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Space Businesses Technology

Fourth SpaceX Rocket Successfully Landed on A Drone Ship (theverge.com) 71

Saturday a SpaceX rocket completed the company's fourth successful landing at sea (watched by over 100,000 viewers on YouTube and Flickr). Saturday's landing means Elon Musk's company has now recovered more than half the rockets they've launched. An anonymous Slashdot reader quotes Saturday's report from The Verge: Tonight's landing was particularly challenging for SpaceX... The Falcon 9 had to carry its onboard satellite -- called JCSAT-16 -- into...a highly elliptical orbit that takes the satellite 20,000 miles out beyond Earth's surface. Getting to GTO requires a lot of speed and uses up a lot of fuel during take off, more so than getting to lower Earth orbit. That makes things difficult for the rocket landing afterward...there's less fuel leftover for the vehicle to reignite its engines and perform the necessary landing maneuvers.

CEO Elon Musk said the company is aiming to launch its first landed rocket sometime this fall...SpaceX's president, Gwynne Shotwell, estimates that reusing these landed Falcon 9 vehicles will lead to a 30 percent reduction in launch costs.

SpaceX named their drone ship "Of Course I Still Love You."
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Fourth SpaceX Rocket Successfully Landed on A Drone Ship

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  • by kaalon ( 2861517 ) on Sunday August 14, 2016 @11:44AM (#52699893)
    Once SpaceX starts flying those "used" cores it will push the whole industry of space flight to the same level of reuse. We are going to see some great advances in engineering coming from all over the world as others start to catch up to SpaceX.
    • Once SpaceX starts flying those "used" cores it will push the whole industry of space flight to the same level of reuse. We are going to see some great advances in engineering coming from all over the world as others start to catch up to SpaceX.

      No, I'm afraid it isn't. Getting into space isn't going to move forwards meaningfully until we get a single stage to orbit vehicle. SpaceX don't even have the closed cycle rocket engines the Russians have had for years, and are trying to get banned by the way, but this isn't going to be done with rockets in the form we have had for decades.

      • No, I'm afraid it isn't. Getting into space isn't going to move forwards meaningfully until we get a single stage to orbit vehicle.

        To qualify this a bit further, any vehicle that tries to continue to carry expensively heavy liquid oxygen around when there is an abundance of oxygen in the atmosphere just isn't going to be viable for single stage to orbit. It has to breathe air for as long as it can.

        • This is completely ignorant. A fully-reusable multi-stage system (which is essentially the goal of SpaceX) expends nothing but fuel and oxidizer ... and your SSTO is better than that HOW?

          Functional SSTO will probably eventually happen, but for anyone who knows anything, the most likely scenario is that improvements in engineering and materials science will render most use cases for SSTO moot. With better (lighter, stronger) materials, efficiency and lift capabilities for reusable multi-stage vehicles skyro

          • This is completely ignorant. A fully-reusable multi-stage system (which is essentially the goal of SpaceX) expends nothing but fuel and oxidizer ... and your SSTO is better than that HOW?

            You haven't the slightest idea what you are talking about..........as most don't. Multi-stages are always going to require more maintenance and complexity.......and carrying around heavy oxygen is expensive, which I'd explained........if you'd bothered to read and comprehend. You just aren't going to hack it with rockets I'm afraid, and anyone faffing about with them still after fifty plus years just isn't doing anything interesting I'm afraid, despite the whooping and hollering.

            Functional SSTO will probably eventually happen, but for anyone who knows anything, the most likely scenario is that improvements in engineering and materials science will render most use cases for SSTO moot.

            Wow.

      • by khallow ( 566160 )

        Getting into space isn't going to move forwards meaningfully until we get a single stage to orbit vehicle.

        I strongly disagree. On a single stage to orbit (SSTO) you have to carry everything with you. Your engines have to operate near optimally in atmosphere and vacuum (while a staged rocket can use different nozzle designs for the first and later stages, and get near optimal performance without requiring a complex system for changing the nozzle and inlet geometries and/or burn characteristics on the fly).

        You further elaborated in a reply:

        To qualify this a bit further, any vehicle that tries to continue to carry expensively heavy liquid oxygen around when there is an abundance of oxygen in the atmosphere just isn't going to be viable for single stage to orbit. It has to breathe air for as long as it can.

        That means greatly increased air resistance right when you're trying to

    • by eth1 ( 94901 )

      Once SpaceX starts flying those "used" cores it will push the whole industry of space flight to the same level of reuse. We are going to see some great advances in engineering coming from all over the world as others start to catch up to SpaceX.

