've never heard of a hydraulic system "using up" its fluid before. Anyone know anything about how/why the rocket is different?

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    --- Most topics have many sides worth arguing, allow me to take one opposite you.
    1. Re:Wait a minute by Shatrat · · Score: 3, Informative

      Maybe they save weight by not providing a return line?

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    2. Re:Wait a minute by scarpa · · Score: 3, Interesting

      It's an open loop system, presumably to save mass.

    3. Re:Wait a minute by infogulch · · Score: 5, Informative
      His tweet reply to this question answers:

      @alankerlin Hydraulics are usually closed, but that adds mass vs short acting open systems. F9 fins only work for 4 mins. We were ~10% off.

    4. Re:Wait a minute by toonces33 · · Score: 1

      Maybe they were using it as fuel.

      Something isn't adding up here, but it wouldn't have surprised me of the obfuscation filter otherwise known as the media has garbled the message.

    5. Re:Wait a minute by Anonymous Coward · · Score: 5, Informative

      Maybe they save weight by not providing a return line?

      And pumps and motors.

      All they need is a pressure tank.

    6. Re:Wait a minute by Anonymous Coward · · Score: 0

      Google is your friend ...

      they use an open-loop system because its too expensive/heavy/useless to have a full closed-loop hydraulic system with pumps and all on board ... so open-loop it is ... besides, they only use it for 4 to 5 minutes.

    7. Re:Wait a minute by pushing-robot · · Score: 5, Insightful

      Less complexity, less weight (and gets lighter as you use it). No pumps, no power source for pumps, no return lines, just a pressurized tank and a few valves.

      Of course, you have to know how much you'll need before the flight, and the longer you'll need it the lesser the savings over a traditional system.

      --
      How can I believe you when you tell me what I don't want to hear?
    8. Re:Wait a minute by Anonymous Coward · · Score: 2, Informative

      It is lighter and more simple to use up (to expel it when it has done its work) any hydraulic fluid than it is to have a scavenger system. While this would be a problem on your car if each time you pushed the break cylinders it squirt out the fluid after it had actuated the break on a rocket it saves on over all weight and complexity just to have "enough" fluid to do the job

    9. Re:Wait a minute by Anonymous Coward · · Score: 1

      Its an open loop system to save mass due to the extra weight of a hydraulic pump and associated support systems. Instead of a closed loop pump, they use pressure from an onboard tank that pressurises the fuel tank when fuel is removed, and it takes some from that to provide pressure for the hydraulic fluid. But as TFS says, there is a limited amount of hydraulic fluid, and that was the cause of the problem.

      The exciting part is that the Falcon first stage made it to the barge and arrived with a low velocity. It looks like that part is solved. The next one should be a success.

    10. Re:Wait a minute by Anonymous Coward · · Score: 0

      An engine is needed to maintain hydraulic pressure, but the fins operate (for the most part) while the engines are off, meaning it's running out of pressurized fluid.

    11. Re:Wait a minute by Anonymous Coward · · Score: 3, Interesting

      Others are posting about an open system. Besides the loss of the hydraulic fluid which would lighten the load you should also consider that to make a closed loop system it would add mass in the parts and tubes which would be required to contain and create the closed loop.

    12. Re:Wait a minute by patniemeyer · · Score: 4, Informative

      In a normal hydraulic system there is a pump that re-pressurizes and returns the hydraulic fluid to a reservoir. To save weight and complexity here since the hydraulics are only used for a few minutes they instead use an "open" hydraulic system in which the pressure comes from a tank of compressed gas and the hydraulic fluid is expelled or burned up as it is used. (The fluid goes one way - out - as it is used).

      After the pressurized gas or fluid was used up they no longer had control over the fins.

    13. Re:Wait a minute by ItsJustAPseudonym · · Score: 4, Funny

      I'm imagining the Guidance Control Guy at SpaceX watching the hydraulic-fluid gauge with extreme trepidation, as the level sinks toward "E".

      "Elon, I TOLD you we should have pulled over and bought more fluid at the last stop!"

    14. Re:Wait a minute by R3d+M3rcury · · Score: 1

      So what happens to the fluid?

    15. Re:Wait a minute by angel'o'sphere · · Score: 1

      I was about to ask the same, a bit more poorly worded perhaps :D

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    16. Re:Wait a minute by ClickOnThis · · Score: 1

      So what happens to the fluid?

      Presumably, it just gets dumped out of the rocket somewhere.

      --
      If it weren't for deadlines, nothing would be late.
    17. Re:Wait a minute by ganjadude · · Score: 1

      probably pumped out, or if flammable burned off

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    18. Re:Wait a minute by Webmoth · · Score: 2

      Everyone is assuming that the spent fluid is being dumped overboard. Do we know that to be the case?

      It's only necessary to expel the spent fluid externally if you want to reduce overall rocket mass while doing so. If that's not necessary, you can still use an open loop system but have a recovery tank to receive the spent fluid, thereby preventing environmental contamination. That's really the only reason to contain it; the cost of lost spent fluid is probably minimal.

      --
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    19. Re:Wait a minute by kellymcdonald78 · · Score: 4, Insightful

      Falcon uses RP-1 as hydraulic fluid so it is likely burned as fuel

    20. Re:Wait a minute by BreakBad · · Score: 4, Funny

      It is poured on dolphins.

    21. Re:Wait a minute by onepoint · · Score: 2

      Extremely funny, but I bet, that small modification might happen that won't increase the weight issue too much. Lot's of nifty ideas floating around here.

      --
      if you see me, smile and say hello.
    22. Re:Wait a minute by Anonymous Coward · · Score: 0

      It's flammable... so it's to barbyque the baby seals for the after-launch party.

    23. Re:Wait a minute by mspohr · · Score: 2

      A new dimension for "range anxiety".

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    24. Re:Wait a minute by hackertourist · · Score: 3, Informative

      The main hydraulic system on the F9 (for gimbaling the engine nozzles) uses RP-1 (i.e. rocket fuel) as its hydraulic fluid. Spent fluid from that system goes into the fuel tank.
      The fins are driven by a separate system at the top of the stage, if they pumped the spent RP-1 overboard you'd have flammable liquids running down the stage, I'm pretty sure they don't want to do that. Returning the RP-1 to the fuel tank is unlikely (needs an insulated pipe around the outside, next to the cold LOX tank). So probably a separate waste tank near the fins.

    25. Re:Wait a minute by LWATCDR · · Score: 2, Interesting

      I wonder if they are using a pressurized accumulator for the fins instead of a pump. Still a bit odd since the air flow that close to landing should have been next to zero and one would assume that they still had thrust vectoring on the main engine.

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    26. Re:Wait a minute by Anonymous Coward · · Score: 0

      Open loop system, saves weight.

      It's not that much different from some other rockets. The Saturn V's first stage actually used some of its fuel (kerosene) as hydraulic fluid to gimbal the engines, then piped it into the combustion chamber.

    27. Re:Wait a minute by Anonymous Coward · · Score: 0

      Other reason to dump to a recovery tank might just be to minimize the number of external vents on the rocket; more vents = more things that could get contaminated, blocked up, filled with spiders etc.

    28. Re:Wait a minute by DroolTwist · · Score: 1

      If it had a waste tank, the load wouldn't get lighter as it's pumped out, no? So it must either get returned, or burned off somehow. If they were really creative they'd use it to burn an 'X' below the rocket so everyone would know it is a SpaceX rocket returning. Amateurs.

    29. Re:Wait a minute by Anonymous Coward · · Score: 0

      It suddenly occurred to me that you don't know everything apparently... might want to reconsider your Space Nuttery in that light...

    30. Re:Wait a minute by idontgno · · Score: 1

      Maybe the main-engine vectoring used hydraulic actuators? Internal verniers, nozzle steering, engine steering... something has to push it around, and why would you have two actuation systems? If you're too mass-cheap for a closed-loop hydraulics, a complete independent actuator system for thrust steering seems like a bad bargain.

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    31. Re:Wait a minute by idontgno · · Score: 2

      I see later down in this discussion that the engine steering is done with pressurized fuel, which is presumably then dumped into the exhaust stream to burn. And the other actuators are too far from there to make it practical to extend the fuel-based hydraulic system to them.

      Weird set of engineering compromises, but they make sense. Too bad about underestimating the capacity needed for the upper hydraulic reserve.

      --
      Welcome to the Panopticon. Used to be a prison, now it's your home.
    32. Re:Wait a minute by v1 · · Score: 1

      but that means you have to carry more fluid. Unless there's very little fluid normally needed, I don't see how ditching the pumps and motors saved enough weight to put enough additional fluid in the reservoir to matter. I see two lines on a weight graph, a horizontal one for the closed-loop, and a curved line representing the open-loop. At some point these lines cross, and the open-loop becomes a worse option. I'm just surprised that point isn't way earlier for them.

      --
      I work for the Department of Redundancy Department.
    33. Re:Wait a minute by theshowmecanuck · · Score: 1

      Presumably if they manage to make something to go to Mars it will have to be a closed loop system since they won't have a way (or an easy way) to top up many types of consumables. I can see getting the idea of landing with these fins to work, but I would think if they wanted to keep it for a long voyage, they'll have to figure out how to make it closed loop at some time.

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    34. Re:Wait a minute by smaddox · · Score: 2

      An open system is also a whole lot simpler. Weight is very important, but so is reliability. If a pump fails (keep in mind the extreme environment), you lose the stage. Increasing the reservoir size is much simpler and more reliable.

    35. Re: Wait a minute by Anonymous Coward · · Score: 0

      Google the tomahawk cruise missile jet engine. It has open lubrication, it's commonly used, even in some aircraft

    36. Re:Wait a minute by LWATCDR · · Score: 2

      Using fuel for hydraulics is standard practice for rocket and jet engines. It is really a given. Using a pressurized total loss hydraulic system for the fins is... an interesting system.

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    37. Re:Wait a minute by petermgreen · · Score: 1

      I would imagine that anything that goes to mars will either have separate ascent and descent stages or some kind of CO2+energy->fuel conversion setup on the mars surface.

      AIUI the "red dragon" sample return proposal from spacex had an unmanned dragon capsule landing and then a much smaller ascent craft to take the sample to mars orbit (where presumablly it would dock with a craft for return to earth).

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    38. Re:Wait a minute by jcr · · Score: 0, Troll

      That's terrible. They should pour it on PETA members.

      -jcr

      --
      The only title of honor that a tyrant can grant is "Enemy of the State."
    39. Re: Wait a minute by codevalley · · Score: 1

      The hydraulic system used on the main engines uses pressurized fuel fed from the fuel turbo-pump and returned to the low pressure manifold. Thus it is impossible to run out of hydraulic fluid if the engine is running. The grids only operate for a few minutes and mostly when the main engines are off and thus require a separate system. The lightest system is a pressurized tank of hydraulic fluid which in this case was a tad too small. Close but no cigar.

    40. Re: Wait a minute by Anonymous Coward · · Score: 0

      It's fuel, it dumps into the exhaust

    41. Re:Wait a minute by Ol+Olsoc · · Score: 1

      but that means you have to carry more fluid. Unless there's very little fluid normally needed,

      Yup, very little fluid is needed. the weight of the pumps and piping would be a lot more weight added to a rocket that already has the extensible legs on it.

      Despite my initial skepticism, I really think Spacex is gonna make this thing work

      --
      The shepherds did so well protecting the flock that the sheep no longer believed that wolves existed.
    42. Re: Wait a minute by Flyskippy1 · · Score: 1

      More fluid, except that they use fuel (RP-1) as the hydraulic fluid, so after it flows from the high pressure tank through the hydraulic system they can dump it into the main fuel tank to reuse.

    43. Re:Wait a minute by Anonymous Coward · · Score: 0

      It's just like how high end automobiles are always using up their turn signal fluid, which accounts for why one only occasionally sees them signalling a turn or lane change.

    44. Re:Wait a minute by Michael+Woodhams · · Score: 1

      If they couldn't dump to fuel tanks, and if dumping RP-1 overboard was a hazard, surely they'd just use a different fluid? If they're using RP-1 for the fins, I think that is a very strong indication that they're dumping to the fuel tanks.

      --
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    45. Re:Wait a minute by Anonymous Coward · · Score: 0

      F9's Merlin-1D engines use RP-1 as fluid for hydraulics. If that runs out during flight, it is already "game over man".

