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In Daring Plan, Tomorrow SpaceX To Land a Rocket On Floating Platform

HughPickens.com writes "The cost of getting to orbit is exorbitant, because the rocket, with its multimillion-dollar engines, ends up as trash in the ocean after one launching, something Elon Musk likens to throwing away a 747 jet after a single transcontinental flight. That's why tomorrow morning at 620 am his company hopes to upend the economics of space travel in a daring plan by attempting to land the first stage of a Falcon 9 rocket intact on a floating platform, 300 feet long and 170 feet wide in the Atlantic Ocean. SpaceX has attempted similar maneuvers on three earlier Falcon 9 flights, and on the second and third attempts, the rocket slowed to a hover before splashing into the water. "We've been able to soft-land the rocket booster in the ocean twice so far," says Musk. "Unfortunately, it sort of sat there for several seconds, then tipped over and exploded. It's quite difficult to reuse at that point."

After the booster falls away and the second stage continues pushing the payload to orbit, its engines will reignite to turn it around and guide it to a spot about 200 miles east of Jacksonville, Florida. Musk puts the chances of success at 50 percent or less but over the dozen or so flights scheduled for this year, "I think it's quite likely, 80 to 90 percent likely, that one of those flights will be able to land and refly." SpaceX will offer its own launch webcast on the company's website beginning at 6 a.m. If SpaceX's gamble succeeds, the company plans to reuse the rocket stage on a later flight. "Reusability is the critical breakthrough needed in rocketry to take things to the next level."
SpaceX announced the plan in December.

151 comments

  1. Deja Vu by AbsoluteXyro · · Score: 1

    Weren't we reading these exact same headlines at nearly the same time last month? What happened?

    1. Re:Deja Vu by Spy+Handler · · Score: 4, Informative

      delayed. Rocket launches get delayed often. If you're new to this, get used to it.

      Stratolaunch does kind of makes sense from the delay perspective, if we're gonna aim at something like daily orbital launches in the future (although of course in this case, the delay wasn't weather-related). Jets are much more tolerant of bad weather than rockets, so being able to fly above the weather or move away from it is pretty appealing.

    2. Re:Deja Vu by OzPeter · · Score: 2

      And the Skylon is looking to build a genuine spaceplane, single stage to orbit, with its funky jet/rocket combined engines,

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    3. Re:Deja Vu by 0123456 · · Score: 1

      And the Skylon is looking to build a genuine spaceplane, single stage to orbit, with its funky jet/rocket combined engines,

      Trouble is, from the numbers I've seen it won't cost much less per pound to orbit than a reusable Falcon, but will cost many times more to develop than a resuable Falcon. The high development cost of SSTOs is why Musk is far more likely to be the one who slashes the cost of getting things into orbit. Obviously, at some point, the cost of recovering and reassembling the stages becomes such a high proportion of the cost of a launch that SSTO will start to make sense.

    4. Re:Deja Vu by cjameshuff · · Score: 1

      That's often cited as an advantage, but jets that have to take off and potentially land (in the case of an abort) while carrying extremely heavy, hazardous, fragile, billion-dollar payloads are not particularly tolerant of bad weather.

      Rockets can be *more* tolerant due to their excess of power, rapid ascent, and lack of large aerodynamic surfaces, but rocket operators have been far more risk averse due to the cost of failure. Even so, they've launched in conditions such as heavy snow that might have grounded a carrier aircraft.

    5. Re:Deja Vu by Megane · · Score: 1

      The launch got delayed to the point where not only were the holidays (Christmas/New Year) coming up, but at the same time, the ISS orbit (remember, this is primarily an ISS service launch) was in a "high beta" period where it got more sunlight than normal, which would have been a higher thermal load on the Dragon capsule.

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    6. Re:Deja Vu by Anonymous Coward · · Score: 0

      the point of OzPeter mentioning skylon was in conjunction with the guy talking about not scrapping launches due to weather and a space plane is theoretically less susceptible to inclement weather than a rocket is. (I mean, assuming either of the grand parent posters are right)

    7. Re:Deja Vu by 0123456 · · Score: 1

      Not really. One shuttle launch I attended was cancelled due to bad weather in Africa, because it would have gone splat if it had to abort and tried to land there. Many landed in California because the weather was too bad to land at KSC, and you only got one chance to land or go splat.

      I don't remember how Skylon is supposed to work, but every pound of excess fuel carried to allow it to abort a landing and try again is a pound less it can carry to orbit. And its payload capacity is already small.