      Another interesting thing that might result from reuse: I keep hearing people say, "who would risk their expensive cargo on a used booster?" I wonder if it won't actually turn out that the second, and maybe even third flights of a given booster prove to be more reliable than the first. (basically natural selection rocket-style)

      • by tsotha ( 720379 )
        That's really the $68,000 question. I wouldn't fly on the first test flight of a brand new commercial airliner, and that's essentially what satellite makers are doing with disposable rockets. But airliners don't take the same punishment as rocket boosters. Nobody really knows if we can build a booster that can fly over and over reliably enough to be, well, relied upon. Maybe SpaceX has already done it with Falcon 9. Maybe the amount of inspection and refurb necessary between flights makes the whole thi
  • by fahrbot-bot ( 874524 ) on Sunday August 14, 2016 @11:49AM (#52699911)

    Getting to GTO requires a lot of speed and uses up a lot of fuel during take off, more so than getting to lower Earth orbit. That makes things difficult for the rocket landing afterward...there's less fuel leftover for the vehicle to reignite its engines and perform the necessary landing maneuvers.

    Does anyone know (or can point me to doc) about how the Falcons perform their descents. Is it powered / controlled the entire time, or parachute (or para-*somehing*) and just powered / controlled near the ground. I imagine the fuel requirements would be different.

    • Re: Less fuel. (Score:5, Informative)

      by Anonymous Coward on Sunday August 14, 2016 @11:59AM (#52699941)

      They slow down mostly through aerodynamic drag. No chute or similar device. The rockets only come on in the last 20 seconds or so to do the final braking.

      During reentry the first stage uses the rocket bells as a heat shield, and during the worst part of it they burn three engines to literally push the atmosphere out of the way "entry burn" to ease the heating until it gets down into the lower atmosphere where drag can slow it. For the ship landings, those are the only two burns, total less than 60 seconds with only 3/1 engines firing.

    • Re:Less fuel. (Score:5, Informative)

      by queazocotal ( 915608 ) on Sunday August 14, 2016 @12:01PM (#52699949)

      The first stage and the second stage disconnect.
      The first stage flips around end to end, and makes a burn to kill most of its velocity.
      Then as it is entering the thicker parts of the atmosphere and it would be destroyed by drag and heating otherwise, rapidly slows at high G using the engines to around mach 1, and turns the engines off.
      It is at this time steering using fins attached to the top of the rocket.
      Once it gets ~10-20 seconds before landing, it lights an engine or three (details vary) and uses the thrust from these vectored in order to precisely land on the barge (along with the fins in the initial portion).

      http://www.spacex.com/sites/sp... [spacex.com] is a nice diagram.

      • Thanks very much! The graphic was very helpful.

        Would a parachute, or more to the point, some type of steerable / controllable drag component deployed during part of the descent help or hurt?

        • by Anonymous Coward

          Since SpaceX wants to land its rockets on Mars eventually, which has a thin atmosphere, they prefer to practice with landing by rocket-engine.

          • Re:Less fuel. (Score:5, Insightful)

            by Gavagai80 ( 1275204 ) on Sunday August 14, 2016 @05:27PM (#52701197) Homepage

            More importantly, parachutes have no precision and are subject to the wind.

            • by Ocker3 ( 1232550 )
              The problem with Mars is actually that the atmosphere is too thin to use parachuts, no matter how large, to land anything of size enough to be useful to use for serious exploration or human visits. The Mars Landers pushed the limits of what we could put on the surface without using retrorockets.
        • Re:Less fuel. (Score:5, Informative)

          by Anonymous Coward on Sunday August 14, 2016 @02:28PM (#52700463)

          It has 4 (not 8) grid fins, small cold gas thrusters, and gimbaled engines, all controlling the rocket. They experimented with parachutes (dropping in the ocean instead of of landing on a ship) but never managed to slow down enough to make them work. It's hitting the outer atmosphere at about 2km/second! The has several problems, for example the rocket spinning up in the airflow centrifuging the remaining fuel to the side of the tank, so engines would stop, the steering find moving more than expected and running out of hydraulic fluid just before landing, etc. Even when practicing powered "landing" on the ocean surface before they had a landing ship, the did not even recover small parts because the rocket would be destroyed by waves and sink before they could get to it. The nearly empty first stage is also lighter than the minimum thrust of one of the 9 engines, so if the landing burn is started too early, it will be going back up before reaching zero altitude. Too late, and it will not have stopped before reaching zero altitude. There also has been a problem with one leg not locking into place and toppling over after landing. They now cool the RP-1 (kerosene) to -6C and the liquid oxygen to 50 degrees above absolute zero to make them denser, to get more performance out of the rocket without making the tanks bigger. This makes launch timing very critical since fuel needs to be pumped into the rocket very fast just before launch, without freezing pipes and quickly heads up while in the rocket where it can't be cooled and can't fit in the tank if warmed up. (boil-off only cools it to the boiling point of oxygen which is already to warm to fit in the tank). beginning 2017 SpaceX will start testing a version with 3 of these rockets connected, with all 3 cores landing separately, 2 on land, and the middle on on the ship in the ocean. Next month, SpaceX will present there plans for an even bigger rocket, that will fly to will fly to Mars, land on Mars, re-fuel, fly back to earth and land again, and also be fully reusable.