      But the fins up top have separate tiny and lightweight open system for the 4-min descent. Simple and lightweight being the main criteria.

    46. Re:Wait a minute by Gavagai80 · · Score: 3, Informative

      The first stage of a rocket is never going to Mars, or even to orbit. They may need something different on a third stage of a Mars rocket, but that's no reason not to keep the first stage simple.

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      This space intentionally left blank
    47. Re:Wait a minute by electrosoccertux · · Score: 1

      Using fuel for hydraulics is standard practice for rocket and jet engines. It is really a given. Using a pressurized total loss hydraulic system is... totally normal design.

      fixed that for you

    48. Re:Wait a minute by electrosoccertux · · Score: 1

      Extremely funny, but I bet, that small modification might happen that won't increase the weight issue too much. Lot's of nifty ideas floating around here.

      some of them crash and burn

    49. Re:Wait a minute by Electricity+Likes+Me · · Score: 2

      They landed on the barge is the thing. And not badly either - you can see it come down, and then fall over due to skew angle. The fact it landed anywhere even near the barge is damn amazing.

    50. Re:Wait a minute by hackertourist · · Score: 1

      The point of an open system was not to dump the hydraulic fluid overboard after use, but to not need a pump that can return and reuse the fluid (and a system to power the pump, and fuel for that etc).

    51. Re: Wait a minute by phayes · · Score: 2

      The booster already had 2 hydraulic systems when they discovered that they needed fins to stabilise the booster on descent. RP-1 is used for the engine actuators at the bottom of the booster and a separate open hydraulic system was used at the top using pressurised Nitrogen to assist in Stage separation. The RP-1 hydraulics are active when the engines are active but the fins are needed throughout descent (when the motor is off most of the time) so the upper hydraulic system is used.

      --
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    52. Re:Wait a minute by Anonymous Coward · · Score: 0

      The hydraulic system on a rocket usually consists of a fluid tank and a pressure tank that pressurizes it. One way lines to actuators and used fluid is just dumped. Russians also have systems where fuel straight from turbopump is used that way as long as the main motor is fired you have pressurised hydraulic fluid available. You cant have closed systems without a pump and there are no good ways to power a pump on a rocket. You could have a closed system where turbopump powers the hydraulic pump while main engine is firing and pressure tank pressurizes fluid while power to pump is not available, but due to extra hardware, weight gains from carrying less fluid dont really pay off and complexity penalty makes it really not worth it.

    53. Re:Wait a minute by Rei · · Score: 2

      Yep. From 1300 meters per second to maybe 3 meters per second, with a CEP that would make military ballistics engineers salivate. So, so close.

      --
      It's times like this I wish I had a friend named 'The Professor'.
    54. Re:Wait a minute by phayes · · Score: 2

      Boosters don't need hydraulics just for the engines, they are also needed to assist in stage separation -- at the opposite side of the booster and at a moment when the engines are off & the RP-1 system is no longer actively being pressurised so they almost always use a separate system using a pressurised tank of fluid. When the need for a hydraulic system for fin actuators on descent was discovered (again, when the engine is mostly off & at the opposite side of the booster) it was logical to use it. They just didn't realise how big it needed to be.

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    55. Re:Wait a minute by phayes · · Score: 1

      Falcon has more that one hydraulic system. That the hydraulics used for the engine verniers uses RP-1 says nothing about the separate systems initially used for stage separation & now also for the fins.

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    56. Re:Wait a minute by phayes · · Score: 1

      You mean like the LEM did?

      Except that the LEM didn't & all the hydraulics in both the moon landing's decent & ascent stages were one use.

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    57. Re:Wait a minute by phayes · · Score: 1

      Just about all of them, to tell you the truth...

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    58. Re:Wait a minute by robbak · · Score: 1

      The pressurized fuel used to gimbal the engines is way down at the bottom of the rocket, and the grid fins are at the top. The engines providing that pressure are not running for most of the descent. For these reasons, you need a separate system at the top for these fins, and a simple pressure-activated total loss system would provide everything that they need (or, at least, would have if provided with a few pints more fluid!)

      --
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    59. Re:Wait a minute by cjameshuff · · Score: 1

      It's not just the pumps and piping, they also save having to carry a power source for those pumps, which all adds up to a mass equivalent to quite a lot of fluid. Are you going to stick a big battery pack and electrically powered pump on the rocket? Or maybe use something driven by toxic hydrazine monopropellant? Or ditch the pump entirely and make the fluid reservoir and one of the existing pressurized helium tanks slightly bigger?

      An open system with larger reserves of fluid is also less susceptible to leaks.

    60. Re:Wait a minute by cjameshuff · · Score: 1

      The fluid requirements would depend on how much the fins were actually being moved around during descent. That's something difficult to estimate without ever having actually flown a stage back to the surface under control of the grid fins.

    61. Re:Wait a minute by Luckyo · · Score: 1

      Normal rocket engine uses a turbine to power all systems.

      That is also why Russian engines are considered to be so much better than anyone else's. They have a unique technology that allows them to dump the turbine exhaust into the combustion chamber and gain additional thrust from it (closed circuit rocket engine), where everyone else has to dump the turbine exhaust out of the circuit without gaining any thrust (open circuit rocket engine). Issue is extreme complexity required in closed circuit, which is so difficult to implement that Lockheed Martin engineers did not believe Russians that a working closed circuit engine even existed until Russians test fired one of their engines in Lockheed Martin's own lab.

      In general, in rocketry you have to make a choice between closed circuit systems that are more complex and difficult to implement to work correctly because of extreme system environment and absolutely tiny problem tolerance levels before system suffers a critical failure under load and wasteful but simpler system with less points of failure.

    62. Re:Wait a minute by Luckyo · · Score: 1

      Typically it's flammable and dumped into combustion chamber to be burned off to generate thrust.

    63. Re:Wait a minute by cjameshuff · · Score: 1

      Apart from being at the wrong end of a rather long vehicle, for most of the landing process the turbopumps aren't running. The engines do use RP-1 pressurized by the fuel turbopump for things like the gimbaling hydraulics, but the fins have to work even while the engines are shut down, and so have a separate system.

    64. Re:Wait a minute by lucien86 · · Score: 1

      In a Mars ship (with long term multi-year missions) maybe electric motors might be a better option than hydraulics. Heavier but with better extended reliability (no fluid to run out of), less complexity, -leading to lower overall weight considering maintenance costs. Other alternatives might include - water hydraulics, pneumatics, vacuum pneumatics, even steam..

      --
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    65. Re:Wait a minute by sjames · · Score: 1

      It would also require an actual pump. An open system can use a simple pressure tank to power it.

    66. Re:Wait a minute by K.+S.+Kyosuke · · Score: 1

      Issue is extreme complexity required in closed circuit, which is so difficult to implement that Lockheed Martin engineers did not believe Russians that a working closed circuit engine even existed until Russians test fired one of their engines in Lockheed Martin's own lab.

      This is a popular legend that actually isn't true, the US had had closed cycle engines before the US engineers saw Russian engines (notably the RS-25). The actual problem was that the Russian-style closed cycle works with a high-pressure, high-temperature oxygen-rich mixture, which is a metallurgical challenge. So it's not closed cycle engines in general but oxygen-rich preburner engines in particular.

      --
      Ezekiel 23:20
    67. Re:Wait a minute by K.+S.+Kyosuke · · Score: 1

      They have thrust vectoring, but the fact that the engine thrust (even throttled down) significantly exceeds the terminal stage mass and you only have one landing attempt probably means that the usable range of terminal trajectories is limited (you can't hover and divert the way that the Grasshopper could), and presumably the premature fin failure led to a situation the terminal guidance couldn't deal with. Additionally, the fins allegedly failed in a non-neutral position - in fact, they were in an extreme position. That's like a ship's rudder getting stuck in a "hard left" position. Even with multiple screws, it's still not a nice situation to be in.

      --
      Ezekiel 23:20
    68. Re:Wait a minute by kellymcdonald78 · · Score: 1

      Stage separation on Falcon is not hydraulic (it's electro mechanical), however you are correct there has been no details released on if the grid fins have a separate system or not.

    69. Re:Wait a minute by Luckyo · · Score: 1

      Kindly point me towards evidence of this, as I have seen LM engineers admit to not thinking this engine was possible on camera until they got to test fire it.

      I've heard some rather pointless attempts to pretend that US had something like it, when in reality the only things that come even close are a couple of test projects that have started recently in attempt to reverse-engineer the Russian engine. You suggestion is one of those lame white washing attempts which amounts to "well we have closed circuit system that doesn't work as an engine because it has no meaningful thrust, but we had a closed circuit so we're not 40 years behind, nosiree".

    70. Re:Wait a minute by K.+S.+Kyosuke · · Score: 1

      As I said, RS-25 existed long before that. You've just widened their surprise from oxygen-rich staged combustion to staged combustion in general (RS-25 runs fuel-rich).

      --
      Ezekiel 23:20
    71. Re:Wait a minute by Luckyo · · Score: 1

      Translation: "we had this thing used for low thrust and we'll pretend really, REALLY hard that it's the same thing as first stage high thrust engine".

      Because you know, when you have horses, that's totally the same thing as invention of internal combustion engines because both use burning process to power the movement.

    72. Re:Wait a minute by K.+S.+Kyosuke · · Score: 1

      "Low thrust"? 2.3 meganewtons per nozzle is actually in the same ballpark as all the Russian kerolox engines. The RD-191 has 2.1 meganewtons. There hasn't really been a lot of engines that large. I'm not sure why you're being deliberately obtuse, but if this floats your boat, whatever.

      --
      Ezekiel 23:20
    73. Re:Wait a minute by Luckyo · · Score: 1

      Ditto. You're like those people who suggest that USSR was democratic because it held elections.

    74. Re:Wait a minute by K.+S.+Kyosuke · · Score: 1

      Actually, you're the one being a deliberately obtuse asshole here. You asked for staged combustion engines, I gave you an American staged combustion engine. You claimed it was a "test project with no meaningful thrust", I refuted that by showing that it has a very decent 2.3 MN of thrust in practical use. You argued "but it isn't a first stage engine!" and "it's different from Russian engines", even though neither being a first stage engine nor being a ultra-high thrust engine nor being an oxy-rich engine were any part of your original request, which merely asked for a staged combustion engine.

      It's difficult to argue with people who randomly move the goalposts, but your deficient knowledge of the history of rocketry isn't my problem. You got what you asked for, and I don't have a crystal ball to see any of your further requirements.

      --
      Ezekiel 23:20
    75. Re:Wait a minute by Luckyo · · Score: 1

      And it's impossible to argue with someone who moved the goal posts at the start of the discussion, while remaining in direct conflict with both US and Soviet engineers who worked on the very engines at the time.

      https://www.youtube.com/watch?...

      Those fucking liars. Clearly slashdot used K.S. Kyosuke knows better than relevant people at Aerojet.

    76. Re:Wait a minute by K.+S.+Kyosuke · · Score: 1

      I didn't move the goalposts. I responded to your original claims that "[dumping] the turbine exhaust into the combustion chamber [to] gain additional thrust from it (closed circuit rocket engine)" - which is EXACTLY what the RS-25 from the 1970s does - was allegedly "a unique technology" that "Lockheed Martin engineers" didn't believe was possible. The way your claims were stated, they were simply untrue and ignorant, perhaps aside from the fact that RS-25 indeed got very complex as a result of using this cycle.

      The funny thing is that Russians were to a large extent forced to develop the oxygen-rich cycle hydrocarbon (and even hypergolic) engines because they didn't have the one thing that Americans did - efficient hydrogen/oxygen upper-stage engines (such as the RL-10) which removed a lot of the need for this cycle in the first stage (and perhaps even more importantly, the need to build the complex and expensive ground facilities for this propellant, which Russians did once - for Energia - and then swiftly canceled it for cost reasons). And once they had such engines as the RD-253, they simply learned to manage without high energy upper stages. Now whether getting hydrolox-crazy like Americans are even today was a good idea is highly debatable (Delta IV!), but that's how it ended up. Nowadays even the Angara is going to use the one Russian hydrogen engine that made it into an actual non-doomed vehicle (at least non-doomed yet!), the RD-0146 (which, unsurprisingly, is a redesign of RL-10).

