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SpaceX Rocket Launch Succeeds, But Landing Test Doesn't

New submitter 0x2A writes: A Falcon 9 rocket built by SpaceX successfully launched a Dragon cargo ship toward the International Space Station early Saturday— and then returned to Earth, apparently impacting its target ocean platform during a landing test in the Atlantic.

"Rocket made it to drone spaceport ship, but landed hard. Close, but no cigar this time. Bodes well for the future tho," Elon Musk tweeted shortly after the launch. He added that they didn't get good video of the landing attempt, so they'll be piecing it together using telemetry and debris. "Ship itself is fine. Some of the support equipment on the deck will need to be replaced."

213 comments

  1. No good video? by amightywind · · Score: 1, Insightful

    No good video? In the era of rocket cam? He should say, no video he wishes to show. Elon Musk is a master propagandist.

    --
    an ill wind that blows no good
    1. Re:No good video? by rHBa · · Score: 4, Informative

      According to Elon "Didn't get good landing/impact video. Pitch dark and foggy."

    2. Re: No good video? by Dan+East · · Score: 5, Informative

      Another news story said it was foggy and zero visibility. The cameras on the rocket really only showed anything when it fell over into the water, where bubbles could be seen.

      Considering spaceX has navigated the rocket exactly where they wanted every landing attempt, I wonder when they will finally get permission to land on, um, actual land. For all we know the ship may have pitched up increasing the velocity that the rocket touched down. Plus I'm sure the poor visibility at sea couldn't have helped either.

      --
      Better known as 318230.
    3. Re:No good video? by Anonymous Coward · · Score: 0

      Riiiight. It's not like we have cameras that can film in the dark and through fog or anything. Oh wait...

    4. Re: No good video? by EnsilZah · · Score: 4, Informative

      The bubbles you're probably referring to were from a camera inside the liquid oxygen tank of the second stage.

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

    5. Re: No good video? by Kjella · · Score: 2

      Considering spaceX has navigated the rocket exactly where they wanted every landing attempt, I wonder when they will finally get permission to land on, um, actual land. For all we know the ship may have pitched up increasing the velocity that the rocket touched down. Plus I'm sure the poor visibility at sea couldn't have helped either.

      Unless there was a huge storm in the area I doubt a 300'x170' barge has much of a pitch and in that case the rocket would probably be much worse off than the barge. And the telemetry shouldn't be much affected by dark and fog, just the cameras. To compare with airplanes I understand category IIIb airports are fairly routine now which means zero visibility landing, 150 feet runway visibility range. And that's basically just so they won't bump into each other while taxiing, zero RVR is possible but would require lots of instruments from runway to the gate and in most whiteout conditions you wouldn't want to be flying anyway because of the winds, not the visibility.

      --
      Live today, because you never know what tomorrow brings
    6. Re: No good video? by Rei · · Score: 1

      All we can say is, if the ship is fine, just some equipment damaged on deck, then this was a very low speed impact. Sounds more like the rocket falling over than anything else. Why? Not a clue. But I guess we'll find out. Maybe Musk's plan of "have it weigh itself down and then we'll weld it to the deck afterwards" wasn't a good one.

      --
      It's times like this I wish I had a friend named 'The Professor'.
    7. Re:No good video? by Anrego · · Score: 1

      I can just imagine what a rocket looks like on IR.

      I'm going to assume either all white or all black, depending on polarity settings.

    8. Re: No good video? by Anonymous Coward · · Score: 0

      I'm north of Orlando and got to watch the launch from my outside my front door. I saw the first stage reentry burn. It was cool looking.

      The rocket flew northeast so I think the barge/platform was a ways out from Jacksonville. The weather report is saying 4-8 foot seas in that area at the time. I imagine that computer-controlled landing of a rocket on a barge that's bouncing up and down 8 feet, in the dark, could be a bit tricky.

    9. Re: No good video? by onepoint · · Score: 1

      300 x 170 is a real bad ratio, it's going to be a sloppy ride. A good stable ratio is in the 30 x 5 x 3 ( L x W X H ). I got to assume he knows something or the barge design is amazingly special
      dry bulk cargo barges are about 195' x 35' ( which is near the 6 x 1 ratio ) https://en.wikipedia.org/wiki/...

      --
      if you see me, smile and say hello.
    10. Re: No good video? by angel'o'sphere · · Score: 1

      300 x 170 is a real bad ratio
      Why do you consider the ration 'bad'? IMHO the ratio does not matter at all, the barge only needs to be big enough to provide the landing space and what ever else they need on it.

      --
      Cost free eBook I read (by iBook/Kobo/Amazon/ObookO/Gutenberg etc.): "The Green Odyssey" by Philip Jose Farmer.
    11. Re: No good video? by onepoint · · Score: 1

      >>
      Why do you consider the ration 'bad'? IMHO the ratio does not matter at all, the barge only needs to be big enough to provide the landing space and what ever else they need on it.

      Vessel stability on all 3 axis, I would guess that something like this needs a really good stable landing platform. It's not easy to keep a platform at the required location. I am going to take a guess that they tested everything to the extreem and this is what they came up with.

      but the most likely size should have been near 1000 x 170, which now writing it, is super huge, just having a hard time picturing 170 feet in width. and the dimentions ... here is a container ship that would be near the dimentions and I can see clearer now https://en.wikipedia.org/wiki/...

      that landing platform would cost a fortune.

      --
      if you see me, smile and say hello.
    12. Re: No good video? by Rei · · Score: 1

      First off, where did you get the impression that Musk said anything like that? Secondly, where did you get the impression that the person you're replying to said anything like that? They never said "land at the same place".

      --
      It's times like this I wish I had a friend named 'The Professor'.
    13. Re: No good video? by rainmaestro · · Score: 1

      The larger the frontal surface area of the vessel, the harder it is to control. Wave motion and tidal forces become more pronounced as the vessel gets wider, making it harder to hold position.

      This "barge" isn't a standard cargo hauler, though. You can see a photo of it at the link below. It was definitely custom-built for this purpose.
      http://www.spacex.com/sites/sp...

    14. Re: No good video? by Kjella · · Score: 1

      300 x 170 is a real bad ratio, it's going to be a sloppy ride. A good stable ratio is in the 30 x 5 x 3 ( L x W X H ). I got to assume he knows something or the barge design is amazingly special
      dry bulk cargo barges are about 195' x 35' ( which is near the 6 x 1 ratio )

      I have no idea what you're hinting at, a few quick searches indicate that the narrower beam (width) the less stable it gets. The shape of your average barge seems more about being able to traverse waterways and efficient loading/unloading at docks, for optimal stability it should probably be square with as low a center of gravity as possible.

      --
      Live today, because you never know what tomorrow brings
    15. Re: No good video? by angel'o'sphere · · Score: 1

      That thing is not a "moving" barge.
      It is only a barge in name. A better name perhaps would be "floating platform" or pontoon.

      So it is pretty stable anyway. Your concerns make no sense to me.

      --
      Cost free eBook I read (by iBook/Kobo/Amazon/ObookO/Gutenberg etc.): "The Green Odyssey" by Philip Jose Farmer.
    16. Re: No good video? by Anonymous Coward · · Score: 0

      Well, I was asleep this morning so I didn't see it. I can't believe they're going through all this work to catch the rocket in the ocean. After all, the Air Force chose Cape Canaveral so that errant rockets would fall away from people. (Consider the failures of a lot of the Snark launches: they made reference to "Snark infested waters.")

      I'm from north Florida, so I get a chuckle from the idea that it would be better if they'd bring down those boosters on land--in Palm Beach County. It might get people to move away from south Florida. That wouldn't work, though. While the easternmost Florida coast is half a degree to the east of Cape Canaveral, launching rockets at the necessary azimuth would lock them out of most of the useful orbital inclinations.

      Maybe Space-X could buy an island in the Bahamas.

    17. Re: No good video? by onepoint · · Score: 1

      A) Thanks for the photo. That explained a ton.
      B) In vessel design, some basic ratio's are used, and stability is important. The dimensions just don't add up to be any good if it's a barge, the roll and pitch just seem way out of line for such a box type shape. Pontoons on the otherhand, they overcome ( better word is reduce ) multiple stability problem.

      so maybe it's a pontoon type platform, all I got is an overhead shot ( which I thank you for )

      --
      if you see me, smile and say hello.
    18. Re: No good video? by the_other_chewey · · Score: 1

      They never said "land at the same place".

      Yes they did. Landing at the launch site is the planned final goal.

    19. Re: No good video? by Rei · · Score: 1

      [Citation needed]

      --
      It's times like this I wish I had a friend named 'The Professor'.
    20. Re:No good video? by FatLittleMonkey · · Score: 1

      I can just imagine what a rocket looks like on IR.

      Or you could just google it.

      --
      Science is all about firing a drunk pig out of a cannon just to see what happens.
    21. Re: No good video? by FatLittleMonkey · · Score: 1

      Why? Not a clue.

      Hydraulics ran out just before landing. So it lost control at the last moment.

      --
      Science is all about firing a drunk pig out of a cannon just to see what happens.
    22. Re: No good video? by FatLittleMonkey · · Score: 1

      300 x 170 is a real bad ratio, it's going to be a sloppy ride.

      The barge itself is 300 x 100ft. The extra width is on the deck only.

      --
      Science is all about firing a drunk pig out of a cannon just to see what happens.
    23. Re: No good video? by cjameshuff · · Score: 2

      Environmental assessment for their landing sites at LC13 at the Cape:
      http://www.patrick.af.mil/shar...

      Return to launch site has been their goal all along. It's only in the last few months that they started talking about the seagoing landing platform approach, and then only for those situations where there wasn't enough propellant left to return, which were previously expected to require more expensive launches that expended cores instead of recovering them (the Falcon Heavy center core and geosynchronous launches, mainly).

    24. Re:No good video? by Ol+Olsoc · · Score: 1
      I was in Titusville to watch the launch this morning.

      At 4:40 something this morning. Kinda dark then. Kinda dark when the first stage came back. To an unmanned barge in the middle of the ocean.

      Dark video is dark except for bright spots of flame. Initial analysis says yeah- bright flame.

      It was dark because the in intiial launch was called off earlier in the week. And the second one had to be when the ISS - the prime mission - was overhead, Uses one each metric shitload less fuel and time when you do it that way. So they had to try it in the dark, and the ISS will be in that good position earlier and earlier before good daylight conditions happen again. Hence, no choice, and not so awesome landing video. I suspect they will have success soon.

      Launch was fun to watch, tho'. Very yellow flamed exhaust, and a lot less smoke than say, a shuttle launch.

      But hey, if you want some ulterior motive theory, have at it.