    8. Re:Deja Vu by david.given · · Score: 1

      A rocket ought to be fairly resistant to bad weather --- they have many more times the control authority that an aeroplane has, due to sodding huge engines, and will be above it very quickly. They already have to deal with very strong winds blowing them sideways as they pass through the jetstream (at 100km/h plus), and they don't have air intakes to suck in rain.

      Does anyone know whether the Falcon 9 can't take off in bad weather, or whether they won't do a launch in bad weather because they'll lose visual contact with the vehicle, which is critical for monitoring the performance of what is fundamentally a prototype?

    9. Re:Deja Vu by 0123456 · · Score: 1

      Does anyone know whether the Falcon 9 can't take off in bad weather, or whether they won't do a launch in bad weather because they'll lose visual contact with the vehicle, which is critical for monitoring the performance of what is fundamentally a prototype?

      Isn't it usually because the range safety entity has to be able to see where the rocket is to decide whether they should blow it up?

    10. Re:Deja Vu by beelsebob · · Score: 1

      The numbers I've seen say that Skylon will cost the same for the first launch. But in being completely reusable, and not needing to carry oxygen on the way up, will become orders of magnitude cheaper once you account for several launches per vehicle.

    11. Re:Deja Vu by beelsebob · · Score: 1

      Skylon works by scooping up the oxygen it will need for orbital flight while still in the atmosphere. Because the oxygen is about 95% of the launch mass that means you can launch with much much much less weight. Even if you need twice as much fuel to land again, you still have a craft that weighs 10% of the original.

    12. Re:Deja Vu by HornWumpus · · Score: 1

      Check your math.

      O atomic weight 16. H atomic weight 1. 16/18 = 88% of 'fuel' weight.

      But it still needs to carry O2 for burns above the atmosphere.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    13. Re:Deja Vu by Anonymous Coward · · Score: 0

      before a launch they test the engines for 3 seconds, the test lasted only a second, and later they were able to go the full 3 seconds but delayed the launch to avoid a ten day period when the ISS (thats the space station) was going to experience a thermal event (the sun shines on it for about ten days straight and they avoid docking during that time)...hence the delay to Jan 6. The event will be over for the Dragon to dock around the 7th pr 8th.

    14. Re:Deja Vu by Anonymous Coward · · Score: 0

      Ah, you have come to that stage where the mind now imagines a Slashdot dupe. At least you haven't imagined a first post to either one. There is still hope.

    15. Re:Deja Vu by Anonymous Coward · · Score: 0

      and you aren't bringing that with you back into atmo.

    16. Re:Deja Vu by Irate+Engineer · · Score: 2

      They want to maintain visual on the 1st stage. The aerodynamics of the high altitude, high Mach number deceleration burns is probably the most important thing they want to study. They need to understand this well for the present objective of controlling and landing the stage, but the aerodynamics is relevant to semi-powered descent of the Dragon spacecraft onto Earth and especially Mars.

      Here is some footage of their last landing attempt

      https://www.youtube.com/watch?v=_UFjK_CFKgA

      This is what SpaceX ultimately is aiming for - a spacecraft that can utilize drag and propulsion in varying proportion to land on any body in the solar system, no parachutes

      https://www.youtube.com/watch?v=Cf_-g3UWQ04

      --

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    17. Re:Deja Vu by Gavagai80 · · Score: 1

      The wiki says it'll be completely reusable within 2 days of landing because of ceramic tiles that protect it from the heat of re-entry. Sounds like a space shuttle. Doubtful that practice will work as well as theory.

      --
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    18. Re:Deja Vu by 0123456 · · Score: 1

      The numbers I've seen say that Skylon will cost the same for the first launch.

      I haven't been following Skylon for a few years, but the last claim I remember was around $100 per pound into orbit ($250 per kg? Or maybe it was $250 per pound?)

      Falcon Heavy is supposed to start around $1000 per pound, and around $100 per pound if and when it becomes fully reusable. So they're in the same ballpark, and probably both have a similar chance of actually making their cost predictions, but one won't cost $10,000,000,000+ to develop.

    19. Re:Deja Vu by Immerman · · Score: 1

      I don't know about other reasons, but I imagine they would be disinclined to take off in bad weather simply because even a slight increase in the risk of a launch failure translates to a high expected dollar loss. Lets say they estimate a 1 percentage point higher chance of a catastrophic failure during bad weather. The rocket alone is worth $55 million, multiply by 1% to find the expected loss per launch over time, that's $550,000 they should expect to lose, on average, every time they launch a rocket in bad weather. Businesses make those kinds of calculations all the time - it's basic cost/benefit analysis.