      --
      Ezekiel 23:20
    77. Re:Wait a minute by cwsumner · · Score: 1

      .... I see two lines on a weight graph, a horizontal one for the closed-loop, and a curved line representing the open-loop. At some point these lines cross, and the open-loop becomes a worse option. I'm just surprised that point isn't way earlier for them.

      Um ... I'm pretty sure that they know how to calculate that.

    78. Re:Wait a minute by cwsumner · · Score: 1

      ... The actual problem was that the Russian-style closed cycle works with a high-pressure, high-temperature oxygen-rich mixture, which is a metallurgical challenge. So it's not closed cycle engines in general but oxygen-rich preburner engines in particular.

      I would think so!
      The phrase "high-temperature oxygen-rich" generally means that the engine burns the metal it's made of, as fuel.
      Think cylinder head pitting, in car engines running too lean. Only more so...

    79. Re:Wait a minute by LWATCDR · · Score: 1

      I would have thought that a electro hydro pack like the one that was used on the Cessna 210 would be the solution of choice. Maybe this is lighter and it should probably be more reliable. I have just never seen a total loss pressurized hydraulic system before.

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    80. Re:Wait a minute by robbak · · Score: 1

      Because any electric hydraulic pump is going to be slow at pumping fluid, you still need the pressurized accumulator, so you can move your control surfaces quickly when you need to. So the reservoir, pump and the batteries are an additional weight, that you would want to omit if you could.

      The reason why you have never seen a total loss pressurized system is that the conditions that call for it are ones that you rarely see - a strong mass constraint (which has to include the power source), and a short time period when it is required. Your plane's system needs to operate over a period of many hours, there is normally a power source on hand (the engine's alternator), and the mass is not really that constrained. Really, a rocket is the only place where a pressurized total loss hydraulic system makes sense.

      (Note that this crash could probably have been avoided with more complex programming. The programming could have kept count of how much hydraulic fluid it was using, and driven the fins to neutral before it ran out. This sort of capability - or even just a fluid level sensor - will doubtless be added before the landing system leaves the testing stage. If dealing with early exhaustion of fluid does turn out to be this easy, then the need for the extra mass completely disappears.)

      --
      Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
  2. Why use hydraulic fluid? by PortHaven · · Score: 1

    Seems to me that I would save that for emergencies. Use the high speed descent to pressurize air for controlling.

    Just saying...

    1. Re:Why use hydraulic fluid? by Anonymous Coward · · Score: 0

      Clearly SpaceX can use your expertise. Why aren't you building rockets?

    2. Re:Why use hydraulic fluid? by Anrego · · Score: 1

      I would assume for the same reason they are using an open system rather than a closed system: to save weight and complexity.

      Also, I'm not a space nutter, but this stuff impresses the hell out of me. That looked damn close.

    3. Re:Why use hydraulic fluid? by Immerman · · Score: 1

      So, instead of taking a larger reservoir of hydraulic fluid you recommend they install a secondary pneumatic control system as well, along with an efficiency leeching ramscoop for collecting compressed air? Sounds like a good way to simultaneously increase complexity and reduce payload to me.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
    4. Re:Why use hydraulic fluid? by Em+Adespoton · · Score: 2

      Seems to me that I would save that for emergencies. Use the high speed descent to pressurize air for controlling.

      Just saying...

      Due to the fact that they've only got 4 mins of fluid, I'd say they're already doing that. It's for the low-speed descent to the capture pad that the fluid is needed. Obviously, they cut their margins a bit too close, and so now will be increasing the fluid instead of decreasing the control time. I'm sure they've run the numbers to see if the other way was more viable, as they want as little extra mass as possible.

    5. Re:Why use hydraulic fluid? by OzPeter · · Score: 4, Informative

      Seems to me that I would save that for emergencies. Use the high speed descent to pressurize air for controlling.

      While IANARE, The problem with pressurized air as a control mechanism is that it is elastic/compressible (while hydraulic fluid is basically non-elastic/non-compressible). Which means that if you use air your control is basically going to suck big donkey's balls as your control vanes will bounce around in the airstream as the air in the control system acts like a big spring. Thus degrading the landing accuracy of your rocket.

      On the other hand hydraulic fluid being stiff means that when you send the control vane to a position it stays there, and the only thing that moves it is a leak or destruction of the vane. Note that they will be some bounce in a hydraulic system, but nowhere near as much as in an air based system.

      Now as to the hydraulic fluid in this case being used up, I am guessing that they considered the mass imposed by a collection system and decided, "fuck it, it's too much mass to recycle it, we're just going to dump that shit overboard".

      --
      I am Slashdot. Are you Slashdot as well?
    6. Re:Why use hydraulic fluid? by Anonymous Coward · · Score: 0

      Well, why not electric fins?

    7. Re:Why use hydraulic fluid? by ganjadude · · Score: 1

      electric motors and batteries would be more weight than the hydraulic fluid is my guess

      --
      have you seen my sig? there are many others like it but none that are the same
    8. Re:Why use hydraulic fluid? by 50000BTU_barbecue · · Score: 2

      Don't tell us, tell them!

      http://www.spacex.com/careers/...

      --
      Mostly random stuff.
    9. Re:Why use hydraulic fluid? by Rei · · Score: 1

      I believe what they're saying is instead of any hydraulic system at all, which would be a simplification, no? And I have no idea what you mean by "efficiency leeching ramscoop", the whole point is to slow down.

      I'm sure that SpaceX had reasons for not going with such a design. One that comes to mind for example would be during hover/low speeds - no ram air. But you don't need to be mean to the GP for suggesting that.

      --
      It's times like this I wish I had a friend named 'The Professor'.
    10. Re:Why use hydraulic fluid? by Immerman · · Score: 1

      >Seems to me that I would save that for emergencies.
      Says otherwise.

      And on the return flight you're already going slow - you slow down almost immediately when you hit thicker air at supersonic speeds without actively pushing through it. If you were lucky you might be able to collect enough air at high enough pressure to be useful during the initial slowdown, but at cruising speeds you're probably sunk. Especially since there's no part of the rocket that reliably faces directly into the line of motion, meaning Bernoulli effects will dramatically lower the effective air pressure at the inlet.

      Besides which the air you collect will likely be wet, dirty, possibly ozone-rich, and would then be fed through systems that are absolutely vital to the whole "don't go boom at the landing site" thing, as we've just seen. Probably counterproductive to the goal of high reliability and easy maintenance.

      It is an interesting idea, but I can see why they'd prefer to stick to a nice simple open loop hydraulic system, at least for now - they've got enough other "interesting ideas" to wrestle with already, no sense in borrowing trouble.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
    11. Re:Why use hydraulic fluid? by Rei · · Score: 1

      "Cruising speed" is otherwise known as "terminal velocity" and is hundreds of meters per second. And I'll reiterate: the *point* is to go slow. Drag is a *good thing* on the way back down.

      Other corrections: It's false that there's no part of the rocket that reliably faces a given angle - it doesn't tumble, it maintains an orientation generally between 0 and 15 degrees relative to the direction of travel. And the concept that bloody air is going to kill a pneumatic piston in a matter of minutes is the height of absurdity. .

      --
      It's times like this I wish I had a friend named 'The Professor'.
    12. Re:Why use hydraulic fluid? by Immerman · · Score: 1

      No, the point is to make it all the way back to the launch site using as little fuel as possible because every pound of extra fuel is a pound of wasted payload. Not just yet, granted, but that's the long term goal.

      Well, yes, the "top" of the rocket will always be pointing "forward" to some degree, but I suspect the angle is considerably higher on the return flight when the point is not to travel up as fast as possible, but horizontally as efficiently as possible (though I may well be wrong) - and pressure falls off fairly rapidly with angle. Meanwhile you probably couldn't even get away with putting a scoop on the higher lip where it would face directly into the wind, because I really doubt the control systems are designed to maintain a particular axial orientation - in fact it almost certainly needs the flexibility to NOT do so in order to handle engine failures, and you don't want an engine failure forcing a pneumatic system failure as well.

      I also thought I was quite clear that I wasn't discussing failure during the first flight - this thing is planned for many reuses, and ozone is considerably more corrosive than water. After dozens of flights you start to have to worry about what sorts of problems might have slipped through your rapid-turnaround refit - this isn't like a nail gun where a bit of stickiness at the wrong moment means you have to pull a wonky nail - we've got a multi-million dollar rocket on the line, not to mention the damage that could be done to the spaceport or whatever else happens to be underneath it when the fins jam in place. And what if you should fly through a cloud? That's a LOT of extra water suddenly running through a system that's designed for air, how much are you willing to bet that the control responsiveness changes in response? And heaven help you should you get a bird lodged in the intake.

      Plus the final and probably most important point, which you completely ignored - you're adding an awful lot of complexity for relatively minimal gains.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
  3. Curiously familiar by pushing-robot · · Score: 5, Funny

    Looks like most of my Kerbal Space Program landings.

    --
    How can I believe you when you tell me what I don't want to hear?
    1. Re:Curiously familiar by Loki_1929 · · Score: 3, Insightful

      Based on my experience in Kerbal, they're 95% of where they need to be. They've done the really hard stuff (controlled burns to bring the craft down at the right spot, slowing the descent at the right time without running out of fuel, etc) successfully. Properly orienting the rocket should be relatively easy assuming that the systems responsible for that haven't run out of fuel. The fact that the engine was able to get it that close without the fins working speaks volumes for how well the thing is operating.

      Even if something else goes wrong the next time or two, they'll have a successful landing shortly. The simple fact that it hit the platform ought to be enough to let them start trying on land after another one or two similar attempts. As failures go, this was extremely successful.

      --
      -- "Government is the great fiction through which everybody endeavors to live at the expense of everybody else."
    2. Re:Curiously familiar by Pascoea · · Score: 1

      Yeah, looks like they came in a little hot, and slightly off-kilter.

    3. Re:Curiously familiar by dkman · · Score: 1

      I'm kind of wondering if they could put some arms on the platform to reach out and grab it at that point. I had wondered how they intend to "manage" it once it does land. A big pole on a boat is one wave away from falling over, so they have to have some plan to "strap it down". If they had 4 claws come up from each corner to stabilize it they may have been able to recover from this landing.

      Then your complex part is terrestrial, where it's not offsetting potential payload and easier to maintain.

      I know it sounds simple on paper - the rocket's still moving and you don't want to damage it. But it's worth thinking about. If your claws end in horseshoe-shaped claws and those claws have rollers (so the rocket can move up and down with little friction - think jerking off the rocket if that helps), then those rollers could be locked in place after landing.

      --
      I refuse to sign
    4. Re:Curiously familiar by Anonymous Coward · · Score: 0, Insightful

      The 1960's called and want their moon lander back. Hell, boeing did this in the early 90's on earth. Color me unimpressed.

    5. Re:Curiously familiar by gnite · · Score: 1

      A big pole that has almost all of it's mass at the bottom (engines, remaining fuel). Also, they stated that after landing they're gonna weld some shoes to the platform over Falcon's feet to provide additional stabilization just to make sure.

    6. Re:Curiously familiar by Anonymous Coward · · Score: 1

      >implying that Boeing propulsively recovered a rocket stage after launching something to orbit with it in the 90s

      [citation needed]

    7. Re:Curiously familiar by __aaclcg7560 · · Score: 1

      More like BBQ Kibbles & Bits landings.

    8. Re:Curiously familiar by Anonymous Coward · · Score: 1

      Do you mean the Delta Clipper (or DC-X)? Made by McDonnell Douglas, which never went into orbit and never launched a second stage to orbit and never went higher that 2500 meters?

      Not quite the same thing. I don't remember Boeing ever making such a rocket in the 90s.

    9. Re:Curiously familiar by Anonymous Coward · · Score: 0

      I had wondered how they intend to "manage" it once it does land. A big pole on a boat is one wave away from falling over, so they have to have some plan to "strap it down".

      My guess - and it is only a guess - is that with the 9 rocket engines being so heavy the center of gravity on that stage is VERY low. Especially because above the engines, it's just an empty tube at that point (no fuel).

    10. Re:Curiously familiar by ColaMan · · Score: 5, Insightful

      Firstly, it was considerably easier to do it on the moon. Low orbital speed, 1/6 the gravity, no air resistance on descent, very light lander (as it wasn't pushing 40+tons of second stage to orbit).