      --
      The shepherds did so well protecting the flock that the sheep no longer believed that wolves existed.
    25. Re: No good video? by Anonymous Coward · · Score: 0

      <citation needed>

    26. Re: No good video? by Rei · · Score: 1

      Point conceded - thanks for the link. :)

      --
      It's times like this I wish I had a friend named 'The Professor'.
    27. Re: No good video? by Teancum · · Score: 1

      Specifically it was the hydraulics on the grid fins that ran out of fluid about a half minute before landing. It will be a few days before more details come out about the position of those fins and how those final seconds might have been impacted, but some attitude control was likely lost along with some braking force as the grid fins do provide some additional drag that might not have been compensated for when that hydraulic system drop out of active control.

      It has been said that the rocket hit landed hard.... whatever that might actually mean in terms of velocity.

    28. Re: No good video? by dywolf · · Score: 1

      His concerns dont make sense to you because you dont understand ship design.
      your ignorance however doesnt invalidate his concerns.

      --
      The guy who said the election was rigged won the presidency with the second-most votes.
    29. Re: No good video? by angel'o'sphere · · Score: 1

      We don't talk about ships, but about a fixed floating platform anchored more or less.
      What do you know what I know? Rofl ...

      Perhaps you should read the links he posts, about moving transportation barges, mainly unpropelled and tugged or pushed by an other ship. That has nothing to do with a floating landing platform.

      but a nice try again with your ad hominems.

      --
      Cost free eBook I read (by iBook/Kobo/Amazon/ObookO/Gutenberg etc.): "The Green Odyssey" by Philip Jose Farmer.
    30. Re: No good video? by cwsumner · · Score: 1

      The sea is not stable. There is a tradeoff between riding over the waves (wide) and cutting into the waves (narrow). The most stable forms are two narrow hulls connected at a distance, so it can do both at once. But that fails in very large waves (it turns over and stays that way). A single hull can right it's self, unless it is topheavy. There is more to designing ship hulls that it would seem at first glance. It took us ten thousand years (or more) to figure this much out.

    31. Re:No good video? by Anonymous Coward · · Score: 0

      Im starting to think the actual thing was shot down rather then crashed, I think as soon as something went wrong, an order was given to blow it up (either self-destruct, or an external source) in order to save the barge... SpaceX probably saw / calculated that they would run out of fluid before getting close to the barge... its not like they cant monitor the hydraulic fluid levels.

      some BBC article (I cant find it anymore) mentioned that the navy/army was on standby in case something went wrong... and something did go wrong.

      I guess we'll see if they ever come out with a video...

  2. Volunteers needed by rossdee · · Score: 1

    For the first manned landings

    1. Re:Volunteers needed by Immerman · · Score: 4, Informative

      There will never be manned landings of the first stage. Or the second. For the simple reason that there is no reason to man them in the first place. As for the crew capsule - well by then they will have had lots of practice landing the first two stages, not to mention the much more similar unmanned cargo capsules which are a much easier control challenge than the booster stages - compare balancing a vertical broom in your palm to balancing a baseball. It might get a bit more exciting if the crew were allowed to wander around during landing, chaotically modifying the mass distribution, but I suspect most everyone would rather be strapped firmly in place anyway.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
    2. Re:Volunteers needed by Anonymous Coward · · Score: 0

      and the world is flat............bah

  3. Minor setback by Dereck1701 · · Score: 5, Insightful

    The fact that it made it to the platform itself is a major milestone, correcting whatever caused it to land hard (rough seas, hardware/software issue, ran out of fuel at the last second) would seem to be childs play compared to what was required to get to that point. Reentering craft usually have landing ellipsis of dozens if not hundreds of square miles and this thing landed on a 300'x170' platform. I look forward to the next (hopefully successful) test.

    1. Re:Minor setback by Zibodiz · · Score: 5, Insightful

      Exactly. The fact that it landed well enough that they're reporting the "ship itself is fine" means that it was a success. It doesn't take much to damage a rocket/module/anything that flies into space beyond use. They probably just landed on top of a toolbox or something.

    2. Re:Minor setback by ssam · · Score: 4, Insightful

      I assume that meant the boat was undamaged, not the rocket.

    3. Re:Minor setback by Anonymous Coward · · Score: 1

      Rocket made it to drone spaceport ship, but landed hard... Ship itself is fine.

      How is this nothing but a great success? Never done before. Minor adjustments need to be made, last bugs ironed out, etc. But the thing landed, and was fine. Congratulations!

    4. Re:Minor setback by thrillseeker · · Score: 1

      "Rockets are tricky".

    5. Re:Minor setback by beelsebob · · Score: 1

      It wasn't fine, it was destroyed in the landing. The ship it landed on is fine.

    6. Re:Minor setback by Kjella · · Score: 2

      Yeah, I'm assuming what this means is that it touched down too hard, one or more of the legs bent/broke and the rocket tumbled over. Or all legs didn't get on the platform and it tipped over. Hopefully next time there's a daytime landing, telemetry and debris will presumably give SpaceX what they need watching it would be way cooler.

      --
      Live today, because you never know what tomorrow brings
    7. Re:Minor setback by DerekLyons · · Score: 1

      Exactly. The fact that it landed well enough that they're reporting the "ship itself is fine" means that it was a success. It doesn't take much to damage a rocket/module/anything that flies into space beyond use.

      That they landed "well enough" to report the ship is fine means... well, pretty much nothing. It doesn't take much to damage the rocket, but it does takes a great deal to significantly damage a steel barge. (Think hitting a chunk of granite with a wineglass.)

    8. Re:Minor setback by lennier1 · · Score: 1

      That they made it this far and were most likely able to retrieve a ton of information for their people to improve the next attempt sounds to me as well like they got their money's worth.

    9. Re: Minor setback by Anonymous Coward · · Score: 1

      What exactly has never been done before? Guiding a rocket to its target? Not really. Landing on legs? What do you think the moon landings were? Or any of many robotic probes?

      I'd have to call this a success too, but it's not even an original idea. It just hadn't been a priority before. One could argue it should have been (and I'd agree) but that's another story.

      I wonder, though, would there be all this fawning over a partial (and useful) success had this been a traditional NASA attempt, or would the headlines have focused on what didn't work because government bad. More likely, SpaceX being a private entity, they just have a lot of paid PR people to drum up support.

    10. Re:Minor setback by HangingChad · · Score: 2

      What they accomplished was absolutely amazing. Anyone who doesn't get how astonishing just getting that close really was doesn't understand the problem.

      There has to be a test range on land somewhere they can try putting one down instead of a pitching platform in the middle of the ocean.

      --
      That's our life, the big wheel of shit. - The Fat Man, Blue Tango Salvage
    11. Re:Minor setback by Anonymous Coward · · Score: 0

      Well said!

    12. Re:Minor setback by Rei · · Score: 1

      It tells us at least that the rocket didn't impact it moving at hundreds of meters a second. Sabot-launch a streamlined wineglass out of an high power air cannon at a chunk of granite and yeah, you'll almost certainly break off chunks of it.

      We can say pretty assuredly say that it got to its final landing stage, was slowly lowering itself to the deck... and then "something" went wrong.

      --
      It's times like this I wish I had a friend named 'The Professor'.
    13. Re: Minor setback by dpilot · · Score: 2

      Every first stage ever made and flown has been simply thrown away after one use. FIrst stages are quite a bit different from whatever is on the top of the stack.

      For that matter, "lander on legs" is a different thing on Earth than it is on the moon or Mars.

      I will agree that there is a decided anti-NASA attitude around here, though.

      --
      The living have better things to do than to continue hating the dead.
    14. Re: Minor setback by Rei · · Score: 5, Informative

      Landing *anything* that's been to space on a barge has never been done before.
      Landing a full-size *first stage* that's delivered a payload to space *anywhere* has never been done before (far, far harder problem than landing a crew capsule, they're massive, hard to control, and imbalanced).

      The thing is nearly as heavy as the Space Shuttle, much larger, a much more unstable shape (due to the nature of rockets), has only stubby grid fins for manueuvering, is controlled by a computer with no ability for real-time corrections by a pilot, and was landing on a barge barely larger than itself. And was created on what's by comparison a shoestring budget. Let's not pretend that this isn't a massive challenge.

      I know it's the nerd-equivalent of being a hipster to berate anyone who expresses any support for SpaceX, but for god's sake, look objectively at the nature of this challenge for a minute. One can hate Elon, but these engineers are not exactly picking the low hanging fruit, and they've still achieved very impressive results thusfar.

      (The real question will be, of course, whether they can actually refurbish these first stages cheaper than they can build them... most people assumed the Shuttle would be dirt cheap to refurbish, after all...)

      --
      It's times like this I wish I had a friend named 'The Professor'.
    15. Re:Minor setback by CrimsonAvenger · · Score: 3, Insightful

      No, it tells us they got the Dragon down onto a 300x170 foot platform before things went south.

      Personally, I'm impressed that the Dragon even found the landing barge on the first try....

      --

      "I do not agree with what you say, but I will defend to the death your right to say it"
    16. Re: Minor setback by MightyYar · · Score: 1

      Every first stage ever made and flown has been simply thrown away after one use.

      Neglecting the space shuttle, of course. And to be fair, even that threw away the fuel tank, which IIRC cost $50 million.

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    17. Re:Minor setback by itzly · · Score: 1

      It wasn't the Dragon capsule, but the 1st stage of the rocket itself.

    18. Re:Minor setback by catchblue22 · · Score: 1

      This was the first flight with the maneuvering grid fins. The fact that they were able to bring the rocket to the barge with an untested maneuvering technology is quite remarkable. It speaks volumes to their modelling software. I can speculate that because of the untested grid fins, the maneuvering was not quite as precise as needed and the rocket engines had to do a large slew just before landing, which burned up too much fuel. My speculation is that the fuel ran out just before landing.

      The fact that the rocket arrived on target and with low enough speed that it didn't crater the barge is quite something, and speaks to the near success of this test.

      --
      This and no other is the root from which a tyrant springs; when first he appears as a protector - Plato (423 to 327 BC)
    19. Re:Minor setback by itzly · · Score: 2

      But rocket science isn't exactly brain surgery.

    20. Re:Minor setback by DerekLyons · · Score: 1

      We can say pretty assuredly say that it got to its final landing stage, was slowly lowering itself to the deck... and then "something" went wrong.

      Well, no - we can't say that. Why? Because we don't know that it was slowly lowering itself to the deck. It impacted at 12/ms, but that low speed could have been the result of a long deceleration burn *or* a last second suicide burn. (And in many ways, the second is often a better strategy.)

      But you'd have to actually know something about the problem rather than being a drooling fanboi to appreciate that.

    21. Re: Minor setback by dpilot · · Score: 2

      I liked David Brin's "Tank Farm Dynamo", which featured a space station made from used external tanks. Part of the premise was that ETs were deliberately discarded the way they were, so that they'd burn on reentry and not become space debris. For negligible cost they could be brought the rest of the way to orbit, available for use there.

      --
      The living have better things to do than to continue hating the dead.
    22. Re:Minor setback by Gavagai80 · · Score: 4, Insightful

      There has to be a test range on land somewhere they can try putting one down instead of a pitching platform in the middle of the ocean.

      Not when you launch eastward from Florida.