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    20. Re:Deja Vu by beelsebob · · Score: 1

      It doesn't need to carry it when it launches though - this is the big benefit. A huge amount of the fuel that rockets carry is for the sole purpose of lifting the fuel and oxydiser for everything after 20km up by 20km. That's when the rocket is heaviest, and when it's having to push through the thickets atmosphere, and when it's travelling slowest (yes, counter intuitively, rockets are more efficient the faster they travel).

      By not having to carry the oxygen for 20km onwards at launch time, you reduce the launch weight hugely, and in doing so enormously reduce the amount of fuel needed to lift that launch weight. Add to that that you don't need to carry the oxidiser for that fuel either, and you come in with an absolutely massive weight saving.

      You also get a space saving, because the oxygen that you pack in as you fly upwards can be packed into the space that the hydrogen you're burning used to take up. That space saving saves weight in the structure of the vehicle, and it saves aerodynamic drag. That's two more large savings there.

    21. Re:Deja Vu by cjameshuff · · Score: 1

      There is no space savings. You can't put oxygen in the hydrogen tank. In fact, Skylon has to carry extra hydrogen for cooling, and the extremely low density of liquid hydrogen makes it an enormous vehicle. This coupled with the need to stay in the atmosphere to breathe air vastly increases losses from aerodynamic drag...something that is actually almost insignificant for a non-airbreathing rocket (only around 100 m/s total, considerably less in some cases) becomes a major loss. There's also the little problem of the oxygen not moving along with the vehicle, it starts off with high relative motion in the direction you're trying to accelerate it in (and is also diluted heavily with nitrogen, and is in the form of low density gas that has to be compressed many times over...). Energy that goes into accelerating oxygen carried by a rocket isn't wasted, it gets that oxygen moving with the rocket so it can later produce full thrust when it is burned. And then there's all the extra structure and equipment that you have to carry to breathe air, which in the case of SSTO vehicles has to be hauled all the way into orbit, and that still has to be done mostly on pure rocket power.

      If you do the math, it turns out you need air breathing engines with extremely high thrust and lift surfaces with very high lift to drag ratios at hypersonic speeds (not typical characteristics of hypersonic engines and lift surfaces) in order to avoid having aerodynamic losses eat up all the specific impulse advantages of air breathing engines. The main thing you accomplish by breathing air in an orbital launch system is replacing dense, easily handled liquid oxygen with low-density, tricky liquid hydrogen and adding vast amounts of complexity to the system.

    22. Re:Deja Vu by cjameshuff · · Score: 1

      Skylon also launches with all the oxygen it needs to reach orbit, it does not extract oxygen from the air or store it for later use. Doing so would require even more machinery to extract and liquefy the oxygen, even more hydrogen to cool and power the machinery, etc.

    23. Re:Deja Vu by cjameshuff · · Score: 1

      If air breathing doesn't reduce the cost of the first launch, it won't reduce the cost of the second, and reuse works at least as well at reducing costs for Skylon's competitors. Actually considerably better for SpaceX and those who choose to take their approach, due to the efficiency gains of staging as well as a much less extreme reentry for the first stage (which constitutes the great majority of the vehicle).

  2. Re usability by Bruha · · Score: 1

    Even if they can recover the engine intact how many times can it be reused. Saving a few million on a higher chance of blowing up multi billion payloads is not exactly wise economically.

    1. Re:Re usability by trout007 · · Score: 3, Interesting

      Their engines are already reused "sort of". They test fire their engines before launch. One time they evens scrubbed a launch after the engines were lit. They fixed the problem in a few hours and launched after that.

      One of the reasons payloads cost multi-billion dollars is because the launchers cause near that amount. Cheaper launchers will lead to cheaper payloads..

      --
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    2. Re:Re usability by Rizgar · · Score: 1

      Yes, because something may go wrong in another approach the status quo is always better. Plus rocket reuse has not happened yet. No judgements until we try.

    3. Re:Re usability by steveg · · Score: 1

      That was the first thing that jumped to my mind. Kind of reminds me of retread tires -- a lot of the truck tire fragments you see by the side of the road are from retread tires that self destructed. A lot of companies buy them because they're cheaper, but the chances that they'll fail is far higher.

      But the consequnces of your first stage failing are much worse than the consequences of your tire shredding on the freeway. And those are bad enough.