        • by tomhath ( 637240 )
          At high altitude a parachute or something similar would burn up. At lower altitudes the terminal velocity is such that it's not needed.
        • Their earliest recovery attempts involved parachuting stages into the ocean unpowered. All those attempts apparently resulted in the vehicle breaking up during reentry. Large supersonic parachutes are very non-trivial to design and deploy, not terribly reliable at the best of times, and are actually rather heavy, and they needed to do powered reentry and landing anyway to get the vehicle down intact. Since they're already doing that, reserving a bit more propellant is simpler than pretty much any other opti

    • Re:Less fuel. (Score:4, Informative)

      by Anonymous Coward on Sunday August 14, 2016 @12:08PM (#52699973)

      At the top of it's trajectory, it is out of the atmosphere. As it is about to hit the atmosphere, it burns with three engines for about 20 seconds so that hitting the atmosphere doesn't shred the rocket. It then lets atmospheric drag slow the rocket the rest of the way. It controls its direction with aerodynamic surfaces called grid fins during this phase. Finally, as it approaches the landing platform, it does a one engine burn so that its velocity hits zero at the precise moment when the legs touch down.

      The idea is to use the atmosphere to do most of the work slowing down the rocket. However, it needs to not be destroyed entering the atmosphere at velocities that are too high, nor be destroyed hitting the barge at terminal velocity. So engines are used in those two phases.

    • by jfdavis668 ( 1414919 ) on Sunday August 14, 2016 @04:23PM (#52700989)
      This is the view from the rocket as it descends and lands: https://www.youtube.com/watch?... [youtube.com]
    • by idji ( 984038 )
      You can watch a landing from the lander perspective and see yourself when the burns happen. https://www.youtube.com/watch?... [youtube.com]
  • Numbers... (Score:5, Insightful)

    by cjameshuff ( 624879 ) on Sunday August 14, 2016 @02:05PM (#52700383) Homepage

    The numbers in the summary are a bit ambiguous/confused:
    This was the *sixth* rocket they've landed. They've landed four on drone ships and two on land. That's nowhere near half the rockets they've launched (this was the 28th Falcon 9), but means just over half of their landing attempts (11 total) have succeeded.

    More importantly, of the last 7 landing attempts, there were only two failures, both due to simple lack of propellant margin due to the demands of those particular launches...there weren't any failures or control problems, they just ran out of propellant. The last actual hardware failure was flight 21, the Jason-3 launch, which actually landed fine, but had an earlier version of the legs which iced up and failed to lock in the extended position. So it's looking like reliability of future landings can be expected to be quite a bit better than 50%.

    All without any nets/cables/tubes/funnels/magnets/giant catcher's mitts.

    • by tomhath ( 637240 ) on Sunday August 14, 2016 @03:44PM (#52700831)

      This was the *sixth* rocket they've landed.

      Well, they landed all of them. Some landings were harder than others.

      • by Anonymous Coward

        Now you're just spreading RUD.

    • Have to admit I haven't followed the details too closely, but I vaguely remember reading that the two failed attempted landings came as a result of a lack of hydraulic fluid in actuators. Apparently there is no recycling of hydraulic fluid in the first stage, because calculations showed that it was more sensible to have a small tank with fluid than have a recirculating system with a pump.

      IIRC, the issue was that the 1st stage simply ran out of hydraulic fluid, resulting in a loss of ability to control th
      • It was only once that they ran out of hydraulic fluid, they fixed that the next flight. Sticky engine gimbal caused another crash. The engine pivots to help steer it for landing, but it was moving too slowly, so they landed at an angle instead of vertical. Finally, one time a landing leg failed to lock. So it landed vertical, but then fell over. They have been learning by crashing, and generally don't have the same problem twice. Since expendable rockets *always* crash, flight testing the landing syst

        • The very first ASDS landing attempt ran out of hydraulic fluid for the grid fins, the engine gimbaling barely managing to get it to the barge...not upright and not at zero velocity.

          The next had a sticky valve...my understanding is it was actually for throttle. The control software would command throttle changes, but the valve wouldn't respond until the commanded change was big enough to break it loose, then it'd stick at the new position. The overall effect was that the throttle was lagging behind what the

          • by tsotha ( 720379 )
            In the "making it work better" vein, they've been experimenting with different reentry attitudes and burns in recent flights. They said they were trying to bleed off more speed in the upper atmosphere to save fuel for the landing. Perhaps they've succeeded, too: on this flight they went back to the single engine landing, which requires more fuel but is easier on the hardware.
          • by ytene ( 4376651 )
            And the single most AMAZING thing about all of this is that they rarely seem to have the same problem twice. The ability of SpaceX to learn from mistakes and solve every problem, properly, is not just good for the space industry, it's remarkable in pretty much any field of endeavour. Sheesh, if the developers where I work got their software bugs ironed out after the first round of testing, they spend 11 months of the year on a beach and still be more productive...

            ;)

            I don't understand why people knock
    • Re: (Score:2, Interesting)

      by Kjella ( 173770 )

      More importantly, of the last 7 landing attempts, there were only two failures, (...) So it's looking like reliability of future landings can be expected to be quite a bit better than 50%.

      Most importantly, none have flown again and until they do it's expensive garbage recovery. For what it's worth I heard they did engine tests and it looks good, but it's more important they nail the launches than the landings.

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