      --
      This space intentionally left blank
    23. Re: Minor setback by catchblue22 · · Score: 1

      ...SpaceX being a private entity, they just have a lot of paid PR people to drum up support.

      I'm sure this is true. And their enemies in the military-industrial complex (Boeing/Lockheed Martin/ULA) have deep pockets to hire propaganda companies to slander SpaceX. In fact, they already have. Look at the client list of this PR (propagandistic relations) company called Shockey Scofield Solutions.

      Reading between the lines, I think this is a company that specializes in greasing palms/pulling levers in Congress and the Senate, as well as constructing sophisticated internet campaigns that include releases to key susceptible news outlets/columnists and hiring fake posters to post on certain widely read comment boards.

      --
      This and no other is the root from which a tyrant springs; when first he appears as a protector - Plato (423 to 327 BC)
    24. Re: Minor setback by angel'o'sphere · · Score: 1

      For negligible cost they could be brought the rest of the way to orbit
      I doubt the cost was negligible. However I remember the original plans to use those tanks for stations etc. A shame we did not leave them in orbit, imho.

      --
      Cost free eBook I read (by iBook/Kobo/Amazon/ObookO/Gutenberg etc.): "The Green Odyssey" by Philip Jose Farmer.
    25. Re:Minor setback by taiwanjohn · · Score: 1

      It will be interesting to see how "bad" this landing was... Was it a total, catastrophic loss, or did it just break a leg on landing and fall over onto the barge platform? The engines are the most expensive part of the "stack", and there are nine of them on the F9 booster stage. If they can salvage six or seven of these Merlin engines from this booster, even that will be a major victory.

      Given the rate of innovation and development we've seen from SpaceX in the last few years, I suspect we'll see them nail the landing within the next couple of launches.

      I can hardly wait! ;-)

      --
      XML is like violence. If it doesn't solve your problem, you're not using enough of it. --AC
    26. Re:Minor setback by Dereck1701 · · Score: 1

      If it was a fuel issue it could explain something. I've never seen a fuel tank camera before (though I am sure they have been flown before) yet at least the video I watched they gave a view of the second stages fuel tank (I believe) for quite a while after ending the burn. I wonder if they were trying to show the NASA guys that they could stage the rocket a little earlier (leaving more fuel in the first stage) due to an ample safety margin (there seemed to be quite a bit of fuel left.)

    27. Re:Minor setback by Rei · · Score: 1

      Grasshopper always did something roughly equivalent to a last second suicide burn, why would Falcon be any different? But that's "slowly lowering itself to the deck". Only for a brief moment, but the key is, getting the velocity down. It clearly had the velocity down. But something went wrong.

      --
      It's times like this I wish I had a friend named 'The Professor'.
    28. Re: Minor setback by itzly · · Score: 1

      The space shuttle fuel tank was not quite in orbit yet, so it would have taken extra fuel to get it there. And if you park it in a low orbit, it needs regular boosts to compensate for the atmospheric drag. But what good would it do to keep an empty fuel tank in orbit ?

    29. Re:Minor setback by CrimsonAvenger · · Score: 1

      Dragon, Falcon, all the same eh?

      Seriously, not sure how I managed to put the wrong name on the rocket. My bad.

      --

      "I do not agree with what you say, but I will defend to the death your right to say it"
    30. Re: Minor setback by angel'o'sphere · · Score: 1

      The idea was to shoot them into a higher orbit.
      That is why I contradicted the idea of the parent that it would be cheap in fuel, as I believe it would need a quite a bit.

      The idea was you could later combine several of them to form what is now the ISS, or similar stations.

      Of course thinking about it, perhaps they figured that an empty tank makes perhaps a hull, but putting the equipment inside in space might be more challenging than building the modules on earth and shoot them up.

      --
      Cost free eBook I read (by iBook/Kobo/Amazon/ObookO/Gutenberg etc.): "The Green Odyssey" by Philip Jose Farmer.
    31. Re: Minor setback by Strider- · · Score: 1

      But what good would it do to keep an empty fuel tank in orbit ?

      Especially one that's covered in foam that's off-gassing, and shedding small bits and pieces over time. Also, never mind the fact that the tanks were built as thin and as lightweight as possible, so had they been pressurized and converted into living spaces, they would have provided little to no shielding against space debris or radiation. Also, never mind the fact that by definition they were almost empty after launch, so you would still need to haul up all the fittings, equipment, furniture, etc... that you would need to stick inside them.

      The reality is that other than the strong-back that held the shuttle and the SRBs together, the ETs were really just giant aluminum cans, and were about as useful as a spent aluminum can.

      --
      ...si hoc legere nimium eruditionis habes...
    32. Re:Minor setback by multi+io · · Score: 1

      Correcting rough seas doesn't seem to be child's play.

    33. Re:Minor setback by Anonymous Coward · · Score: 0

      There has to be a test range on land somewhere they can try putting one down instead of a pitching platform in the middle of the ocean.

      aside from landing a rocket over places where people live, a bad idea, how do you test landing on the ocean on a test range? The whole point is that the rocket will be falling from a launch Eastward from Florida. It doesn't have enough fuel to fly all the way back to land.

    34. Re: Minor setback by FatLittleMonkey · · Score: 1

      What exactly has never been done before?

      Landing a six story building on a barge in the ocean after launching a commercial capsule to the International Space Station.

      --
      Science is all about firing a drunk pig out of a cannon just to see what happens.
    35. Re:Minor setback by Dereck1701 · · Score: 1

      You can't change rough seas but you can get a ship that is equipped to handle them better (semi-submersible oil platforms for example) or make sea roughness at the landing platform part of the launch criteria much like the launch site wind/rain/electrical launch criteria.

    36. Re: Minor setback by NoMaster · · Score: 1

      Also, never mind the fact that the tanks were built as thin and as lightweight as possible, so had they been pressurized and converted into living spaces, they would have provided little to no shielding against space debris or radiation. Also, never mind the fact that by definition they were almost empty after launch, so you would still need to haul up all the fittings, equipment, furniture, etc... that you would need to stick inside them.

      Also, never mind the fact that it was one of the options seriously considered for what became Skylab...

      --
      What part of "a well regulated militia" do you not understand?
    37. Re: Minor setback by Anonymous Coward · · Score: 0

      I believe it would have taken 2% more fuel to put the tank into orbit. They actually intentionally made sure the thing ended up in the ocean for safety reasons. The problem is it would have been a pretty low orbit, think of all the rocket fuel expended to keep the ISS from falling out of the sky. While a single SS Fuel tank would have had more internal volume than the entire ISS. Keeping something that huge up there would have been expensive.

    38. Re:Minor setback by Anonymous Coward · · Score: 0
    39. Re:Minor setback by Teancum · · Score: 1

      It would be hugely valuable if simply some engines were recovered in some form at all, and send to McGregor for disassembly and engineering review. In other words, if just one engine landed on the deck in a couple of salvageable pieces (not even flight worthy.... just enough to examine), it will still be a valuable exercise.

      It is now looking like SpaceX underestimated the amount of hydraulic fluid needed to keep the grid fins operational at the end of the flight. A small detail sort of like the nut that destroyed Falcon 1 Flight 1 as well as some of the other early Falcon 1 flights that had other correctable but significant flaws that kept the flight from being perfect.

    40. Re:Minor setback by Teancum · · Score: 1

      There has to be a test range on land somewhere they can try putting one down instead of a pitching platform in the middle of the ocean.

      There is such a test range. It is called "Spaceport America", the same place where Virgin Galactic is doing their test flights and planning on providing regular service for the Spaceship Two. In this case, SpaceX is using the facility for a vertical launch due to the high altitude flight restrictions of the area (in part due to the White Sands Missile Range next to this spaceport in New Mexico). It isn't to get the rocket to orbit, but they do plan on testing landing procedures in a repeated fashion and in a way that doesn't tie up the Florida launch site either.

      SpaceX has also done some extensive testing at their McGregor, Texas facility where they perform primarily the engine tests. You can see these tests on YouTube, including watching the cows go into a panic with the rocket sounds on a nearby ranch. The problem with the Texas facility is that the FAA hasn't given SpaceX the clearance they need to test at higher altitudes...which is why they are moving the tests to New Mexico.

      More tests are planned this year, so expect to see some more posts about the vehicle in coming months. This particular test done today happened mainly because they were going to ditch the stage in the ocean otherwise, so they might as well try to get some engineering data to help refine the process under full flight conditions. SpaceX has been using this strategy as well for the past several launches, including some tests that had the rocket hover over the ocean prior to engine shutdown.

    41. Re: Minor setback by Teancum · · Score: 1

      The space shuttle fuel tank was not quite in orbit yet, so it would have taken extra fuel to get it there.

      The extra fuel was in the tank anyway as reserve fuel. The only reason why it was jettisoned before full orbit had to do with trying to keep it from cluttering up LEO with more space debris, so hanging onto the tank would have been trivial by comparison. It would have required a slight design change in the tank construction to make it useful though, and likely some in-orbit construction in order to make the tanks useful on a practical level, but neither the fuel nor applications were a problem. It was mainly an issue of getting a very conservative thinking congress (on space issues) to agree to funding any mission that would use the tank.

      At this point, it is a moot idea since the Shuttle program is no more, but it was an interesting idea that could have been utilizing a resource that otherwise was discarded.

    42. Re:Minor setback by Teancum · · Score: 1

      It should be pointed out that as the Falcon 1 1st stage empties out, even one engine burning at minimum throttle is still strong enough to provide positive lift to the whole stage. In other words, it simply must land with at least some fuel remaining in the tank as it would be ascending and not landing otherwise (unless the tank was dry, but that wouldn't be a landing). It definitely wasn't the fuel reserve that caused this problem.

      The one clearly identified problem was that the grid fins stopped working due to a loss of hydraulic fluid to keep them operational at the end of the flight. I'm sure more will come up as the issues are found.

    43. Re: Minor setback by ScrewMaster · · Score: 1

      Reading between the lines, I think this is a company that specializes in greasing palms/pulling levers in Congress and the Senate, as well as constructing sophisticated internet campaigns that include releases to key susceptible news outlets/columnists and hiring fake posters to post on certain widely read comment boards.

      So, highly-paid, professional astroturfers.

      --
      The higher the technology, the sharper that two-edged sword.
    44. Re:Minor setback by Anonymous Coward · · Score: 0

      There has to be a test range on land somewhere they can try putting one down instead of a pitching platform in the middle of the ocean.

      there is, they already tried it. research the dev process for the landing legs.

    45. Re:Minor setback by Anonymous Coward · · Score: 0

      Dragon, Falcon, all the same eh?

      It's all well and good until the dragon tries to perch on your arm. Also, dragons hate it when you try to put the hood on.

    46. Re: Minor setback by cwsumner · · Score: 1

      It was actually a great success. The just didn't want to say that, because the politicians and salesmen would not understand. 8-)

      Loosing the rocket at the end was like scratching the paint on your car door when you get out in the parking lot. Annoying, sure, but the parking was a success because you can still walk.