      --
      Ignorance killed the cat. Curiosity was framed.
    4. Re:Re usability by Spy+Handler · · Score: 1

      depends. But in the case of SpaceX merlins, a lot. They were designed with reusability in mind and also they don't throttle it up to max capacity for longevity. What exactly is a lot? Nobody knows, not even SpaceX. They'll know after they try it a few times. But a dozen reuse doesn't seem unreasonable at this stage.

      Today most P-51 and Corsair owners don't use WEP (war emergency power) on their precious warbirds to save engine wear... same principle.

    5. Re:Re usability by Anonymous Coward · · Score: 0

      Gwynne Shotwell mentioned once that they expect that the engine can be cycled 40 times. It's not clear what a "cycle" is and whether it considers the stresses of atmospheric flight (very hot engines against very cold atmosphere, hypersonic flight) but hopefully they can be reused at least a few times.

      Not all payloads are multi-billion dollars, anyways. The military and other expensive payload customers could still buy new rockets, which could be cheaper if SpaceX knows that they can be reused a few times for customers using discount rockets.

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

      Almost makes me wonder if they could make them just that little bit tougher to begin with so they can last even longer when re-used, preventing the need to make new ones would save billions over the years.

      I still await the day that a multi-stage re-usable comes back, like the Shuttle.
      I've not been following Scramjet research for a while, but the last time I looked at it, it looked promising.
      Having the private industries get behind re-usability is a good thing, takes us one step closer to a fully space-faring society.
      This coupled with space-mining will hopefully bring a calm to the human race that we haven't seen since, well, ever.
      Or it will just go pear-shaped and there will be space battles and space piracy. Time for piracy!

    7. Re:Re usability by catchblue22 · · Score: 3, Informative

      Even if they can recover the engine intact how many times can it be reused. Saving a few million on a higher chance of blowing up multi billion payloads is not exactly wise economically.

      I have heard they have already put engines through 40 or more simulated launch cycles. These engines were designed to be reliable. To a certain extent, having tested an engine through previous launches might imply more reliability, at least up to a certain point. In any case, if they recover the rocket, they will be able to analyze how the launch has affected the structure and systems.

      These rockets do not use hydrogen, and thus do not have the problems of embrittlement that the shuttle engines had. I suspect one of the bigger problems will be coking from using kerosine fuel, but I also suspect that can be mitigated using solvents to clean the fuel systems.

      --
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    8. Re:Re usability by jythie · · Score: 2

      Long term that is what they will have to determine. Reuse of rockets has been a thing for a long time, but in most cases it ends up not being economically viable. Right now SpaceX has some very optimistic estimates regarding reuse and its associated costs, but so did NASA. It generally ends up being worse than they hope, but sometimes it still works out well enough. Though if they continue to move towards human cargo that will change the equation significantly.

    9. Re:Re usability by Garfong · · Score: 1, Informative

      Plus rocket reuse has not happened yet.

      Except by NASA from 1981-2011.

    10. Re:Re usability by Anonymous Coward · · Score: 0

      They re-used the SSMEs on each Shuttle Orbiter how many times each? Sure they were overhauled between flights, but that's cheaper than building a new engine each time.

      Besides, once out of the R&D phase, liquid rocket engines almost never blow up. Not the way solids do. If one starts to show a problem in flight you just shut it down and burn the others a bit longer.

    11. Re:Re usability by GTRacer · · Score: 1

      I thought the only rocket-related thing reused from the shuttles was the fuel tank, and that only after reconditioning it post-ocean swim.

      SpaceX wants to soft-land the whole first stage in a way that won't require a lot of reconditioning. If it works, it would be a different sort of thing than the shuttles.

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    12. Re:Re usability by itzly · · Score: 1

      Reuse of the shuttle took several months of costly refurbishing for each launch, though.

    13. Re:Re usability by Rizgar · · Score: 1

      McDonnell Douglas DC-X and stuff like that never really did payload. Plus sending scuba teams to retrieve components followed by massive refurbs are not what I consider truly reusable at least in the 747 analogy Musk keeps making. But I am willing to say all I do is read about this stuff and not work in that industry so I could just be misinformed.

    14. Re:Re usability by Anonymous Coward · · Score: 0

      Well, that and the orbiter.

    15. Re:Re usability by GTRacer · · Score: 2

      Though if they continue to move towards human cargo that will change the equation significantly.

      Honest question: You have a ticket to the ISS. You can choose a rocket that just came out of the VAB* or one that recently launched and returned whole and was turned around for this flight. Which do you trust more?