      Secondly, this stage was doing Mach 8 to 10 at about 80km altitude when it separated from the second stage. They did an extra burn that briefly popped it out of the atmosphere, reversed its course, then did a hypersonic re-entry tail first and (nearly) landed on a 50x60m barge.

      Nobody has done that before. Not the guys with the shuttle SRB's, they just fell back to earth (and were strong enough to withstand the tumbling in the atmosphere, being SRBs). Not Boeing with it's dinky little hops of 10,000 feet in a continuously-stable attitude at subsonic speeds. Nobody has gotten this far before with the return of the first stage of a liquid-fuelled booster. Seeing as those things are enormously complex and very expensive, it'd be great to get one back in one piece to use again.

      --

      You are in a twisty maze of processor lines, all alike.
      There is a lot of hype here.
    11. Re:Curiously familiar by Andrio · · Score: 1

      Elon did an AMA on reddit last week. Someone asked what software SpaceX uses for their rocket simulations, and Elon responded: "Kerbal!"

      --
      The Internet King? I wonder if he could provide faster nudity.
    12. Re:Curiously familiar by phayes · · Score: 1

      Good guess but the first stage is also 14 stories tall & might tip over if the wind is other than dead calm.

      Elon twitted a while ago that they were planning on welding shoes over the landing legs to stabilise the booster until it reaches port. I assume the they are planning on some longer term system but nothing has filtered out yet.

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    13. Re:Curiously familiar by petermgreen · · Score: 1

      My understanding was that the long term plan was to return most first stages directly to a landing site on land. When they don't have enough fuel to do that they would land it on the barge then partially refuel the stage and fly it back to base. Of course this relies on them managing to convince the powers that be that it's safe to land falcon 9 first stages on land.

      --
      note: i'm known as plugwash most places but i screwd up registering that here somehow in the past and now can't register
    14. Re:Curiously familiar by phayes · · Score: 1

      For the first few boosters recorded intact, they will be bringing the barge back into port with the first stage on it so that they can study them (and not risk losing them). Partial refuelling & then hopping to base is only intended to be a temporary mesure depending on how long it takes for the authorities to accept that a 1st stage recovery area is safe enough for direct descent. If Space-X keeps "soft-landing" the barge, even if they don't recover the first stages, the partial refuel & hop may never become necessary.

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
  4. frist psot by Anonymous Coward · · Score: 0

    In soviet russia, the rocket lands you.

    1. Re:frist psot by colordotmatrix · · Score: 0

      In soviet russia, the rocket lands you.

      Or lands on you...

    2. Re:frist psot by Anonymous Coward · · Score: 0

      Close, but no cigar.

  5. Amazing by netrat · · Score: 1

    I think I've watched the loop 50 times.

  6. We need more... by colordotmatrix · · Score: 0

    Capt'n, I'm givin' ya all we got!!!!!

  7. This test was a successful failure by catchblue22 · · Score: 5, Informative

    This was the first time SpaceX had flown the new grid fin control system on a real first stage under real conditions. They did not know exactly how well the grid fins would behave. As it turned out, the grid fins had to move more than they expected during the descent (or the forces were larger than they expected), so they ran out of hydraulic fluid 30 seconds before landing. This is similar to an airplane losing control of its elevator just before landing. The fact that the rocket reached the barge and that its vertical speed was reasonably slow (certainly not 100m/s) indicates the resiliency of their systems. They are putting 50% more fluid into the system, so this shouldn't happen next time.

    I think this video is epically cool. I can watch it again and again. Simply awesome.

    --
    This and no other is the root from which a tyrant springs; when first he appears as a protector - Plato (423 to 327 BC)
    1. Re:This test was a successful failure by Anrego · · Score: 1

      Indeed. I'm not a space nutter, but this impresses the hell out of me. With a problem this hard, the fact that they are down to minor mistakes like this and not major fundamental issues is awesome.

    2. Re:This test was a successful failure by Anonymous Coward · · Score: 0

      What is a "space nutter", exactly?

    3. Re:This test was a successful failure by Anrego · · Score: 1

      Lots of people find space interesting and are generally supportive of ongoing research and efforts, but generally maintain a healthy balance of other interests.

      Space nuttery is in my opinion defined by an unhealthy and unrealistic obsession with space. These are people who would (or at least have said they would) sell all their worldly possessions for the opportunity to spend some time in space, who would volunteer for a one way trip to mars. Basically a space nutter is someone who spends a fair bit of time flailing their arms and shouting "SPAAACCEEE" excitedly.

    4. Re:This test was a successful failure by Anonymous Coward · · Score: 0

      You keep using that term, though. Judging by your post history, it seems like you have a grudge against space nuttery. Care to share why that might be?

    5. Re:This test was a successful failure by Anrego · · Score: 1

      It's a fairly commonly used term, and I wouldn't really call it a grudge so much as an acknowledgement of the disconnect in reality with those who assume an out of proportion interest in anything involving space.

    6. Re:This test was a successful failure by Dishevel · · Score: 4, Funny
      If you like something less than he does you are a denier.

      If you like it more than he does you are a nutter.

      This is really easy stuff.

      --
      Why is it so hard to only have politicians for a few years, then have them go away?
    7. Re:This test was a successful failure by Bo'Bob'O · · Score: 1

      Interesting that despite running out of fluid 30 seconds before the crash. It still landed in nearly the exact center of the platform. Is it just that it dosn't take much maneuvering even to cover that distance? Or was the platform moving to 'catch' it I wonder?

    8. Re:This test was a successful failure by Anonymous Coward · · Score: 0

      And that's just the Level I Nutters. Wait until you see the ones who seriously think they speak for the "species", or prepare for the asteroid of death, or think we will colonize Mars, or indeed the entire universe.

      At that point, it has nothing to do anymore with reality, science, or engineering; rather, it becomes a religion for self-styled techno-atheists.

    9. Re:This test was a successful failure by Megol · · Score: 1

      Fanatics that think the real world is a sci-fi soap opera. Or at least want it to be.

    10. Re:This test was a successful failure by smaddox · · Score: 1

      I'm guessing the on-board guidance computer prioritizes position over angle. Thus, when the fins stopped controlling the angle of descent, the engine compensated to hit the target position.

      Just a guess, though.

    11. Re:This test was a successful failure by Anonymous Coward · · Score: 0

      "grudge "

      You keep using that term... I can't just have observed a behavior and come up with a name for it?

    12. Re:This test was a successful failure by Anonymous Coward · · Score: 0

      One thing I've noticed about Space Nutters is that they're overwhelmingly software programmer types. In other words, they really don't know anything about physical reality. They assume that progress in Field A automatically means the same progress in Fields B, C, and D.

      They've spent their entire lives gobbling up sci-fi TV, novels, and hanging out with like-minded comic book fans, and spent their time speculating about various doomsday scenarios, sometimes stretching into the billions of years into the future.

      Completely ignoring the fact that evolution is still happening, and therefore no matter what there won't BE a human race in a far shorter time interval than that!

      In other words, they have far more in common with a religion, complete with its doomsday scenario, its criteria for good and bad behavior, and its Promised Land (which apparently is anything but land).

      Pay enough attention, you'll see the same tired old clichés and hackneyed fallacious "arguments" trotted out with monotonous regularity.

      They squeal like vampires in sunlight when you try to understand the origins of their religion.

      http://www.theatlantic.com/tec...

      And facts don't get in their way.

      http://physics.ucsd.edu/do-the...
      http://physics.ucsd.edu/do-the...

      And the more grandiose and improbable their fantasy, the stronger the belief.

      http://physics.ucsd.edu/do-the...

      It's a jejune, failed philosophy from an earlier, naive era and should be buried along with steam locomotives, corsets, and buggy whips.

    13. Re: This test was a successful failure by Anonymous Coward · · Score: 0

      You "anti nutters" might consider looking up some old articles in newspapers quoting some learned individuals stating that traveling more than 50 mph would be fatal to humans (pre locomotive and cars), or that a rocket could never fly in space as it needs something more than a vacuum against which to react (the New York Times, criticizing Robert Goddard).

      It would be useful and educational for you to see what people who think like you were saying back then about stuff in development before you go popping off about what humans will or will not accomplish.

  8. SpaceX II by fustakrakich · · Score: 1

    Now with more fluids! First 3000 customers get an extra half liter!

    You know, there are places where being 'innovative' is not the wisest move.

    --
    “He’s not deformed, he’s just drunk!”
  9. Try Again Next Time by Forgefather · · Score: 5, Insightful

    What gets me most about this is the nonchalant attitude.

    "yea we blew up the rocket and the barge, but no biggie. We'll do better next time"

    I think that is why nerds get so exited over SpaceX. That attitude of not letting fear of failure dictate future actions.

    --
    "There are lies, there are damn lies, and there are statistics"
    1. Re:Try Again Next Time by Hotawa+Hawk-eye · · Score: 4, Informative

      To be fair, the pictures I've seen of the barge indicate it came through mostly unscathed. So they only blew up the rocket. :)

    2. Re:Try Again Next Time by Anrego · · Score: 2

      Gotta agree.

      Business in general has become very risk adverse with a few exceptions (spacex and google being the big ones). Many of us feel constrained in this environment where everything we do has to mostly work or we won't get a second change or an opportunity to improve it. Everything has become about risk management and ROI and soul crushing metrics. It's very refreshing to see this kind of apparent "lets just do something we know probably won't work the first time, and keep doing it until it does" attitude.

    3. Re:Try Again Next Time by Forgefather · · Score: 1

      I just got a look at the vine b/c the site is blocked at my work. My thoughts are:
      It was much closer than I thought, and that must be one tough barge.

      --
      "There are lies, there are damn lies, and there are statistics"
    4. Re:Try Again Next Time by Kjella · · Score: 1

      Well, they usually just let it fall in the ocean so I don't quite see the big risk they're taking here. The rocket will be FUBAR anyway, the barge is basically a bulk metal piece and I assume that if they were looking at a high speed impact they would have fired the engines to avoid significantly damaging/sinking the barge. The money is spend on all the R&D on engine control, fins, legs and whatnot. They got nothing to lose in the actual landing attempt, basically they get a free shot with every rocket they send up that doesn't max out the payload capacity.

      Yeah, going for it is pretty damn tough but once they've committed they can't really pussyfoot around. What I do like is the open attitude though, it's not like a sealed accident report or anything it's SpaceX publishing a video "Hey, look at our rocket blow up!" and it's cool. In fact, I think they might get more appreciation when they do get the landing right than if they'd done it on the first try and made it look easy. Now it's more like it is really hard and if you screw up even a little here's what happens it goes boom. I sure think their PR department knows what they're doing.

      --
      Live today, because you never know what tomorrow brings
    5. Re:Try Again Next Time by Anonymous Coward · · Score: 0

      The nonchalent attitude also gets me -- in a bad way. Their "investigation" (and I use the term loosely) is already complete, they identified what went wrong, and fixed it, all in a matter of days? This means they didn't really do an investigation, involving engineers, analysis, and fault diagnosis. They did an investigation for the cameras.

      The fact what they think went wrong was insufficient hydraulic fluid, and not their engineering process that allowed a major mistake to make it into the design and not be detected during testing, is the *real* problem.

    6. Re:Try Again Next Time by Dishevel · · Score: 2
      Yes, Exactly. They should slow way down and spend a ton of extra money to make sure the next time they do not blow up their disposable rocket.

      Fuck you.

      --
      Why is it so hard to only have politicians for a few years, then have them go away?
    7. Re:Try Again Next Time by EndlessNameless · · Score: 4, Insightful

      The fact what they think went wrong was insufficient hydraulic fluid, and not their engineering process that allowed a major mistake to make it into the design and not be detected during testing, is the *real* problem.

      It was detected during testing. Their entire retrievable/reusable concept is being developed and tested right now. Their contractual requirement is to put payload into orbit. The landing mechanism is merely an economic advantage for the company that will keep their costs lower; their contracts certainly don't specify it as a requirement.

      Some shops use an iterative design process. It usually comes with being new to the market (and thus lacking the funds for extended pre-operative testing).

      Some shops even do iterative design as standard practice when they are well-funded.