  4. What floated by the Dragon's solar panels? by Anonymous Coward · · Score: 2, Interesting

    About 10 minutes and 15 or 20 seconds after the launch, a camera was showing the backs of some solar panels of the Dragon. At that time, it looked like something floated to the upper left, and then floated out of view. The thing was light-colored, and it looked like it was tumbling. Does anyone know what that was? A piece of paper?

    1. Re: What floated by the Dragon's solar panels? by Anonymous Coward · · Score: 0

      Aliens

    2. Re:What floated by the Dragon's solar panels? by Anonymous Coward · · Score: 1

      Yes, it was a piece of paper from the script for the "launch." They forgot to remove it from the NASA soundstage where the "launch" was being filmed.

    3. Re:What floated by the Dragon's solar panels? by Anonymous Coward · · Score: 3, Informative

      Probably just a flake of ice, the rocket/spacecraft are generally covered with it on launch and if you look closely it sheds it throughout the flight.

    4. Re:What floated by the Dragon's solar panels? by MouseR · · Score: 1

      My thoughts as well but it's still surprising a chunk of ice would still be on the vehicle after it went supersonic.

      That's a hell of a lot of friction.

    5. Re:What floated by the Dragon's solar panels? by ColdWetDog · · Score: 1

      The primary buffer panel?

      --
      Faster! Faster! Faster would be better!
    6. Re:What floated by the Dragon's solar panels? by Anonymous Coward · · Score: 0

      Hell of a boundary layer too.

    7. Re:What floated by the Dragon's solar panels? by Strider- · · Score: 1

      Probably a cover (either foil or tyvek, not sure what they use) that covers over the RCS jets while the rocket launches, then is discarded when the jet is first fired. A similar thing was occasionally seen on shuttle launches. These covers are there to keep crap (both bird, and rainwater etc...) out of the jets while the rocket is sitting on the pad.

      --
      ...si hoc legere nimium eruditionis habes...
  5. it made it home by onepoint · · Score: 4, Insightful

    Well, I think it's a milestone. Just getting it to land on the platform, in the dark, without any human help. That speaks a lot of the hard work that people invested. So it gets some damage, big deal.
    I am glad that it was not a total success, otherwise people might get into lazy thinking and not look for bugs. I believe (not sure, cannot cite sources on this), but some airplane was not tested enough because everything happened perfect on testing, it was placed into production (1950's). Over the course of a year or 2, the planes were having issues and a few crashed. And they had to stop production. Some sort of fault in the structure.

    So, in summary, He's done it!!! now to get all the bugs worked out.

    --
    if you see me, smile and say hello.
    1. Re:it made it home by thrich81 · · Score: 4, Informative

      Sounds like the aircraft you are describing is the De Havilland Comet, http://en.wikipedia.org/wiki/D...

    2. Re:it made it home by Lunix+Nutcase · · Score: 1

      Well, I think it's a milestone. Just getting it to land on the platform, in the dark, without any human help.

      What is all that special about landing in the dark? You do realize we have all sorts of cameras that can "see" in the dark, right?

    3. Re:it made it home by DerekLyons · · Score: 1

      I am glad that it was not a total success, otherwise people might get into lazy thinking and not look for bugs. I believe (not sure, cannot cite sources on this), but some airplane was not tested enough because everything happened perfect on testing, it was placed into production (1950's). Over the course of a year or 2, the planes were having issues and a few crashed. And they had to stop production. Some sort of fault in the structure.

      You're probably thinking of the Comet - the problems were less ones of insufficient testing than ones of not knowing how to build such an aircraft and what to test for in the first place. Comet was the first jet airliner, and entered service when there wasn't a lot of experience with large jets of any kind.

      Either way, no booster is tested in any way close to as much as a typical... well, pretty much anything else is tested. It's not at all unusual for rockets to carry actual payloads on their first launch, and to be declared fully operational after less than a handful.

    4. Re:it made it home by onepoint · · Score: 1

      What is special about landing in the dark... hmmm.
      a) Depth perception in darkness changes (given they could use some sort of sonar type bounce to get a distance reading)
      b) Blindness of the camera's when the thrusters are activated.
      c) Landing on the water, barges move up and down, that's really impressive, it's only so stable. This is nothing like a carrier landing in any way.

      Well anyway, I am amazed and cheering for them!!!

      --
      if you see me, smile and say hello.
    5. Re:it made it home by onepoint · · Score: 1

      thank you

      --
      if you see me, smile and say hello.
    6. Re:it made it home by Lunix+Nutcase · · Score: 1

      a) Depth perception in darkness changes (given they could use some sort of sonar type bounce to get a distance reading)

      There are all sorts of sensors and readings to use to land in the dark especially when automated. You do realize that planes fly all the time in the dark and in fog, right?

      b) Blindness of the camera's when the thrusters are activated.

      You wouldn't be using only cameras. You would have a host of other sensors to provide all manner of positional information. None of this is new or impressive.

      c) Landing on the water, barges move up and down, that's really impressive, it's only so stable. This is nothing like a carrier landing in any way.

      Sure, that is impressive, but has nothing to do with being in the dark. Such a thing is tricky regardless of the amount of light.

    7. Re:it made it home by onepoint · · Score: 1

      >>You do realize that planes fly all the time in the dark and in fog, right?
      Yes, I do and that's with humans at the stick, but the plane can land itself. on a stable platform ( runway ) that has know variables, big space, a performance design that have been tested and tested and updated almost to the point that it's automated, but at the end, a pilot is still required just in case. Landing and takeoffs are still the highest risk points of a flight.

      But this landing, this is a tiny little speck, and it hit the mark! it's really a super amazing thing.

      Now I'll give you a perspective that might help you understanding my views
      you are looking at current technology, seeing the future and mixing in rose colored glasses ... It's not an insult, we expected wireless Dick Tracy watch's but they did not happen till the late 90's. I, myself bitch and complain about nanobot's not being injected into the human blood stream to remove bad blood cells ( I really expected that to happen by 2000, and I am still waiting ) and there is a ton more.

      this happens to everyone, we mix the future with the current. It's not a bad thing at all, it just shows us what we desire as humans and what we can succeed at. Without this expectation, we would not be able to grow, Knowing that you expect it and if it had failed, someone out thier would be trying to solve it. It's in our nature ( or at least I think it is )

      --
      if you see me, smile and say hello.
    8. Re:it made it home by Anonymous Coward · · Score: 0

      A) Sonar probably isn't going to be much of an option with a rocket engine firing

  6. New meaning by caffiend666 · · Score: 1

    New meaning to "Hit the deck!" Or "Incoming!" Perhaps they should rename the barge to "Oh fuck!" Seriously, congrats though SpaceX

    --
    Here's to losing my Karma Bonus again....
  7. No video? by Immerman · · Score: 1, Redundant

    Come on, didn't they learn their lesson trying to reconstruct video to analyze earlier water landings? Here you've got a big frigging barge that they expect to be ground zero for an important rocket crash - I would have expected them to mount a few automatic cameras on nearby buoys so they'd be sure to get multiple videos of the crash to learn as much as possible

    --
    --- Most topics have many sides worth arguing, allow me to take one opposite you.
    1. Re:No video? by Anonymous Coward · · Score: 0

      SpaceX is a very touchy when it comes to failures. Heck, there are times that the video feed on the NASA network (at KSC) is cut for the SpaceX launch pad or there is an embargo of the feed.

    2. Re:No video? by rmdingler · · Score: 1

      "...pitch dark and foggy..."

      And a real pity no technology exists to illuminate a scheduled landing to allow clear recording by the cameras that were deployed.

      --
      Happiness in intelligent people is the rarest thing I know.

      Ernest Hemingway

    3. Re:No video? by Megane · · Score: 1

      Hey, give 'em a break. They have to launch at exactly the right moment to catch ISS, and today's moment was simply too early to have any sunlight there. The dense fog didn't help either. On the other hand, it didn't land in the water, so they can finally take the SD card out of the GoPro in the rocket!

      I just want to see a picture of rocket bits on the barge, broken or not.

      --
      #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
    4. Re:No video? by EnsilZah · · Score: 1

      The guys at http://www.reddit.com/r/spacex have been following the Autonomous Spaceport Drone Ship (That 'Drone' really helps with the abbreviation) from a cruise ship that has a webcam pointed in its general direction when it's in port, hopefully we'll get a glimpse of it when it gets back.

    5. Re:No video? by ColdWetDog · · Score: 2

      Yeah guys, it's early in the sequence. They may well have low light / infrared cameras pointing at the thing. They probably don't have cameras hovering around waiting to transmit from the middle of nowhere in realtime. Further, most IR cameras have reduced spatial resolution compared to visual range so they may have decided that the investment in time and money wasn't worth it. The telemetry will show the engineers the important stuff. He's not doing this to make YouTube videos.

      --
      Faster! Faster! Faster would be better!
    6. Re:No video? by wiredlogic · · Score: 1

      It is inconceivable that they didn't have cameras all over the barge. The problem is that SpaceX is on track to put all of its competitors out of business and they will seize on any scrap of "evidence" to trot in front of Congress to claim that their rockets are dangerous. The 50% odds of success Musk claimed were probably bogus too but a necessary lie to keep the detractors at bay.

      --
      I am becoming gerund, destroyer of verbs.
    7. Re:No video? by Pallas+Athena · · Score: 1

      I suppose the real issue is the fog. Darkness, well you have high-sensitive camera's, spotlights, ... - and don't forget, an incoming _rocket_ - that's quite a large candlelight! Fog, however, is a different beast. There is nothing that you can do that allows you to create sufficient quality video in dense fog.

    8. Re:No video? by Pallas+Athena · · Score: 1

      Has anyone here experience as to how an infrared camera fares when you point it at a rocket exhaust?

    9. Re:No video? by Anonymous Coward · · Score: 0

      That, or SpaceX just don't want to look bad. Also not sure how competitors would use footage of a descending 1st stage to claim danger to the ascending payload.

      Musk is a very productive fellow but don't idolize him too much, it leads to mistakes.

    10. Re: No video? by Anonymous Coward · · Score: 0

      Flood lights aren't particularly good in foggy conditions, and can actually be a hindrance.

    11. Re: No video? by Anonymous Coward · · Score: 0

      As has been asked and answered many times in this thread already, it was pitch black and foggy, so the cameras they did have didn't see much.

    12. Re:No video? by robbak · · Score: 1

      In the reddit AMA, Musk stated that the 50% wasn't calculated from anything, but was just a guess. And we didn't expect to get video of a failure, because of persons using such video to create bad publicity.

      All of us over at r/spacex are ecstatic about this. The mission was a 100% success (so far), and the landing, 90%.

      --
      Prediction for end of Universe #42: Fencepost error in Quantum_bogosort.cpp
  8. A bit off topic by alexander_686 · · Score: 1

    I have a semi-related questions – why not add wings and land the first stage like a airplane or done?

    Is the extra weight for the fuel needed to land the first stage really that much less than the extra weight for wings? Even if the wings weighted more, I would think that the simpler design would win over. Of course, I am assuming that balancing a multi-ton pencil on a pillar of flame is hard.

    1. Re:A bit off topic by Anonymous Coward · · Score: 2, Interesting

      Adds a *lot* of extra drag and parasitic mass on the ascent. Still, the Russians planned to do that with the Baikal flyback booster: http://en.wikipedia.org/wiki/Baikal_%28rocket_booster%29. They may decide to revive it, given the apparent progress SpaceX is making...

    2. Re:A bit off topic by EnglishTim · · Score: 1

      My guess is that folding wings & landing gear would be heavier and more difficult to produce. Also, it would mean you'd need a landing strip to land at, which would mean it would have to fly over land; probably a harder thing to get clearance for.

    3. Re:A bit off topic by Dereck1701 · · Score: 1

      There are some working on a similar concept (Stratolaunch, Russian Re-entry Rocket Module (RRM), defunct Roton Rocket). To each their own, I would imagine that SpaceX didn't want to try to mix disciplines (rocketry & aircraft) and add moving parts. You can't just put a wing on a rocket and launch it, doing so adds immense drag and difficult to resolve aerodynamic forces so they often have to be stowed/folded into the rocket somehow. The only craft that I believe has successfully added fixed wings is the shuttle and that did it through brute force (SRBs) and a minimal aerodynamics (it screamed towards its runway at around 600 mph and then slams on the airbrakes and puts itself into controlled a stall to land at over 200 mph).

    4. Re:A bit off topic by itzly · · Score: 1

      I am assuming that balancing a multi-ton pencil on a pillar of flame is hard.

      No doubt that it is hard, but the control system does not add a lot of mass or drag, so there's a big reward for figuring it out.

    5. Re:A bit off topic by alexander_686 · · Score: 1

      Maybe. While your points are valid, I would be careful about using the Space Shuttle as a key exhibit because it was the result of a stupid compromise.

      The Space Shuttle was designed to land at the Vandenberg Air Force Base, which is much further north than Kennedy. In order to reach that far north the Space Shuttle needed a delta wing and had to come in screaming fast. The civilians at NASA would have preferred a straight wing. While it could not have reach Vandenberg, it was lighter and landing the thing would have been easier since it would have been at lower speeds.

      I personally think this one of those stupid compromise decisions that morphed the Space Shuttle from a cheap reliable pickup truck into one of the most complex and expensive machines to run and set back our space program by 20 years.

    6. Re:A bit off topic by Rei · · Score: 1

      It is hard - extremely hard. Stability is only part of the problem, hover offers a lot of other problems that don't crop up when the craft is facing strong and roughly steady G forces. But landing like that gives mass benefits. And small mass benefits on one stage means very large benefits for your payload capacity delivered to space. So if you can pull it off, it's a big win.

      --
      It's times like this I wish I had a friend named 'The Professor'.
    7. Re: A bit off topic by joh · · Score: 4, Informative

      Putting wings on something that consists of empty tanks in front and heavy engines in the tail is harder. A rocket stage has totally the wrong center of gravity to fly this way. Try to throw a dart with the heavy tip backwards and you will see why.

    8. Re:A bit off topic by MightyYar · · Score: 1

      I don't think the fuel is "extra"... I think it is safety margin fuel that would otherwise be wasted. Remember that this thing has to be able to make it to orbit even with the loss of an engine or two.

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    9. Re:A bit off topic by MightyYar · · Score: 1

      It also had to land fully-loaded, because the military wanted to be able to bring stuff back from space.

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    10. Re: A bit off topic by Anonymous Coward · · Score: 0

      The extra margin and engine-out capability is not a requirement, just something that SpaceX designed as extra mission assurance (and for their own motives for testing first stage reusability). A few of the earlier satellite launch contracts chose to use the extra margin to boost the satellites into a more optimal orbit (to save maneuvering fuel for the satellites) instead.

    11. Re:A bit off topic by underlord_999 · · Score: 1

      There are a few statements in your post that are misleading / incorrect.

      While Vandenberg AFB did have runways extended to over 15000 feet to support Shuttle landings, the more important criteria for delta wings was that the Shuttle would have been *launched* from Vandenberg (from SLC-6) for *polar-orbit* missions.

      A landing site at Vandenberg AFB in California or Edwards AFB (also California) being further *north* has little to do with the delta wing shape. It's the fact that the mission profile for a polar orbit is very different than what was flown from Kennedy.

      Launching from Vandenberg would have the shuttle launching south (for polar orbit insertion) rather than launching east as it did for Florida launches. This was primarily for military missions, performing a satellite capture or deployment and then landing once-around the Earth.

      Landing once-around after a polar orbit means that your launch/landing site has rotated with the Earth, 22.5 degrees east or roughly 1500 miles.

      The straight-wing shape was unable to accommodate a translation west-to-east of that extent and so, a delta-wing was needed. A straight-wing shape, as proposed, mandated an extremely high angle-of-attack re-entry which necessarily lead to a dangerous flight transition: from stalling blunt-body re-entry to a subsonic flight. A stalling aircraft leads to increased risk of total loss-of-control and breakup of the vehicle.

    12. Re:A bit off topic by FatLittleMonkey · · Score: 1

      And small mass benefits on one stage means very large benefits for your payload capacity delivered to space.

      You are getting your rocket equation backwards. While small changes to payload result in exponentially increasing changes through the stages, reciprocally it takes a large change to the first stage to have a small effect on payload.

      --
      Science is all about firing a drunk pig out of a cannon just to see what happens.
    13. Re: A bit off topic by subreality · · Score: 1

      You could fly it with the engines in front. It's easy to flip it around before reentry.

    14. Re:A bit off topic by Teancum · · Score: 1

      The Space Shuttle was designed to land at the Vandenberg Air Force Base

      Was there a Shuttle landing strip at VAFB? An air strip that could bring the Shuttle on the 747 carrier certainly existed and was even used on a couple occasions (when the Enterprise showed up there for some fitting tests), but I don't think it was ever intended to land there.

      On the other hand, Vandenberg was to be a launch site for polar launches with an emphasis on military payloads that never ended up being used with the Shuttle. I'm pretty sure any such landings were to happen at Edwards AFB, but I might be wrong on that issue.

      The big change to the Shuttle was the cross-range requirement where it could potentially evade Soviet (at the time) tracking and be able to do a single orbit mission to put a military payload into orbit and land immediately after deployment. Such a flight would require significant turning since over the course of the mission a straight wing would have put the Shuttle over the middle of the Pacific Ocean (when launched from Vandenberg). Again, no such mission ever actually happened, but it was one of the things that adversely impacted the shuttle design since it was designed to fly such a mission.

    15. Re: A bit off topic by Teancum · · Score: 1

      The extra margin and engine-out capability is not a requirement

      On the contrary. It is a requirement as per NASA contracts, but also standard practice in the rocket industry. It is called reserve fuel. Look it up. Every successful launcher that has put things into orbit has such a reserve fuel load that never gets used except in emergency conditions.

      SpaceX is merely taking advantage of that reserve fuel after the 2nd stage has been lit up to be able to do something useful with the 1st stage. The engine-out capability is something that has been used by other rocket designers as well, including something Werner Von Braun used in his design of the Saturn V.... something that even made a couple Apollo flights successful that would have failed had that capability not been there.

      You don't plan on using the reserve fuel in a nominal flight to boost performance. SpaceX did launch a geosynchronous orbit satellite that pushed the reserve fuel load to the point that testing of the 1st stage landing procedures didn't happen, but it still had the reserve fuel left in the 1st stage after stage separation. It was later said that SpaceX did test the landing process anyway on that flight, but it was rather low-key and didn't involve a hover test.

    16. Re:A bit off topic by cbhacking · · Score: 1

      Yep. SpaceX has said that a full-capacity F9 launch probably won't have the fuel reserve for a propulsive landing (though it should still have the fuel for engine-out capability; the other rockets just burn longer although that does use a bit more fuel total). However, most rocket launches aren't maximum capacity. Frequently you run into volume rather than mass limits, or you need to place one thing into a precise orbit and there's nothing else you're putting in an even slightly-similar orbit. In those cases, assuming no engine failures or similar (which could also mean there's not enough fuel reserve for flyback and propulsive landing), the first stage still has several percent fuel left at separation, but relatively little mass; the second stage and payload are gone, as is the majority of the fuel.

      --
      There's no place I could be, since I've found Serenity...
    17. Re: A bit off topic by Anonymous Coward · · Score: 0

      How about flying it backwards: heavy engines in front, empty tanks behind? It should be gliding at this point anyway, so you're not using the engines as engines. And the aerodynamics are terrible either way around.

    18. Re: A bit off topic by Anonymous Coward · · Score: 0

      What will happen to a dart thrown backwards will have a lot more to do with aerodynamics than weight distribution.

    19. Re: A bit off topic by werepants · · Score: 1

      Don't know what I'm doing replying to an AC - but weight distribution is not at all separate from aerodynamics. Look up center of pressure some time and center of mass - the location of these is what determines whether you can get stable flight. Hint: put heavy shit forward, put air resistance towards the rear.

      If you don't believe me, try throwing a dart without extra weight in the tip.

  9. No KSP at SpaceX? by Keruo · · Score: 1

    One of the first contracts in KSP career mode gets you to save one stage with parachutes, maybe SpaceX should look into something similar..

    --
    There are no atheists when recovering from tape backup.
    1. Re:No KSP at SpaceX? by EnglishTim · · Score: 4, Informative

      Firstly, I think SpaceX were trying to get away from parachute recoveries. The Shuttle solid booster rockets used to parachute down into the ocean, but the problem with that is that they need completely cleaning out and refurbishing between each flight.

      Secondly, they would need more than parachutes to recover the first stage because it is travelling so fast when it separates (not sure of the exact number, but somewhere between 2 and 4 Kilometers per second). They have to do a retrograde burn to slow down enough to safely re-enter the atmosphere.

    2. Re:No KSP at SpaceX? by cheesybagel · · Score: 1

      They already tried that more than once. It did not work well. The impact on landing is too large. You need the retro-rocket burn.

    3. Re:No KSP at SpaceX? by Anonymous Coward · · Score: 0

      They already tried that more than once. It did not work well. The impact on landing is too large. You need the retro-rocket burn.

      In addition, my understanding is that a parachute would introduce a whole set of different stresses on the booster structure.

      That is, the booster structure is designed to withstand the tremendous compression forces from the launch. Hanging the booster from a parachute creates a set of tension forces. The parachute at the top and the heavy engine at the bottom of the booster would literally tear the booster apart.

    4. Re:No KSP at SpaceX? by Dereck1701 · · Score: 1

      I've heard that parachutes are fairly expensive, not horribly reliable (on the Ares-1x test flight 2 out of 3 failed), aren't really reusable and don't really decelerate spacecraft enough for a soft landing. There is a reason why most capsule spacecraft land in the ocean, landing on ground requires retrorockets.