      They were only required to launch supplies to the ISS. The ability to test and refine their landing mechanism is a bonus for the company. Hell, NASA's other contractor doesn't even have a reusable vehicle.

      In conclusion: Do you know what we call a service that fulfills its contractual requirements? A success.

      --

      ---
      According to the latest ruleset, this post should be modded as Vorpal Flamebait +5.
    8. Re:Try Again Next Time by Steve+Blake · · Score: 1

      This was the testing silly.

    9. Re:Try Again Next Time by Bo'Bob'O · · Score: 1

      It looks like they lost a hydraulic pump for one of their thrusters from the photos I've seen. So not quite unscathed, that was probably tens of thousands of dollars of damage, but that's chump change if they can make it work.

    10. Re:Try Again Next Time by Bo'Bob'O · · Score: 1

      They don't have stock-holders or congressmen holding the purse strings to try and impress. They don't need to downplay or spin the outcome of a test flight because everyone involved knows that a good testing program will have some failures. And in fact finding new failure modes in early testing is better then not finding them at all.

      So while to SpaceX this was a useful test; their stocks would be falling right now, sending bean counters into a panic were they publicly traded.

    11. Re:Try Again Next Time by Zorpheus · · Score: 1

      It was said before the flight that it is only a 50% chance that the landing works, since a landing like this was not tested before. This was the test.

    12. Re:Try Again Next Time by Anonymous Coward · · Score: 0

      There is such a thing as "paralysis by analysis". I find SpaceX refreshing because they move relatively quickly and have very ambitious goals. That, and they've had an extraordinary amount of success so far.

      Besides, in this case the cause of the problem was pretty simple; they ran out of hydraulic fuel shortly before touchdown. That's a pretty easy and obvious problem to detect and diagnose...

    13. Re:Try Again Next Time by IronChef · · Score: 1

      It's a lot better attitude than they have at my job: "This might not be the most successful thing we've ever done, so we better not even try."

    14. Re:Try Again Next Time by NormalVisual · · Score: 1

      Their "investigation" (and I use the term loosely) is already complete, they identified what went wrong, and fixed it, all in a matter of days?

      I'm guessing they knew what went wrong shortly before the landing when they saw the telemetry indicating they were out of fluid.

      that allowed a major mistake to make it into the design and not be detected during testing

      This *was* detected during testing.

      --
      Please stand clear of the doors, por favor mantenganse alejado de las puertas
    15. Re:Try Again Next Time by Rei · · Score: 1

      Apart from actually launching a rocket to space and then having it descend and attempt to land, what's your proposed method to determine how much the fins have to move during a real-world descent and thus how much hydraulic fluid they'll consume? (beyond the simulations, which SpaceX uses extensively; they're invaluable but don't correspond 100% to real-world flight scenarios)

      --
      It's times like this I wish I had a friend named 'The Professor'.
    16. Re: Try Again Next Time by Anonymous Coward · · Score: 0

      You do realize that one of the distinctive features of the US space program has always been that failures are shown to everybody. That was in sharp contrast with how the Soviets did it in the day. It was quite intentional.

  10. "Amazing video" by Anonymous Coward · · Score: 0

    On vine? Are you fucking serious? It's 7 seconds long.

    1. Re:"Amazing video" by ganjadude · · Score: 2

      doesnt make it any less awesome. I hate vine but hey, in this case its better than no video

      --
      have you seen my sig? there are many others like it but none that are the same
    2. Re:"Amazing video" by Anonymous Coward · · Score: 0

      Yeah but "amazing"? Really?

  11. Fix slashdot! by Carewolf · · Score: 4, Informative

    WTF is going on with the left margin. God damn it, it is broken in every single browser. Are they crapping on classic slashdot to punish us for beta not working?

    1. Re:Fix slashdot! by ihtoit · · Score: 2

      yes. Right bar is fucked as well. Mine ends up at the bottom of the scroll.

      FIX THIS SHIT, DICE!

      --
      Political debates have me rolling my eyes so much I think I got optical whiplash. I should sue. - Foamy The Squirrel
    2. Re:Fix slashdot! by TFlan91 · · Score: 3, Informative

      It's all these damn ads they've added.

      I swear every other week I find a new ad bar, or some ad has moved and margins are all fucked.

      Atleast they keep it interesting...

    3. Re:Fix slashdot! by ganjadude · · Score: 4, Insightful

      you see ads?

      --
      have you seen my sig? there are many others like it but none that are the same
    4. Re:Fix slashdot! by sconeu · · Score: 2

      What are these ads of which you speak? NoScript and AdBlockPlus, and I haven't seen an ad on Slashdot in YEARS.... except for Slashvertisements, of course.

      --
      General Relativity: Space-time tells matter where to go; Matter tells space-time what shape to be.
    5. Re:Fix slashdot! by TFlan91 · · Score: 2

      Only when my disable ads checkbox isnt checked

    6. Re:Fix slashdot! by bondsbw · · Score: 1

      it is broken in every single browser

      Looks fine in Lynx.

      --
      All my liberal friends think I'm a conservative, all my conservative friends think I'm a liberal.
    7. Re:Fix slashdot! by Anonymous Coward · · Score: 1

      I haven't seen an ad on Slashdot in YEARS.... except for Slashvertisements, of course.

      That's what GreaseMonkey is for. I have considered using it for bringing back the OMG PONIES!!!11 theme, but it seems like too much work, especially rewriting all the articles.

  12. Re:How did they run out of fluid? by Em+Adespoton · · Score: 1

    My guess is that fluids encountering massive temperature and pressure shifts can't be reclaimed in the normal way during the flight? Just a guess though.

  13. Better quit from Musk by OzPeter · · Score: 4, Informative

    he tweeted

    Next rocket landing on drone ship in 2 to 3 weeks w way more hydraulic fluid. At least it shd explode for a diff reason.

    --
    I am Slashdot. Are you Slashdot as well?
    1. Re:Better quit from Musk by BreakBad · · Score: 5, Funny

      At least it shd explode for a diff reason.

      Too much hydraulic fluid?

    2. Re:Better quit from Musk by SuperKendall · · Score: 1

      Just like water in nuclear reactors, you can't have too much hydraulic fluid in a rocket landing.

      --
      "There is more worth loving than we have strength to love." - Brian Jay Stanley
    3. Re:Better quit from Musk by lgw · · Score: 1

      Best SNL skit ever. That was Ed Asner, right?

      --
      Socialism: a lie told by totalitarians and believed by fools.
    4. Re:Better quit from Musk by SuperKendall · · Score: 1

      Yes, Ed Asner. Sadly the only online clip I could find of it led to a YouTube entry that had been scrubbed.

      It's come to mind countless times to be over the years, way more than any other skit SNL ever did for some reason. I can tolerate every other crappy thing SNL ever produced or will produce (and that is a LOT) just because that one skit was produced for humanity.

      --
      "There is more worth loving than we have strength to love." - Brian Jay Stanley
    5. Re:Better quit from Musk by stoatwblr · · Score: 1

      Any amount of water in a civil nuclear reactor is "too much water".

      LFTRs ftw.

  14. no more RUDs, then? by ihtoit · · Score: 4, Informative

    To borrow from the KSP forum, that's "Rapid Unscheduled Disassembly". Or, "explosions", to the uninitiated.

    --
    Political debates have me rolling my eyes so much I think I got optical whiplash. I should sue. - Foamy The Squirrel
  15. Re:How did they run out of fluid? by catchblue22 · · Score: 3, Informative

    Hydraulic systems are in a loop, with the "spent" fluid recirculating back to the reservoir. How did they "run out"?

    Where did the fluid go?

    The system is an open hydraulic system. Closed systems require tanks and pumps which carry a mass penalty. They only need the system to function for about 4 minutes. Why bother with a closed system when the functioning period is so short. They will increase the amount of fluid by 50% so this shouldn't happen again. All in all a nearly successful experiment.

    --
    This and no other is the root from which a tyrant springs; when first he appears as a protector - Plato (423 to 327 BC)
  16. Re:You have been challenged statist! by Scottingham · · Score: 1

    Explain your alternative ideology, please.

    What about corporations as large/powerful as states? Are they good or bad?

    --
    Remember, when feeding trolls, be sure to keep your hand flat.

  17. Try Again Next Time by Anonymous Coward · · Score: 0

    They just blew up the rocket. Usually the rocket just falls in the ocean so to see it "almost" land is cool. Next time it just might work!

  18. One thing missing by Anonymous Coward · · Score: 0

    All they needed was a big butterfly net and they had it ;)
    Someone has a robot trained to throw a lasso perhaps?

    Rotate around CG and that looks right on target.

  19. Well Done, SpaceX by Anonymous Coward · · Score: 5, Insightful

    This was the first Falcon 9v1.1 flight [1] with gridfins and [2] sent to land on a teeny tiny little platform at sea (a MUCH smaller target than an aircraft carrier, while descending from MUCH higher than any carrier pilot and having no wings and only VERY limited fuel and throttle-range for lift and control)

    It was an excellent display of competence that puts Boeing and Lockheed-Martin to shame; both mega-corps have been sucking billions from the government nipple for many decades without ever once even TRYING to make such an improvement for which they certainly had the expertise and resources. These giant aerospace companies were born as innovative entrepreneurial entities that invested in technological advances and experiments to advance "the state of the art" in order to win their share of the free market.... but after the deaths of their founders they got hired-gun CEOs and moved to a model of only innovating when they could get the government to give them billions of dollars to do it. With many decades of "cost-plus" contracts (where the government pays "whatever it costs, PLUS some percent as profit") the big bloated defense contractors have had no incentive to innovate (ABSOLUTELY ZERO incentive to reduce costs) and have become lazy. SpaceX and more more like it are needed to drive the big old firms into either returning to efficiency and innovation, or bankruptcy.

    1. Re:Well Done, SpaceX by Anonymous Coward · · Score: 0

      Really? Boeing did a vertical landing in the 90's. I know you weren't alive then, but this is not new. In fact, Grumman built one that did a rocket landing ON THE FUCKING MOON in the 60's, Study your history. Seriously. SpaceX is the first to do with with their own money, but it's been demonstrated decades ago.

    2. Re:Well Done, SpaceX by edremy · · Score: 2
      Really? Boeing returned a first stage booster from an orbital launch to the ground, intact? [Citation please] I've been following the space program since I was born- my first memory is Apollo 11, and I'm pretty sure Boeing has never managed anything like this at all.

      And yes, the LEM managed a landing and ascent. On the moon. With no air. And 1/6th the gravity. And using separate ascent and landing stages- the stage that launched to lunar orbit was *not* recovered intact, and the landing stage was discarded after descent. It's not exactly the same problem.

      --
      "Seven Deadly Sins? I thought it was a to-do list!"
    3. Re:Well Done, SpaceX by Twinbee · · Score: 1

      Is SpaceX's rocket not a dual-stage one then, but only a single stage (no second stage at all) ?

      --
      Why OpalCalc is the best Windows calc
    4. Re: Well Done, SpaceX by Anonymous Coward · · Score: 0

      Yeah, because absolutely NONE of SpaxeX's money comes from the government. Idiot. What the hell do you think this launch was FOR? And who paid for it? They tacked an experiment onto the end of someone else's mission.

      Smart for them because they got someone else to pay for their launch vehicle. Personally I wouldn't have let them do that on a flight with my payload, but as the big bad government space program has ALWAYS done, they put up with it to encourage innovation.

      SpaceX would not exist without the government, and they could not do what they did if others hadn't done other things before them. You free market freaks just don't get that.

      BTW, I am not especially defending the way space programs have traditionally been funded, or meddled with by corrupt congresscritters eager to get pork for districts that are just unsuited to space work. I do guarantee that if SpaceX gets huge contracts and not the relatively tiny stuff they have now that they will be subject to the same pressures though. That's a problem with a harder fix.

      Don't even think about saying "the less government the better, always" at this point because every single massive endeavor in the history of humanity has been directly sponsored by or heavily aided by government. It has to be that way because there's no immediate profit in huge exploration and colonization efforts.

  20. Re: Convenience stores have better video coverage by ColdWetDog · · Score: 1

    Convince stores in the middle of the Atlantic Ocean? At night? In foggy weather? I'm sue we will see other camera views but this isn't capturing pics of some twerp stealing potato chips.

    Further, I don't recall Musk saying anything along the lines that this was about you.