    5. Re:No KSP at SpaceX? by Anonymous Coward · · Score: 0

      Even with a perfect rocket born, ending in 0 velocity at 0 altitude above the ocean, there is still a lot of damage, just from the stage falling over and hitting the waves. Parachutes can't prevent falling over, the only solution is to not fall over by landing on a land (or a ship).

      The space shuttle boosters landed using parachutes, and did survive the waves. I assume they stronger (and therefore unnecessary heavier) than the SpaceX rockets, and as far as I know, the space shuttle boosters where stored but never actually re-used, since it was to difficult to determine if the water landing caused any damage.

    6. Re:No KSP at SpaceX? by ClayJar · · Score: 1

      The SRBs from Shuttle launches were indeed reused... after a fashion. Each booster was four segments. After each flight and recovery, the boosters were disassembled and the segments renovated and reloaded. The segments were not kept together as a set, so each SRB used in a launch would have four segments each with their own history. (This was expressly noted on NASA TV during each launch, with comments about the oldest and newest segments on the flight and so on.)

      As for SpaceX, early Falcon 9 flights had parachutes on the first stage, but the stages did not survive reentry (much less make it all the way to landing). Since you can not land anything large on Mars with parachutes, SpaceX would have eventually had to work on hypersonic retropropulsion, propulsive landings, and so on; they merely pivoted away from the parachute "dead end" and went straight to propulsive recovery with Falcon 9 v1.1.

  10. In other words ... by frank249 · · Score: 1

    The operation was a success but the patient died.

    --

    Today's vices may be tomorrow's virtues.

    1. Re:In other words ... by Anonymous Coward · · Score: 0

      Nah, the patient is heading to the ISS quite nicely. The tools we used for the surgery won't be re-usable though.

  11. Re:Meanwhile the UFOs are flying everywhere by Anonymous Coward · · Score: 0

    The first three videos did not convince me of anything. One frame, depicing brownish residue near a docking port. Perhaps due to this place:

    http://en.wikipedia.org/wiki/File:Zvezda_toilet.jpg

    Now what? Should I watch the rest of the obnoxius commentary in hope of there being quality unexplainedness there?

  12. classical by Anonymous Coward · · Score: 0

    mechanics that is: the trajectory was well known, the masses were well known. The motor control is hi-tech, but well known.

    It makes sense tat it would get to the landing platform within a good accuracy. And with all the sensors nowadays, good precision. Gravity is your friend here.

    Now gravity is not your friend when you're trying to control decel, which is what we're looking at.

    Total failure without any video. I mean, with all the drone tech out there, they didn't have a drone circling and filming the landing? Total let down--we want video!.

    1. Re:classical by Anonymous Coward · · Score: 0

      Total failure without any video. I mean, with all the drone tech out there, they didn't have a drone circling and filming the landing? Total let down--we want video!.

      At night?! In a fog!!?

      Good luck with that!

  13. Re:Meanwhile the UFOs are flying everywhere by Anonymous Coward · · Score: 0

    If you are in space, there is no "hypersonic", as there is no "sonic".

    Right angle turns are rather simple for a low mass plasma.

    All depends on the contracts...

  14. Twitter: Ran out of Hydralic fluid by frank249 · · Score: 5, Informative

    Elon Musk @elonmusk "Grid fins worked extremely well from hypersonic velocity to subsonic, but ran out of hydraulic fluid right before landing."
    "Upcoming flight already has 50% more hydraulic fluid, so should have plenty of margin for landing attempt next month."

    --

    Today's vices may be tomorrow's virtues.

  15. Re:Twitter: Ran out of Hydralic fluid by photonic · · Score: 1

    The fact that he can make this claim only half a day after the fact (so I assume they had no time to piece together the debris) means that they did recover the most valuable part: the telemetry. Overall, they achieved probably 95% of the required challenges. With around 5 successful retro burns, 1 low-level flame out due to loss of roll control, 2 soft water landings, 1 bullseye impact on a boat and around ten successful low altitude tests with grasshopper, only extremely bad luck can stop them from making a good landing in the next few attempts.

    --
    karma police: arrest this man, he talks in maths; he buzzes like a fridge, he's like a detuned radio. [radiohead]
  16. Strange definition of success by Dcnjoe60 · · Score: 0

    For SpaceX to be successful, it needs to be able to achieve it's mission in space and arrive home safely. I understand wanting to put a positive spin on things, but really, if only accompished your mission is space is the measure of success, then the last flight of the Shuttle Columbia was a fantastic success, too. A successful mission requires accomplishing the goals and returning safely.

    1. Re:Strange definition of success by Anonymous Coward · · Score: 1

      The previous landing tests (on the ocean surface, without actual landing platform) did not use the steering fins, and had a landing accuracy in the order of 10km. Hitting the ship is a _huge_ improvement in accuracy, even if it was just outside the new 10m error margin.

      Slowing the rocket down to 0 speed at 0 altitude is also very tricky. The engines can only be throttled down to 70% of there max power, so even with one of the 9 engines, the minimum thrust is more than the weight of the (empty) first stage. Start the landing burn too soon, and the rocket will go back up before reaching 0 altitude, start the landing burn too late and you won't reach 0 speed before reaching 0 altitude.

    2. Re:Strange definition of success by EnsilZah · · Score: 1

      The mission is to deliver cargo to the ISS for their client, NASA.
      Landing the first stage is a separate internal goal and the data they got from this attempt is progress towards that goal.

    3. Re:Strange definition of success by Dcnjoe60 · · Score: 0

      The mission is to deliver cargo to the ISS for their client, NASA.
      Landing the first stage is a separate internal goal and the data they got from this attempt is progress towards that goal.

      And the Apollo mission was to land a man on the moon. There is an implied goal of returning safely. What is the point of SpaceX using a reusuable launch vehicle if it doesn't matter what happens to it on the way back? Again, by that measure, the Shuttle Columbia was a successful mission. They accomplished what they set out to do. Returning safely, was just an internal goal.

    4. Re:Strange definition of success by Anonymous Coward · · Score: 0

      There's no implied goal to return something which everybody before you used to dump as expendable. Landing the first stage is SpaceX's internal goal, because they aim higher than the rest.

    5. Re:Strange definition of success by EnsilZah · · Score: 1

      The difference is that for the manned flights you've mentioned, returning the astronauts back to earth was part of the primary objective and they wouldn't have launched if they didn't have a high likelihood of accomplishing it.

      The goal of SpaceX Falcon 9 launches is to deliver cargo to orbit, once that is accomplished the mission is a success.

      The fact that they can use the spent first stage of the rocket for development testing towards developing reusability instead of just letting it splash down into the ocean is a bonus.

    6. Re: Strange definition of success by Anonymous Coward · · Score: 0

      You seem to mix up two things here - the Dragon Spacecraft is currently in orbit - that is the part that is going to return with either cargo or crew back to earth at the end of the mission.

      What landed/tried to land today is the first stage of the ROCKET, not the mission spacecraft. The rockets so far have always been throwaway and crashed in the ocean or somewhere with low population after they boosted the second stage with the spacecraft. the goal here is now to recover the first stage and reuse it - something that has never been done by anyone, be it NASA or anyone else. NASA returned and reused the boosters on the space shuttle via chute and splashdown, but they had to be extensively rebuilt each time due to salt water corrosion. spaceX is currently doing something amazing that has never been done before with so much ambition, that's why everyone is looking forward to them succeeding.

    7. Re: Strange definition of success by alexandergruel · · Score: 1

      You seem to mix up two things here - the Dragon Spacecraft is currently in orbit - that is the part that is going to return with either cargo or crew back to earth at the end of the mission. What landed/tried to land today is the first stage of the ROCKET, not the mission spacecraft. The rockets so far have always been throwaway and crashed in the ocean or somewhere with low population after they boosted the second stage with the spacecraft. the goal here is now to recover the first stage and reuse it - something that has never been done by anyone, be it NASA or anyone else. NASA returned and reused the boosters on the space shuttle via chute and splashdown, but they had to be extensively rebuilt each time due to salt water corrosion. spaceX is currently doing something amazing that has never been done before with so much ambition, that's why everyone is looking forward to them succeeding.

    8. Re:Strange definition of success by Morky · · Score: 3, Insightful

      You may not have been following what SpaceX is trying to do an the methodology to get there. The mission is to resupply the ISS, which looks to be a 100% success for the fifth time, pending a safe docking on Monday. They also have returned a payload of cargo to return to Earth safely four times. The Progress Raduga capsule can only return 150 kg of cargo, where Dragon can return 2500 kg, pressurized. They are doing all of this at a much lower cost than the competition. This is the mission and they have been 100% successful with Falcon 9 v1.1 every time.

      They have a long-term goal of full reusability for their spacecraft, starting with the most expensive part of the launch, the first stage booster. Because every other launch in the history of rocketry has involved the destruction of the first stage, they build the cost of losing the first stage into the total launch cost. (The space shuttle's boosters parachuted back to Earth, but were not reusable - just parts of them, and only after a great deal of costly refurbishment.) Each attempt to land the booster is an experiment at this point, which has the benefit of being a freebee, as the booster has already been paid for. Attempt one spun out of control, but they got good data, understood the problem and adjusted. Attempts two and three had the booster vertical and hovering over the ocean. This was 100% success, as there was no more optimal outcome for the experiment. However, the landing point was not a precision target, but a 10 sq km range. On today's first attempt to land on a solid surface, they had to land with extreme precision, which they did successfully, but came down too hard. These are experiments, so each step forward, as long as the failures produce actionable data, can be deemed a success.

    9. Re:Strange definition of success by Anonymous Coward · · Score: 0

      And the Apollo mission was to land a man on the moon. There is an implied goal of returning safely. What is the point of SpaceX using a reusuable launch vehicle if it doesn't matter what happens to it on the way back? Again, by that measure, the Shuttle Columbia was a successful mission. They accomplished what they set out to do. Returning safely, was just an internal goal.

      Implied goal of returning safely??

      "I believe that this nation should commit itself to achieving the goal, before this decade is out, of landing a man on the moon and returning him safely to the earth."

      -President Kennedy, Address to Congress on Urgent National Needs, May 25, 1961

    10. Re:Strange definition of success by cbhacking · · Score: 1

      Wow, you're a special kind of dense, aren't you?

      Columbia and most of the Apollo flights were manned. Calling safe return "just an internal goal" is not only moronic, it's flat-out wrong in the case of Apollo:

      "this nation should commit itself to achieving the goal, before the decade is out, of landing a man on the moon and returning him safely to the earth."

      JFK (emphasis mine), 25 May 1961, http://www.jfklibrary.org/JFK/...