    --
    Faster! Faster! Faster would be better!
  21. Re:You have been challenged statist! by Anonymous Coward · · Score: 0

    I don't think I have presented an alternate idealogy, have I?

    "corporations as large/powerful as states? Are they good or bad?"

    Corporations as large/powerful as states always work in league with the state. And corruption always follows; were it not to then what would be the point of the corporation joining forces with the state?

    And to continue this discussion one needs to note, that it is the state that retains control of the guns, because that is what makes them a state. Meaning, when push comes to shove you don't rreally have a large powerful corporation and a state, you have a state in control of a large corporation, who let's them think they have some degree of power. And what is this other than a different flavor of big government statist tyranny. This is not a good thing, generally, for individual liberty, is it?

    At any rate, you haven't really presented me with an argument for statism/socialism here, all you really did was ask a question, and not a terribly difficult one.

    Calling me a troll doesn't count as a winning argument for socialism.

  22. hey, are you gonna blow that up? can I have it? by Thud457 · · Score: 2

    So they only blew up the rocket.

    Hey, their competitors would have just thrown it away anyway...

    --

    the preceding comment is my own and in no way reflects the opinion of the Joint Chiefs of Staff

    1. Re:hey, are you gonna blow that up? can I have it? by Rei · · Score: 1

      Yeah, it's kind of funny, but with this "failure" SpaceX will still end up recovering more of their first stage than is recovered for 99% of first stages launched in the history of man. Not like any of it will likely be of any use except for analysis and then scrap, but still...

      --
      It's times like this I wish I had a friend named 'The Professor'.
  23. Ford Pinto rocket by Anonymous Coward · · Score: 0

    The thing barely nudged the barge at a slightly wrong angle and blew up. I'm not too convinced that the outcome will be any better even if it touches down upright. Still, props to SpaceX for being the pioneers.

    1. Re:Ford Pinto rocket by Guspaz · · Score: 1

      It has landing legs. When it hits at a 45 degree angle (that's a lot more than "slightly wrong"), the legs on that side break and the engine assembly smashes into the landing pad.

  24. Re:You have been challenged statist! by Anonymous Coward · · Score: 0

    Do you consider socialist anarchy / anarchist socialism impossible, or are you just avoiding that option to be annoying to us "pinko commies"?

    P.S. I won't argue with you, because I'm obviously not a statist. It just seems awfully strange that you automatically associate socialism with statism.

  25. Re:You have been challenged statist! by Anonymous Coward · · Score: 0

    Do you think all people have a right to healthcare? Do you think all people have a right to a minimum wage, and paid days off to boot,

    Why do you think some people shouldn't have a right to healthcare?
    Why do you think some people shouldn't have paid days off?
    Why do you think some people shouldn't have a right to a minimum wage?

    Not like it matters, those are all value judgements and therefore cannot be actual facts.

  26. Re:You have been challenged statist! by Anonymous Coward · · Score: 0

    Socialism is statism.

    Socialism is a political/economic system where ownership or conttrol of property in or is trending towards the collective. Socialism is simply a form of statism. The term statism is preferred because it encompasses all forms of tyrannical systems, not just 'socialism'. Hence, communism, fascism, socialism are all correctly understood to be statist.

    Now if you are happuly not a socialist/statist, perhaps you know someone who you want to send here so they can have reality explained to them by me.

  27. Re:You have been challenged statist! by Anonymous Coward · · Score: 0

    These are not value judgements in any way.

    Healthcare is a service that has to be performed by other men. Healthcare does not well up out of the ground, nor does it grow on trees. Paid days off, in the same way, have to be paid for by someone.

    If you have a right to healthcare, then this means other people must work to provide you this care. Will these other men be paid? Paid for by who? At what rate? What if the provider does not want to work for the rate you agree to, will some agent force them to do this work? (Forcing other men to work? That used to be called slavery!)

    No thing, that requires other men to spend their time or money can ever be a right of another.

    You have the right to free speech. No one has to work or spend money to give you this right.

    You do not have the right to healthcare.

    You do of course have the right to go out, get a job and purchase any healthcare you want. But it is not a right. No matter what the Obama administration tells you, this is not a right.

  28. Re:Convenience stores have better video coverage by niw3 · · Score: 1

    Some low or mid end high speed cameras would be great. With DC lighting during landing. We could see lots of details. I mean, they could.

  29. Re:Convenience stores have better video coverage by Megane · · Score: 2

    The "garbled footage" was a radio signal from the incoming first stage. Getting good communications from a vehicle during re-entry is a hard problem. And a GoPro (at least before this landing attempt) wouldn't have helped much because it would have been on the ocean floor along with the rest of the rocket.

    And in the case of this particular landing attempt, it was before sunrise in heavy fog.

    --
    #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
  30. trial and error by multi+io · · Score: 1

    It seems SpaceX is relying on a trial-and-error strategy during the development of the soft landing capability of their booster much more than they (or others in the industry) do for other components or capabilities of space launch or other aeronautical systems. I don't see (unmanned) rockets or drones being developed in this fashion. Even large rockets that can achieve orbit will normally be modeled, simulated and tested component-wise to the point that they will usually work at the first or second attempt when the entire system is integrated and tested for the first time. So why is this so different here? Is it just cheaper? Or is it actually that much harder to make the rocket land softly on its own exhaust jet than to make it go into orbit?

    1. Re:trial and error by Anonymous Coward · · Score: 0

      Soft landing is a much harder problem than launch. Going up, if you are off by a dozen miles it doesn't matter because you will do an OMS burn anyway. The Apollo program regularly had an engine fail during launch putting them miles off course. They outright didn't care. Coming down, you are trying to find a small target and fall on it gently without tipping over. Backwards. In the wind. In this case, they also had a hard control failure 30s before touchdown, which is usually fatal regardless of vehicle. This was also the first attempt ever to land a VTO first stage.

    2. Re:trial and error by Anonymous Coward · · Score: 0

      >Or is it actually that much harder to make the rocket land softly on its own exhaust jet than to make it go into orbit?

      You have no idea. Getting things up is relatively easy, you lit a big fire and keep the rocket pointing up. Docking to the station is a little bit more precise, but that's nothing compared to making a reentry, restarting the engines, pinpointing a tiny target in the middle of the ocean in bad weather, making it with enough fuel and actually landing upright.

      I know that KSP isn't exactly real life, but it should give you a good idea of the difference. Even the autopilot (MechJeb) in the game, which is by the way a completely deterministic simulation, has trouble making a precise landing at a given target. But it can send pretty much anything with enough boosters and structs into space.

    3. Re:trial and error by Mysticalfruit · · Score: 1

      SpaceX has modeled the hell out of it. It's just really really hard. Honestly, I'd rather they fail in spectacular fashion and explore all the dark corners of their design before they stick people on the top of it. What's great about this is it's all gravy at this point. Once they work all the kinks out, it's going to eviscerate the competition when it comes to cost to orbit per ton. I can only imagine every other commercial launch company must look at SpaceX with a mix of horror and amazement.

      --
      Yes Francis, the world has gone crazy.
    4. Re:trial and error by bledri · · Score: 4, Informative

      It seems SpaceX is relying on a trial-and-error strategy during the development of the soft landing capability of their booster much more than they (or others in the industry) do for other components or capabilities of space launch or other aeronautical systems. I don't see (unmanned) rockets or drones being developed in this fashion. Even large rockets that can achieve orbit will normally be modeled, simulated and tested component-wise to the point that they will usually work at the first or second attempt when the entire system is integrated and tested for the first time. So why is this so different here? Is it just cheaper? Or is it actually that much harder to make the rocket land softly on its own exhaust jet than to make it go into orbit?

      It's important to remember that the primary mission was a complete success. The Dragon delivered the cargo to the ISS and is awaiting trash and cargo to return to Earth. This was a post mission experiment meant to collect data. It's very common to completely loose a rocket in the early flights, but that's not what happened here.

      SpaceX does what's called LEAN development, which is basically like agile software development. Really all development is incremental, the difference with lean/agile is you admit that instead of pretending that you can design the perfect solution from the start. SpaceX has a huge computer cluster and they model the hell out of everything they do. Then they try it to see how it works in the real world, measure the results and make improvements. The experiments are always done after stage separation in a way that collects important data without putting the mission as risk. You can call that trial and error, but that does the process a disservice.

      There have been experimental rockets and landers that land vertically, most notably the DCX. But no one has reentered a first stage of an actual in service rocket, the previous vehicles have always been test platforms and never accelerating to launch vehicle velocities nor going to launch vehicle altitudes. NASA has flown aircraft to collect data from earlier SpaceX missions because no one else has EVER controlled a first stage's return to earth. (Shuttle SRBs were not controlled, just big steel tubes falling from lower and slower than the F9.) The first stage is a long cylinder with blunt ends and it reenters the atmosphere at hypersonic velocities. On top of that, it's a super light weight and fragile airframe. Just getting the thing down to terminal velocity in one piece is a big deal.

      The LEAN development model is less expensive than the classic approach. It's also faster and yields really good results. You learn about problems sooner and don't bake them too deeply into your design. Look at it this way, the closest competitor to SpaceX in developing a reusable VTVL rocket is Blue Origin, started by Jeff Bezos. Blue Origin started with more money than SpaceX and before SpaceX. SpaceX is delivering cargo to the ISS, and about to test the Dragon V2 abort system in preparation of flying astronauts in 2017. They are also self funding the development of a much bigger reusable rocket (slightly bigger than the Saturn V). They are doing all of this while providing the least expensive launch prices in the world. Less expensive than Russia. Meanwhile Blue Origin hasn't even reached orbit. They aren't even trying to reach orbit, they are still developing a suborbital rocket, even though they have a number of experienced engineers that worked on the DCX. Oh, to be fair, Blue Origin is developing an engine for use by ULA (and Blue Origin) and doing some work on a man rated capsule. But nothing is anywhere close to flying.

      --
      Some privacy policy Slashdot.
    5. Re:trial and error by catmistake · · Score: 1

      Soft landing is a much harder problem than launch.

      I don't see what the problem is. Its isn't brain surgery.

  31. I'll take that kind of progress any day. by xeno · · Score: 4, Insightful

    Hey, as these things go, this was a very very good failure. Consider that we've just progressed from the old reality's typical "the vehicle will splash down somewhere in this 500-square-mile area of the ocean," to Spacex's new reality of "we accurately flew down to a 0.0018-square-mile platform, and borked the touchdown on this first try."

    I'll take that kind of progress any day.

    --
    I think not...(*poof*)
  32. Re:You have been challenged statist! by Anonymous Coward · · Score: 0

    And I should add; no where did I say that a person should not have paid days off. I do, and I like them.

    However, this is not a right and for the state to force one man to provide paid days off to another is just another way that the statist pushes wealth redistribution (Marxism) on us.

    As I said, my arguments *cannot* be defeated, I am right, and the statist is wrong every time.

    Now, are there are difficult questions, because these have been pretty easy.

  33. I've got an idea !! by Altesse · · Score: 1

    Seeing this and pondering about this problem, I suddenly came up with a terrific idea, for which I'll file a patent as soon as possible.

    The basic idea, without revealing too much detail, would be to store some sort of very large sheet of tissue, or some other strong fabric, inside a pack or something. The sheet -- which could be duplicated as needed, to improve safety, let's say three of them -- would be neatly folded in order: 1/ to be stored efficiently and 2/ to deploy quickly and as widely as possible.
    At some point in the reentry, let's say a few miles above the landing spot, the sheets would deploy thanks to a system of sorts -- let's say an altimeter -- and, by the magic of fluid mechanics and the Archimedes principle, would slow the rocket enough for it to land safely.

    Now that I think of it, that system could be extended to people, who could jump from an airplane, just for fun or for military operations. Hmmm...

    1. Re:I've got an idea !! by Carnildo · · Score: 2

      Parachutes don't have the accuracy needed to land on a barge, and splashing down in the ocean means complete disassembly to get the residual salt off all the parts.

      The Shuttle SRBs could do parachute recovery with ocean splashdown because they consisted of a small number of very large parts, and needed pressure-washing to get the fuel residue off anyway. Taking a liquid-fuel rocket apart is a much harder task.

      --
      "They redundantly repeated themselves over and over again incessantly without end ad infinitum" -- ibid.
    2. Re:I've got an idea !! by electrosoccertux · · Score: 1

      they often tear at high velocity, and require significant refurbishment after every use

    3. Re:I've got an idea !! by phayes · · Score: 1

      BZZZTTTT! Wrong answer!

      Space-X already looked into and abandoned using parachutes. It's not feasible.

      The reinforcements needed to attach parachutes to an almost empty 1st stage in addition to a parachute big & strong enough to bring a 14 story high object back from near-space at supersonic speeds would add tons & STILL not guarantee a soft enough landing for it to be worth it.

      Got any other brilliant ideas? Maybe lots of balloons to cushion the landing? The spare slip&slide you have in the garden?

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
  34. First Reports vs. Actual Video by __aaclcg7560 · · Score: 1

    The first reports I read said the rocket came down to hard and damaged the platform. I thought it landed vertically by coming in too fast and smashing the platform surface. Watching the video, the rocket landed sideways before exploding. Things always goes badly when they go sideways.

  35. Come clean Mr. Musk by Anonymous Coward · · Score: 0

    ~amightywind was skeptical that Musk had no video of the disaster, and now he has been proven right. What else aren't you showing us Mr. Musk?

  36. Wicked Cool by samwhite_y · · Score: 1

    I personally find this is about as cool as anything I have seen in the last decade. What they are doing requires the very best engineering that mankind currently offers -- I'll take this over building 2000 feet tall buildings, or 50 mile long bridges any day.

  37. Re:Convenience stores have better video coverage by Anonymous Coward · · Score: 0

    Just a few hundred dollars' worth of additional GoPros pre-set at various angles on the landing platform would dramatically increase the quality of coverage.

    The rocket project itself is orders of magnitude more complex than the problem of recording it. It's not asking much and in return they would have a very useful visual record of the landing.

    NASA made proper documentation of the Apollo missions a priority and the world is better off for it.

  38. Re:You have been challenged statist! by firewrought · · Score: 1

    your idealogy is FALSE and that you blindly and sheepishly support a failed system

    All ideologies are false. That's what makes them so tasty. We crave simple rules and easy answers for this complex, interwoven world of ours. And once we subscribe to a set of Answers, we can confidently stride them out upon others... especially those weaker souls who may want to look at an issue from multiple angles and acknowledge the inherent difficulties of society's seemingly numerous and intractable problems. There's nothing better than feeling intellectually invulnerable and knowing that all voices that run in any way counter to your own are automatically corrupt or incompetent, dismissible out of hand without even having to listen to them. The world is so clear when righteousness runs thru your veins.

    Whatever the source--left or right, extremist or complacent-- unchecked ideology is the true enemy of humanity .

    (Yah, I know... don't feed the trolls, but I've been where AC is, and it is a trap unto itself.)

    --
    -1, Too Many Layers Of Abstraction
  39. Re:Convenience stores have better video coverage by Anonymous Coward · · Score: 0

    Did we watch the same footage? The video I saw wasn't from any camera mounted to the rocket, it was from one fixed in the corner of the barge.

  40. Re:You have been challenged statist! by Anonymous Coward · · Score: 0

    You can choose a ready guide
    In some celestial voice
    If you choose not to decide
    You still have made a choice
    --Peart

    Saying all ideologies are false does not make them false. You may not believe in them, this is fine, however your political system is shaped by them and you cannot escape from this. These idealogies exist, and other men believe in them. Idealogy comes from many sources, philosophy, the writings of others etc.

    The idealogy of statism can be distilled to the following (never mind all the altruistic nonsense that exists in Marx that the statist preaches and watch what they do): "We few are going to take from the many because we have the guns".

    Now if you want to assert that this is not true (it is) or that it is a good thing (it is not) then you are welcome to do so.

    That being said, there is nothing wrong with "look at an issue from multiple angles and acknowledge the inherent difficulties of society's seemingly numerous and intractable problems", this is an admirable trait.

    Since you aren't asking a question, I will respond to your saying I am a troll. Not so. I am not trying to distract as such, I am interested in this discussion, and will do as I have stated above. I am only choosing this forum as this is where the population that I am trying to adddress is to be found. I am honestly looking to have this discussion with exactly the people who frequent this forum - the socialist (call it Democrat if that makes it clearer to you) demographic of Slashdot is well known, and I am seeking specifically to avoid political forums.

    Troll? I prefer to think of this as an off topic post, which is what it is. It would be great if this could be posted as a main thread, but I just don't see this happening.

    Anyway, still waiting for those challenging questions...

  41. parachute by kharchenko · · Score: 1

    Remind me again, why doing this crazy rocket landing is better than using a parachute recovery like the shuttle boosters did?

    1. Re:parachute by xfade551 · · Score: 1

      The shuttle's Solid Rocket Boosters always had a bunch of salt water damage that had to be cleaned up and refurbished before being reused, and that refurbishment process costs only slightly less than manufacturing from scratch. The Falcon 9 is a liquid fuel rocket, so that same saltwater has even more things it can damage like pipes and pumps. SpaceX is trying to avoid any major saltwater clean-up, yet still have a place to put the rocket down that's unlikely to hurt anyone when the landing still fails every so often: "Oops, I guess that part was only good for 6 landings, not 7", "Crap, the forecast was wrong! The rocket is now incoming and we got high winds", etc.

    2. Re:parachute by xeno · · Score: 3, Informative

      Because parachute recovery is a method of salvage, while "crazy rocket landing" is a method of full reuse without refurbishment.

      Keep in mind that refurbishing the waterlogged shuttle boosters ended up being 3X more costly than original estimates, much of the nozzle apparatus was completely trashed each time, and the whole process took months to turn around a single booster.

      SpaceX is working toward an airplane/airport-style refuel-and-refly-immediately model. That autonomous landing platform is actually a fuel depot, with the eventual intention to refuel first stages and relaunch them immediately for short hops back to a proper launch facility where they can be fitted with a new payload within a day. Crazy? Maybe. Wrong? I don't think so.

      --
      I think not...(*poof*)
    3. Re:parachute by bledri · · Score: 4, Informative

      Remind me again, why doing this crazy rocket landing is better than using a parachute recovery like the shuttle boosters did?

      SpaceX tried parachute recovery with the F9 v1 (the rocket flying now is the v1.1, though really is more like a version 2). After multiple attempts, they could not get the rocket to survive reentry. There are many reasons for this. First of all, the shuttle boasters were big heavy steal tubes. That's fine for a strap on booster, but not so good for the first stage. Rocket stages are very light weight, since the lighter the rocket the more payload it can carry (this is true for boosters too, but it's a different trade off when coupled to a "first stage".) Second the shuttle boosters separated at lower speed and a lower altitude than the first stage of an F9. So you have a much lighter, complex F9 reentering at much higher velocities. Third, the shuttle boosters were more "refurbished" than reused. The goal of SpaceX is to (ultimately) land the first stage and be able to refuel and relaunch it with a minimum of work. Shuttle boosters had to be fished out of the water, disassembled, cleaned, inspected, etc... SpaceX was hoping to use parachutes as a first step, but they always hoped to eventually land the boosters. Their timeline just got accelerated when uncontrolled reentries kept breaking up.

      --
      Some privacy policy Slashdot.
    4. Re:parachute by nedlohs · · Score: 1

      Crazy?

      Landing your rocket on a fuel depot. Of course not! What could possibly go wrong? :)

    5. Re:parachute by fgodfrey · · Score: 2

      One of the biggest reasons is that, in the location this is happening, parachutes means "lands in the ocean" which implies that your rocket is going to get bathed in salt water, probably engines first. I'm sure you could design some sort of a deployable cover to cover the engines (although they're have to be vented of fuel and cooled first) that would prevent salt water from entering, but I doubt that would be less complex than this scheme and it would almost certainly be heavier.

      Finally, remember that one of Elon Musk's long term goals is to land on Mars (whether he will actually achieve that, I have no idea, but he's heading in the right direction) and for that, parachutes won't work. So, this whole thing is really an R&D program. Even if they "only" recover 50% of the spent stages, that's a lot of "cost of goods sold" to cut out.....

      --
      Go Badgers! -- #include "std/disclaimer.h"
    6. Re:parachute by rocket+rancher · · Score: 1

      Keep in mind that refurbishing the waterlogged shuttle boosters ended up being 3X more costly than original estimates, much of the nozzle apparatus was completely trashed each time, and the whole process took months to turn around a single booster.

      "ended up being 3X more costly..." you make it sound like the prime contractor didn't know this all along. When you land a cost-plus contract with the government (or anybody, for that matter) your job suddenly becomes to make the contract as costly as possible while still appearing to be executing due diligence. This is why Lockheed, Raytheon, Boeing, and the other contractors have been able to hoover up hundreds of billions of taxpayer dollars, with only the lame and inefficient STS to show for it. For the amount of taxpayer dollars diverted to the US space program starting with the boondoggle Apollo program PR stunt (yes it was PR. It was all fuck the Russians and their fucking sputnik, we have to one-up the commie bastards by going to the goddamn moon) we could have fixed our social safety net and cured poverty, and put money into useful areas of research, like medicine and energy production/distribution, and fixed our broken education and healthcare systems. Instead, we created a whole new class of welfare client, the aerospace/defense contractor, and managed to keep the Cold War going for 40 more years. Why do you think Tea Party darling Ted Cruz is now the gatekeeper for the US Government's science and technology funding? It's because Musk proved that you don't need a huge fucking corporate welfare system to support basic research. There is also the added political bonus of Musk's achievement discrediting every dollar the US government spent on "space research." One of Cruz's direct responsibilities is overseeing NASA funding, and it is going to be next to impossible to fight his budget cuts when all Cruz has to do is point to Elon Musk's SpaceX success. The Tea Party wing of the GOP is going to be insufferable for a long, long time....

    7. Re:parachute by Anonymous Coward · · Score: 0

      "First of all, the shuttle boasters [sic] were big heavy steal [sic] tubes. That's fine for a strap on booster, but not so good for the first stage."

      SRBs *are* the Shuttle's first stage.

  42. Re:You have been challenged statist! by cmdr_klarg · · Score: 1

    Or hide in your anonymity and know you are a coward

    Quite the bluster from an Anonymous Coward.

    --
    THE SOFTWARE, IT NO WORKY!!!
  43. Am I missing something? by Anonymous Coward · · Score: 0

    I watched the video and I can't understand how this rocket could be reused? I mean even if it hit the target it looks like it still would have broke apart significantly.
    My impression was I guess a more controlled landing, not a controlled crash.

    1. Re:Am I missing something? by 0123456 · · Score: 1

      It's supposed to land like this:

      https://www.youtube.com/watch?...

      You know, vertical and stuff.

  44. Re: Convenience stores have better video coverage by Anonymous Coward · · Score: 0

    I don't recall me saying it was about me, either.

    Your points are irrelevant. Neither the Atlantic-ness nor the night-timeness nor the fogginess had anything to do with the poor quality of the coverage. The coverage was poor because it was taken from a single, not-great position and the camera was aimed mainly at the deck. This could be solved with a handful of additional cameras.

  45. Re:You have been challenged statist! by Anonymous Coward · · Score: 0

    No not bluster, I mean this literally.

    Socialism consists of taking from those that produce in society, keeping most of the money in the hands of the ruling elite, and giving some amount of this money back to those in society that do not produce. This money is taken by means of violence - that is to say if you do not give your money to the state they will put you in jail, and if you resist you will eventually be forced to do so by men with guns (and this is observable fact, of course).

    This is theft, it cannot be described any other way.

    I don't much care for people who steal my money.

    And like I said, my arguments cannot be defeated. Go ahead and try. If you cannot justify and rationalize your support of socialism, then you are just a common thief, and a coward. (Not that you specifically stated this is your position, I am speaking in the general).

  46. Open hydraulic Systems are Common in Rockets by Anonymous Coward · · Score: 0

    open hydraulic systems are common in rockets ; very light weight but limited in usage time

  47. Re:How did they run out of fluid? by drinkypoo · · Score: 1

    Closed systems require tanks and pumps which carry a mass penalty.