      Second, you seem to be deeply confused (or trolling) about the difference between a space vehicle and a launch system. Dragon is a space ship, a "vehicle"; it carries stuff. The Dragon 2 (Crew Dragon) will carry people. It is, obviously, of critical importance to return them safely. Falcon 9 first stage isn't even an entire launch system, just the most expensive part of one (the first stage). A spent first stage is a like a (really expensive) spent bullet cartridge; sure, you save money on future shots if you collect it and re-use it, but the goal of any given shot is to fire the bullet and hit the target. Similarly, the goal of a Dragon/Falcon 9 launch is to put Dragon in orbit, and recover it safely.

      In fairness, it's inaccurate to say that the CRS-5 mission is successful yet. Dragon hasn't even berthed with the ISS yet, much less returned safely to Earth. That doesn't seem to be your objection at all, though.

      --
      There's no place I could be, since I've found Serenity...
  17. Reinventing the wheel -- Am I missing something? by ClaraBow · · Score: 1

    Is SpaceX accomplish something that hasn't been done by NASA? I don't understand all the excitement over landing a rocket when it has already been done so many times before? Am I missing someone?

  18. Re:Reinventing the wheel -- Am I missing something by Chibi+Merrow · · Score: 3, Informative

    Yes, that's exactly what they're doing. No one has soft-landed the first stage of a rocket after using it to launch something into orbit before. That stage normally burns up on reentry or is debris in the ocean.

    --
    Maxim: People cannot follow directions.
    Increases in truth directly with the length of time spent explaining them
  19. Re:Meanwhile the UFOs are flying everywhere by Anonymous Coward · · Score: 0

    @the person who started spouting vulgarities:

    Kindly, retard, you are not speaking to an employee of your silly government, but an amateur rocketry person from the former USSR. You are hereby most strongly advised to sod off (if you don't know how, please request instructions) and return with quality video.

    I mean this. Quality video. If you have any problems obtaining it from NASA, do cough up the money to monitor the ISS from Earth (there are those things called "telescopes", aren't there) or from space (one can purchase satellite launches, cannot one?). If all the world's conspiracy theorists put their money where their mouth is, you'd have ISS under 24/7 coverage, would you not?

    Well, why don't you? Lizards took the money?

  20. Re:Reinventing the wheel -- Am I missing something by frank249 · · Score: 1

    NASA has used parachutes for rentry. Several new technologies needed to be developed and tested to facilitate successful launch and recovery of both stages of the SpaceX reusable rocket launching system. Following the completion of the third high-altitude controlled-descent test, and the completion of the third low-altitude flight of the second-generation prototype test vehicle (plus eight flights of the first-generation Grasshopper prototype flight test vehicle), SpaceX indicated that they are now able to consistently "reenter from space at hypersonic velocity, restart main engines twice, deploy landing legs and touch down at near zero velocity."[29]

    The technologies that were developed for this program, some of which are still being refined, include::

            restartable ignition system for the first-stage booster[17] Restarts are required at both supersonic velocities in the upper atmosphere—in order to decelerate the high velocity away from the launch pad and put the booster on a descent trajectory back toward the launch pad—and at high transonic velocities in the lower atmosphere—in order to slow the terminal descent and to perform a soft landing.[30]
            new attitude control technology—for the booster stage and second stage—to bring the descending rocket body through the atmosphere in a manner conducive both to non-destructive return and sufficient aerodynamic control such that the terminal phase of the landing is possible.[30] This includes sufficient roll control authority to keep the rocket from spinning excessively as occurred on the first high-altitude flight test in September 2013, where the roll rate exceeded the capabilities of the booster attitude control system (ACS) and the fuel in the tanks "centrifuged" to the side of the tank shutting down the single engine involved in the low-altitude deceleration maneuver.[21][31] The technology needs to handle the transition from the vacuum of space at hypersonic conditions, decelerating to supersonic velocities and passing through transonic buffet, before relighting one of the main-stage engines at terminal velocity.[19]
            throttleable rocket engine technology is required to reduce engine thrust because the full thrust of even a single Merlin 1D engine exceeds the weight of the nearly empty booster core.[32][33]
            terminal guidance and landing capability,[13] including a vehicle control system and a control system software algorithm to be able to land a rocket with the thrust-to-weight ratio of the vehicle greater than one,[34] with closed-loop thrust vector and throttle control[35]
            navigation sensor suite for precision landing[30][36]
            lightweight, deployable landing gear for the booster stage.[10] In May 2013, the design was shown to be a nested, telescoping piston on an A-frame. The total span of the four carbon fiber/aluminum extensible landing legs[37][38] is approximately 18 meters (60 ft), and they weigh less than 2,100 kilograms (4,600 lb); the deployment system uses high-pressure Helium as the working fluid.[39][40]
            hypersonic grid fins were added to the design beginning on the fifth ocean-descent test flight. Arranged in an "X" configuration, the grid fins control the descending rocket's lift vector to enable a much more precise landing location.[41]
            a large floating landing platform in order to test pinpoint landings prior to receiving permission from the US government to bring returning rocket stages into US airspace over land. In the event, SpaceX built the Autonomous spaceport drone ship in 2014,[42] and intends to conduct an initial flight test and landing attempt in January 2015.[43]
            large-surface-area thermal protection system to absorb the heat load of deceleration of the second stage from orbital velocity to terminal velocity[30][44]

    --

    Today's vices may be tomorrow's virtues.

  21. Re:Meanwhile the UFOs are flying everywhere by Anonymous Coward · · Score: 0

    P.S.

    @the person who started spouting vulgarities

    Quality video also helps guard against forgeries BY conspiracy theorists who, after all, are known to stretch things in the name of getting more coverage.

    Since a good artist can cook up anything they want with Blender and Photoshop, make an effort. Make it seem like Photoshop skills of level 9000 would be needed... pfft.

    Either way, I'll watch the rest of your crummy videos and comment on what I see.

  22. Re:Reinventing the wheel -- Am I missing something by Anonymous Coward · · Score: 0

    If you are referring to the space shuttle: yes that could land, but needed a very expensive 3 month re-build, and the boosters where recovered, but never re-used.

    SpaceX is aiming for not much more than refueling, with an turnaround in hours. There current rockets are all designed AND build as reusable, but at a price that makes them very competitive, even when reserving a lot of fuel for testing landing, but not yet re-using anything.

  23. Re:Meanwhile the UFOs are flying everywhere by Anonymous Coward · · Score: 0

    General impression? Video resolution sucks. Blurry, low-resolution, unfocused... ultimately pointless.

    video 4: go figure, at least the speck of light accelerates nicely, unfortunately it's a few pixels across, so don't expect me to call it alien

    video 5: video is hand-filmed, unable to identify floating object due to lack of focus and resolution, if video is authentic I would guess a detached piece of the station or a leaving cargo ship, by the way you said they cut live feed, well they obviously didn't, since it's manually filmed... a crew member would be filming an occasion of interest, especially if they knew in advance of when to look for it

    video 6: video lacks both context and any resemblance of clarity, there is no way to tell whether it was taken in space or in a clouded fish tank, way to go

    video 7: where for fucks sake is the damn UFO?

    video 8: an incredibly small video artifact is indeed visible, sorry, it could be anything, I don't declare "aliens" when I see stuff like that

  24. There is Spacecraft Software Workshop ... by Anonymous Coward · · Score: 0

    There is a spacecraft software workshop called the Workshop on Spacecraft Software ... The SpaceX guys should attend it. It was held at Caltech last year (in December) and I heard it was really good.

    Website is www.flightsoftware.org ...

  25. Re:Twitter: Ran out of Hydralic fluid by Wraithlyn · · Score: 1

    Telemetry by its very definition is transmitted to a remote monitoring station... the word literally means "remote measure". They didn't have to "recover" it (like a physical airplane flight data recorder or something).

    --
    "Mind, as manifested by the capacity to make choices, is to some extent present in every electron." -Freeman Dyson
  26. what about a net? by DeBaas · · Score: 2

    Honest question, I'm no rocket scientist so I really don't know: Since they seem to be able to hit the mark, why not just put a big net on the drone ship to 'catch' it rather than try to land it on legs?

    --
    ---
    1. Re:what about a net? by Anonymous Coward · · Score: 0

      Simply because the hardware is too fragile to fall over. It buckles and ruptures due to the non-controlled fall.

    2. Re:what about a net? by Anonymous Coward · · Score: 0

      I thought the same thing, but if your using a net, then that means you using parachutes and if your using those then your landings are not going to be precise. The idea of a controlled landing actually is easier and cheaper. Its suffering the same stress's maintains the same flight orientation, everything it was designed and engineered to do, except in reverse.

      I really hope they get approval for land based landings...

    3. Re:what about a net? by Anonymous Coward · · Score: 0

      - The net would have to withstand the landing burn (4000 Kelvin exhaust or so), or catch the stage at 150m/s (approx 300mph) terminal velocity
      - the tipping over stage will probably expierince enough bending forces that it will be bent before it is horizontal
      - the net would be HUGE. think 100x100 meter, and another 50m-100m or so for vertical dampening
      - a dozen other problems

      A better idea is using a hook on top of the stage and a rope. But alone the structural reinforcements to the stage makes this idea infeasible.

      Have a look at nasaspaceflight.com. I'm also an armachair rocket scientist and learnt a lot there. Just be carfull with questions involving nets and ropes :)

    4. Re:what about a net? by jaa101 · · Score: 1

      These rockets are really big. The square/cube means that big things are not as strong as little ones. Get two toy cars and smash them into each other. Now try the same thing with two full sized vehicles and compare the results. Sure you could catch a model rocket with a butterfly net and it will fly again. This idea just doesn't scale up.

    5. Re:what about a net? by Anonymous Coward · · Score: 0

      Because it wants to land standing up, and falling over in a net is probably about as bad as falling over in the ocean. And then you'd be looking at a metal net (that won't burn/melt from the rocket firing over it), and have to start wondering about stuff the net is contacting (fins, etc).

      I would say you would have to have an active capture system on the ship to avoid the need for landing gear, which actually might not be that unreasonable (you could eliminate landing gear and just have some attachment points) but would be a lot of engineering that might not really be needed and better spent elsewhere. Besides, any landing screw up could destroy another chunk of expensive equipment then.

    6. Re:what about a net? by Anonymous Coward · · Score: 0

      Because they was unsure if they would hit the mark. Since they have to rocket burn to slow down either way, why not rocket burn to slow down enough to land on legs which are basically just there to stabilize it. A net would just make recovery slower and is also more complicated then you would think in that:

      - has to be strong enough to handle the rocket burn
      - big enough enough to keep the rocket from tilting, which would cause damage thanks to gravity
      - as before, would have to close up the net upon landing to wrap the rocket preventing it from falling, meaning it would either have to be placed really high into the air (which has it own set of complications) or some mechanical way to tighten the net in conjunction with the rocket.

      Basically, landing on legs is more beneficial while the complexity of having a net is not necessarily being simpler.

    7. Re:what about a net? by Anonymous Coward · · Score: 0

      Because the final objective is mars.

    8. Re:what about a net? by Anonymous Coward · · Score: 0

      My guess would be that the rocket stage is so heavy that a net would either break or have about as much elasticity in it as a concrete floor does. Another possible problem is that bouncing around in the net might subject the rocket stage to impacts from the side (e.g. if it comes down at a 45 degree angle) that the rocket would have to be built to withstand and that might add too much weight to the rocket. The bouncing around might also damage components inside the rocket, like people (imagine what would happen if we landed planes in nets and the plane bounces around). The net itself might also need to be repaired quite often and the point of this is for the whole thing to be reusable. Soft landing on legs seems like the best option for something that's supposed to be almost immediately reusable after landing - if it can be done, and it looks like they thing they're close.

    9. Re:what about a net? by cbhacking · · Score: 1

      The most expensive part of the first stage (which itself is the most expensive part of the stack) is the rocket motors. You don't want those landing on *anything*, including a net. The legs are intended to keep the motors well off whatever surface you land on.

      Also, the rockets are firing on descent (both for slowing and for maneuvering). There's a final braking burn right at landing. Any net that can survive this braking burn is probably tougher stuff than you want the rocket running into even at relatively miniscule speeds.

      --
      There's no place I could be, since I've found Serenity...
    10. Re:what about a net? by Khan+Fused · · Score: 1

      I imagine a net light enough to be stretched across a football field sized target, yet strong enough to catch a 14 story building falling out of the sky, would be its own level of engineering/material science marvel.

      --
      This mind intentionally left blank.
  27. Re:Twitter: Ran out of Hydralic fluid by Enigma2175 · · Score: 1

    Elon Musk @elonmusk "Grid fins worked extremely well from hypersonic velocity to subsonic, but ran out of hydraulic fluid right before landing."
    "Upcoming flight already has 50% more hydraulic fluid, so should have plenty of margin for landing attempt next month."

    That's odd, does anyone know why it would run out of hydraulic fluid? Usually a hydraulic system is a closed loop, are they constantly dumping hydraulic fluid from this stage?

    --

    Enigma

  28. It is very difficult to understand by Anonymous Coward · · Score: 0

    that in the era of 3D printers that pay for themselves in a year, why anyone would go with the 1970s concept of reusing a rocket.

    Just keep 3D printing new ones. The more you 3D print, the cheaper it gets, Luddites.

    1. Re:It is very difficult to understand by Anonymous Coward · · Score: 0

      I am 3D printing my model rockets, you insensitive clod -- nozzles and all, just a little bit of clay needs to be added for thermal protection...

  29. Re:Twitter: Ran out of Hydralic fluid by Kjella · · Score: 5, Informative

    Not an official reply but answered on Twitter:

    Chris (Robotbeat) @Robotbeat 3h3 hours ago
    @dtarsgeorge @rocketrepreneur In aerospace, hydraulics are pressurized with gas (no pump) and no return lines. Pretty standard, actually.

    --
    Live today, because you never know what tomorrow brings
  30. And you believe the BS story??? by Anonymous Coward · · Score: 0

    Do you know what hydraulic fluid is or have any clue on how it is used??

    Sorry but that story is pure BS. The only way hydraulic fluid can be "used / lost" is if the vehicle had a major rupture in a hydraulic fluid line ... and that will affect the landing gear (only item that can potentially use hydraulic fluids).

    1. Re:And you believe the BS story??? by swillden · · Score: 2

      The only way hydraulic fluid can be "used / lost" is if the vehicle had a major rupture in a hydraulic fluid line

      True only if the hydraulic system is closed. Apparently that's not the way it's done in rocketry: "Chris (Robotbeat) (see robotbeat@ comment).

      and that will affect the landing gear (only item that can potentially use hydraulic fluids)

      The grid fins are hydraulically actuated.

      --
      Note to ACs: I usually delete AC replies without reading them. If you want to talk to me, log in.
  31. Re:Reinventing the wheel -- Am I missing something by Anonymous Coward · · Score: 0

    Sorry to burst your bubble. Other countries (ie: Russia) have already done a barge landing successfully .... but abandoned the idea because it wasn't cost effective.

  32. Re:Reinventing the wheel -- Am I missing something by swillden · · Score: 1

    Sorry to burst your bubble. Other countries (ie: Russia) have already done a barge landing successfully .... but abandoned the idea because it wasn't cost effective.

    Not of a first stage.

    --
    Note to ACs: I usually delete AC replies without reading them. If you want to talk to me, log in.
  33. Re:Twitter: Ran out of Hydralic fluid by Anonymous Coward · · Score: 0

    There was that launch last year where they received the telemetry using a jury-rigged pizza pan antenna pointed out the window of an airplane. The telemetry data was OK but the onboard video was garbled.

  34. Re:Twitter: Ran out of Hydralic fluid by Anonymous Coward · · Score: 1

    They're using the fuel/oxidizer as their source of hydraulic fluids.

    Propellants are fed via a single shaft, dual impeller turbo-pump. The turbo-pump also provides high pressure fluid for the hydraulic actuators, which then recycles into the low pressure inlet. This eliminates the need for a separate hydraulic power system and means that thrust vector control failure by running out of hydraulic fluid is not possible. A third use of the turbo-pump is to provide power to pivot the turbine exhaust nozzle for roll control purposes.

    Ironically, they didn't have a thrust vector control failure, but a control surface failure... by running out of hydraulic fluid. I think they'll dial it in for the next one, though.

  35. Re:Twitter: Ran out of Hydralic fluid by dunkelfalke · · Score: 1

    Aren't hydraulics that are pressurised with gas actually pneumatics?

    --
    "It's such a fine line between stupid and clever" -- David St. Hubbins, Spinal Tap
  36. Re:Twitter: Ran out of Hydralic fluid by frank249 · · Score: 1

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

    --

    Today's vices may be tomorrow's virtues.

  37. Re:Twitter: Ran out of Hydralic fluid by Anonymous Coward · · Score: 0

    I don't think so it uses the pressurized gas to push the hydraulic fluid instead of pressurizing it with a pump (which would need power, add mass and require fluid lines back to close the loop). in a pneumatic system, there wouldn't be any oil pumped through to the actuators, it would just be gas

    it's all about compression ... http://en.wikipedia.org/wiki/Pneumatics#Comparison_to_hydraulics

  38. Re:Twitter: Ran out of Hydralic fluid by Mal-2 · · Score: 1

    Not when the gas stays in the tanks (at least until the liquids run out) and the liquids do the actual work.

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  39. Re:Twitter: Ran out of Hydralic fluid by jklovanc · · Score: 1

    No. By that theory hydraulics that are pressurized by a pump should be called mechanicals. They are called hydroponics because fluid is used to move actuators. It does not matter what produces the pressure.

  40. Re:Reinventing the wheel -- Am I missing something by Anonymous Coward · · Score: 0

    So they landed a second or third stage for the hell of it??? Are you really that ignorant??

  41. Reply by Musk - This is an open loop system. by robbak · · Score: 1

    @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.

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  42. Re:Reinventing the wheel -- Am I missing something by Anonymous Coward · · Score: 0

    Citation. Put up or shut up.

  43. Actually it was a MAJOR partial SUCCESS ! by macpacheco · · Score: 2

    There were two goals far more important than actually recovering the first stage:
      1 - Having the stage navigate to the landing pad. It would have been a major failure if the rocket landed 2 miles away and were fished out of the water.
      2 - Not destroying the landing barge (its worth far more than the first stage, and it would take a few months to prepare another one).
    Additionally, in less than 24 hrs SpaceX already knows what went wrong, have a fix for it, and intends to try again on the next launch (about 3 weeks from now, end of scheduled for January).
    So, calling it a failure is like saying this glass is 10% empty !
    SpaceX has already managed to have the rocket hover for a second or two meters from water, but back then there were no precision in where the rocket was aiming to splash. The difference is many changes were made to the rocket to steer it.
    SpaceX might have a dozen shots at trying this in 2015 alone.

  44. Re:Twitter: Ran out of Hydralic fluid by Anonymous Coward · · Score: 0

    Only if the actuator fluid is the gas itself. If the gas is just being used to pressurize the hydraulic fluid, then they are hydraulics.

  45. Re:Reinventing the wheel -- Am I missing something by swillden · · Score: 1

    So they landed a second or third stage for the hell of it???

    AFAIK, they've only landed a capsule. If you have a citation showing something else, I'd love to see it.

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  46. Re:Twitter: Ran out of Hydralic fluid by Anonymous Coward · · Score: 0

    It can be water that's being pressurised with gas...

  47. Re: So far, SpaceX is still at 60% rate of failur by Anonymous Coward · · Score: 0

    Lying troll.

  48. Re:So far, SpaceX is still at 60% rate of failure by Teancum · · Score: 1

    [citation needed]

    Really, this is just utter troll talk here that shows you don't know what you are talking about. That SpaceX keeps pushing the envelope is true, but they've definitely delivered payloads to the desired location in orbit on multiple occasions, including 100% of the primary payloads on the Falcon 9. That they might have set some additional goals on each mission to go beyond the bare minimum expected and then fail on some minor point only goes to show that they aren't trying to stay safe either.

  49. Re:Reinventing the wheel -- Am I missing something by Teancum · · Score: 1

    There was the DC-X program that tried to do mostly the same thing that SpaceX is doing here with this barge landing, but the DC-X never made the trip into orbit and only did pretty much what the Grasshopper did earlier. The DC-X was supposed to lead to a rocket that went into orbit and could be similarly reusable, but funding for that program was cut during the Reagan administration. Surprisingly, it is Blue Origin that purchased all of the IP rights to that technology and not SpaceX... but that is another story.

  50. Re:Reinventing the wheel -- Am I missing something by swillden · · Score: 1

    The AC's claim was that "other countries (ie: Russia) have already done a barge landing successfully". As I understand it, Russia has landed capsules, but on land not on a barge, and nothing as big and difficult to control as a first stage.

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  51. Proof by Anonymous Coward · · Score: 0

    Falcon failed to land as designed. This proves that science is fallable and that climate change is false.

  52. Re:Reinventing the wheel -- Am I missing something by Teancum · · Score: 1

    I agree that the AC was simply showing a lack of knowledge about the topic. Russia is the world leader in propulsion technology (the next generation engine called the Raptor that SpaceX is building is based upon Russian technology), so I wouldn't dismiss Russia at all in terms of spaceflight technology on any level. None the less, there have been some other attempts by people other than SpaceX to get a reusable flight vehicle to do a controlled landing.

    There are also some scholarly papers that have attempted to prove that what SpaceX is doing here is technologically impossible as well, trying to demonstrate that reusable systems for stage recovery will eat up all of the payload mass making such a rocket useless on a practical level. I believe some Russian propulsion scientists were involved in one of those papers that included some hardware tests. Seeing a rocket stage successfully deliver a payload to the ISS of several metric tons of cargo and land in a near-miss but for the want of a couple gallons of hydraulic fluid sort of shows that those papers might not be entirely accurate or at least there might be ways to reduce the mass of such recovery systems and still deliver a practical payload into orbit.