    Strictly speaking, you don't need multiple reservoirs for a closed hydraulic system. You only need one, and that reservoir can be your accumulator. In practice we usually have at least two; one is the accumulator, and one of them permits degassing the fluid which can be necessary as it heats up. With an open system you definitely only need the accumulator, and some kind of control valve. On a spacecraft, hopefully you also have a backup. A shuttle valve is one valve that lets you pump fluid in (or from) multiple directions, usually two of them, and which you can run with a servo (or however) to get variable control over hydraulic flow. Most hydraulic systems with a pump also need a pressure relief valve, which is a common point of failure. Sometimes they just have a pressure switch, which is another common point of failure.

    On a car, the power steering system has a reservoir with degassing typically attached to the pump, but sometimes nearby. The shock absorbers are a closed system, but [typically] use a nitrogen-charged diaphragm to handle the fact that the interior volume of the shock changes; both as the shaft enters the body of the shock, and as the working fluid heats up.

    Anyone out there know the specific layout of the control system for each vane? I'd imagine that the fluid is going to the cylinders and then to the control systems and on to the waste ports, but that's where my imagination ran out since I'm not a rocket scientist nor do I play one on teevee

    --
    "You're right," Fisheye says. "I should have set it on 'whip' or 'chop.'"
  48. Radio coverage by nojayuk · · Score: 2

    The problem with blackout during a hot re-entry from orbit is plasma from the heatshield or tiles (in the case of the Shuttle) blocking radio signals at Mach 20 or so (about 6 km/second or thereabouts). This wasn't the case of the Falcon first stages as they were never going fast enough in the atmosphere to produce any plasma. If any of them had then the bottom of the stage would have melted since it's mostly lightweight low-melting-point alloys. Those sorts of temps would also have damaged a lot of the motors, the actuators, the guide fins etc.

    As for the accuracy thing, again it was not a re-entry from orbit and the stage had guidance systems to bring it down to the barge, much as the Shuttle never had a problem finding the runway and painting the centreline during its landings. What puzzled me more was the speed at which the stage hit the barge. It should have been a lot slower, even with the failure of the guidance fins.

    1. Re:Radio coverage by 0123456 · · Score: 1

      What puzzled me more was the speed at which the stage hit the barge. It should have been a lot slower, even with the failure of the guidance fins.

      It was coming down tipped over at 45 degrees, using much of the thrust for trajectory correction when it should have been used for slowing down for landing. So I'm not surprised it hit hard.

    2. Re:Radio coverage by Amazing+Proton+Boy · · Score: 1

      There are no significant aerodynamic forces on the fins at this very low speed either. We aren't getting the whole story. I suspect an instability caused a feedback loop.

  49. Think of it as evolution in action by Bruce+Perens · · Score: 1

    Think of it as evolution in action. You can stay on one planet while some disaster takes it out. We have lots of choices of disaster, don't we? The human race can continue via those "space nutters".

    Sure, we should try to avoid the disaster, etc., but planets are not forever.

    1. Re:Think of it as evolution in action by Anonymous Coward · · Score: 0

      And here we go, the tiresome Space Nutter religious hymns trotted out again.

      "but planets are not forever."

      Neither is your body, yet I don't see anything near the fervor and knee-jerk fanaticism for life extension.

      Is that because there was a show called Star Trek, but not one called Life Trek?

      You religious atheists are mystifying to me...

  50. Re:You have been challenged statist! by lgw · · Score: 1

    You can choose a ready guide
    In some celestial voice
    If you choose not to decide
    You still have made a choice
    --Peart

    They sang that lyric, but the printed lyric books read "You cannot have made a choice". I've always loved the fact that they described agnosticism both ways.

    --
    Socialism: a lie told by totalitarians and believed by fools.
  51. Re:You have been challenged statist! by DamnStupidElf · · Score: 2

    I dunno, I'm happy enough with my voluntary free association with the United States. I'm free to leave if I stop liking it, as are you.

    What anti-state people don't seem to grasp is that the very same people who you hate in the government, the people who want to control your life and take things from you, weren't made that way by big government. Just look at Mexico. Big drug cartels (who may or may not be entirely the creation of anti-drug big government) are more powerful than the government. Wherever there is an advantage to be had by banding together and robbing the weaker or more honest people, you'll find that niche being filled. The job of government is to fill that niche with the least harmful and most inept robbers. That overpaid, uncooperative, unfriendly civil servant that you despite? Give them a gun and a posse and see how well that turns out for you.

  52. Isn't this too complicated? by eexaa · · Score: 2

    I mean, If it's already slowed down like this, why not just gently land the rocket into the ocean and take it up with some prepared nets/ropes? IMHO it can save a lot of headache from trying to hit a platform this small.

    If the water getting in the rocket is problem, what about a gigantic sheet of plastic on the water surface? (still cheaper and more reliable than hitting the landing pad).

    1. Re:Isn't this too complicated? by Anonymous Coward · · Score: 0

      GPS makes hitting the platform pretty easy. Doing it gently in a controlled attitude is the hard part.

  53. Hard Landing by Dereck1701 · · Score: 1

    Wow, when Musk said that it was a "hard landing" I thought he may have been exaggerating, he wasn't. Though it was VERY close. If I'm not mistaken the rocket is oriented pretty well (though is off the landing pad) just before it suddenly goes 45 degrees (presumably in an attempt to get to the barge) and slams into the deck. A larger pad would definitely help, but they may be able to tweak the navigation software to make it work.

  54. Fins went hard-over when the system ran dry. by robbak · · Score: 3, Interesting

    Elon stated while being questioned last week that the steering fins went hard-over (which means they were driven to their maximum angle) when the fluid ran out. With the fins pushing the rocket over, it didn't have much hope of landing. And, yes, a pressurized accumulator is the most likely design of this system.

    /u/DixieAlpha over at reddit programmed a Kerbal Space Program model to try to land with grid fins fixed at 30 degrees. The results were scarily similar to this landing.

    --
    Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
  55. Investigation was over ~20 seconds before landing. by robbak · · Score: 1

    The fact that the next launch was already going to carry 50% more fluid indicates that they had an idea that there might not have been enough. That decision about how much fluid was needed would have been made early on, and they could not have fixed it later, as this secondary experiment could not be allowed to interfere with the primary mission.

    The engineers monitoring the landing would have seen the fins be driven to hardover and known instantly that they'd run out of fluid (if they didn't have a sensor for that). Elon tweeted that they'd run out of hydraulic fluid within hours of impact.

    As others have stated, this was testing anyway.

    --
    Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
  56. Do stores take pictures of rocket engines in fog? by robbak · · Score: 1

    The initial reason for not releasing video was that it was dark and foggy, and the video was not fit to release. While this may have been more about controlling the news cycle by forcing the media to use pictures of the successful launch, it is clear that this video required a lot of levels adjustment to make it acceptable, and that has created noise in the image. However, apart from the drops of water on the lens, which is unavoidable, the quality is quite good.

    --
    Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
  57. Re: Convenience stores have better video coverage by robbak · · Score: 1

    Those handful of cameras were either toasted, or the images were washed out by the glare and the mist. There were a good many cameras on the barge, in various places.

    --
    Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
  58. Solid boosters vs. liquid rockets. by robbak · · Score: 1

    Solid booster casings are a very different beast. A solid booster rocket needs to be very strong, because the combustion chamber of a SRB is literally the entire rocket. The whole thing needs to withstand combustion chamber pressure. So it is strong, tough (and heavy), so you can do what you like with it.

    A liquid fuel rocket is a much more fragile beast. If allowed to tumble through the atmosphere, or hit the water at parachute speeds, it would be totally destroyed.

    --
    Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
  59. Bingo fuel means no brakes, no manuevering by rocket+rancher · · Score: 1

    They are using fuel as hydraulic fluid, an old and (apparently) still stupid idea. The SR-71 used JP-6 as fuel and hydraulic fluid -- one Habu pilot told me, "yeah, dumb engineering decision. If you are on bingo fuel, you might as well plan for a ditch, because bingo also means you are out of brakes and maneuvering." That was 35+ years ago. You'd think Elon would have covered that base.

    1. Re:Bingo fuel means no brakes, no manuevering by cjameshuff · · Score: 1

      They only use fuel as hydraulic fluid for the engines, the fins use a different system that has to operate when the engines (and the turbopumps pressurizing the fuel) are shut down. If you're out of fuel, you don't need to gimbal the engines. And it was rather clearly not out of fuel, considering the big plume of fire coming out of the bottom of the rocket.

  60. The problem was the control fins. by robbak · · Score: 1

    The fault that caused this failure was the control fins running out of pressurized hydraulic fluid. When this happened, they were driven fully to one side, pushing the rocket over. The engine tried it's best to counter that, but it didn't have a hope.

    A fellow fan tried something similar in the Kerbal Space Simulator. I imagine the real flight was very much like this:

    http://gfycat.com/PointedWhisp...

    --
    Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
    1. Re:The problem was the control fins. by Dereck1701 · · Score: 1

      The grid fins may have contributed to the booster being off course from the pad but I have a hard time believing that they would have caused such an (apparently) abrupt change of orientation. Such control surfaces usually only function significantly at high speed, not at the slow speeds at landing. Think about it like putting your hand out of a car window, at 25 mph nothing happens, when you get up to 45 you get a little bit of push, but its only at 55+ when you can really have an effect.

    2. Re:The problem was the control fins. by robbak · · Score: 1

      The rocket decelerates quickly during quite a short landing burn, so they would have had a strong effect until the last few seconds. Indeed, the loss of that force as the rocket comes to a stop would have been an important part of the crash - the rocket would have been countering the influence of the grid fins pushing the top of the rocket away from the camera, while tilting the rocket toward the camera to get it back to the platform. Then the rocket slows and that force dies away. Now the rocket has to go from working hard forcing the rocket to tilt toward us against that force, to trying to push it back upright with that force suddenly gone. You can see that it was trying, because the rocket flame is directed away from us, illuminating the far side of the rocket, leaving the near side in darkness.

      Nope. Grid fins explain what we see very well.

      --
      Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
  61. Re: You have been challenged statist! by Anonymous Coward · · Score: 0

    I can say I don't necessarily agree with everything you just said, but it was so refreshing to read compared to the libertarian claptrap will usually get around here.

  62. Almost by BobSteinVisiBone · · Score: 1

    Sure, that looks almost fixed. Kind of in the way PayPal is almost e-money.

    --
    Bob Stein, http://bobste.in
  63. "More unlikely than likely" by cbeaudry · · Score: 1

    48% confidence that 2014 is the warmest year on record. (Straight from the 2014 NOAA state of climate report)

    Warmest year on record, by 0.04C with an error margin of 0.09C (Seriously?)

    http://wattsupwiththat.com/201...

  64. Ok jerk, by Anonymous Coward · · Score: 0

    1. I was alive for the moon landing. I was actually IN THE VAB during a Saturn V stacking... so NO, the DC-X did not pre-date me... and, BTW, the DC-X NEVER went over a few thousand feet up, NEVER even went supersonic, NEVER carried a payload (Falcon lofted a second stage AND payload out of the atmosphere) and had a huge area of (stable and fixed) desert to land on.

    2. Yeah, Grumman did an excellent job on the Apollo LEMs (COMPLETELY on a cost-plus government dime), but several important caveats:

    2a. Every LEM was flown by a test pilot CDR, aided by a flight engineer (mis-named LMP (Lunar Module Pilot))

    2b. The LEMs all landed vertically on the MOON, therefore: NO atmospheric effects like wind and transonic shock waves, only 1/6th gravity, MILES of landing fixed and stable area (not a rolling and pitching barge at sea)

    2c. As soon as government stopped shovelling the dollars, Grumman stopped innovating.

    So, NO, you only THINK it's been done before because you are not as informed as you think you are.

    I am NOT a typical twenty-something SpaceX fanboy who thinks Musk can do no wrong and will deliver utopia while being totally ignorant of history. It's precisely because I know the history, was there to see much of what is significant to this discussion, and value the classical "free market" and the benefits of competition that I was willing to say "Well Done" the the Hawthorne team.

    Footnote: one thing that makes my earlier points even further is that even the SpaceX main facility in Hawthorne USED TO BE a Boeing facility.... again: the "big boys" had EVERYTHING to do this but simply chose NOT TO over the past decades for a very simple reason: "cost-plus" contracts. With cost-plus contracts, vendors are actually DE-INCENTIVISED to improve and lower costs because their "plus" part would SHRINK since it is calculated as a percentage of a base amount that would be reduced.