      * Yes, I know SpaceX isn't using the VAB now but you get the idea...

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    16. Re:Re usability by Isca · · Score: 4, Informative
      The fuel tank was destroyed every launch, it burns up shortly after it is jettisoned.

      The external solid boosters were sort of reused - the entire rocket needed to be disassembled, and about 5k parts were refurbished and reused. The shuttle engines themselves were pretty much the same thing, they were taken apart and refurbished every mission.

      SpaceX wants to only partially disassemble key components of their 1st stage in a way that they could potentially send up the same 1st stage within a week. Some parts will be replaced, most others inspected, but they are not all getting rebuilt/refurbished every single takeoff.

    17. Re:Re usability by justaguylikeme · · Score: 2

      I thought the only rocket-related thing reused from the shuttles was the fuel tank, and that only after reconditioning it post-ocean swim.

      No, actually it was the Solid Rocket Boosters that were reused. After burnout, they were jettisoned at a (relatively) low altitude. The external tank, which stayed connected to the orbiter to a substantially higher altitude did not survive reentry.

    18. Re:Re usability by Drethon · · Score: 2

      That little bit tougher adds weight and cost to the rocket. May pay off in the long run but not on the first launch.

    19. Re:Re usability by morgauxo · · Score: 3, Informative

      The nice thing about SpaceX's approach is that a Rocket launches, flies and lands like a rocket. The shuttle, spaceplane aproach attempts to build something that is both a rocket and an airplane. The result may be both rocket and plane but it is neither a very good rocket nor a very good plane.

      Space shuttle pilots use to refer to the lander as a "flying brick". That was not a compliment!

    20. Re:Re usability by itzly · · Score: 2

      With a brand new rocket, you risk faulty assembly. With a used one you risk wear and tear. Hard to say which one is better. It all depends on the other parameters that you're not saying.

    21. Re:Re usability by Anonymous Coward · · Score: 0

      Actually the rockets were resued. The external fuel tank was thrown away each time (distinergrated in reenty)

    22. Re:Re usability by jklovanc · · Score: 1

      Almost makes me wonder if they could make them just that little bit tougher to begin with

      Tougher means heavier. Every additional pound used for toughness is one less usable pound for payload.

      I still await the day that a multi-stage re-usable comes back, like the Shuttle.

      Except that the solid rocket boosters and fuel tanks were not reusable. Only the engines were re-used and that after expensive overhauls.

      This coupled with space-mining will hopefully bring a calm to the human race that we haven't seen since, well, ever.

      We can not return land or food from space so we will still have conflict on Earth.

    23. Re:Re usability by jklovanc · · Score: 3, Interesting

      The SRBs were re-used as well as the engines connected to the Shuttle itself.
      The external tank is jettisoned too high to recover. It was thought that it could be used in space to construct something but that was never done.

    24. Re:Re usability by rasmusbr · · Score: 3, Interesting

      Even if they can recover the engine intact how many times can it be reused. Saving a few million on a higher chance of blowing up multi billion payloads is not exactly wise economically.

      Think of it this way: if they can fly the first stage 20 times, that along with some cost optimizations of the upper stage could cut the cost per pound by a factor of ten. Then it would become economical to launch mere multi-hundred million dollar payloads. That would dramatically reduce the economical risk of any single launch, as long as the rocket is not ten times as likely to blow up, but rather only maybe twice as likely.

      Of course, anyone who launches a lot of rockets of the same type is likely to become really good at getting that type to orbit in one piece. Just look at the Russians and their now ancient Soyuz rocket.

      Keep cutting costs and you might one day have a system where you could launch a ten million dollar payload, which you could easily insure at your local insurance company.

    25. Re:Re usability by Anonymous Coward · · Score: 1

      Coking is largely a problem with a high olefin content. The cut of kerosene they're using has a very low percentage of olefins in order to cut down on coking. This was established way back when we first tried to use the JP series cuts of kerosene as RP.

    26. Re:Re usability by Strider- · · Score: 4, Informative

      The external tank is jettisoned too high to recover. It was thought that it could be used in space to construct something but that was never done.

      As much as this played out in various types of fiction and so forth, the reality is that the tanks wouldn't have been all that useful in orbit. The foam insulation would have off-gassed significantly and dumped all sorts of crap into your orbital environment, and the tanks themselves had nowhere near the shielding required to be used for human habitation (both radiation, and micrometeorite).

      --
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    27. Re:Re usability by 0123456 · · Score: 1

      Tougher means heavier. Every additional pound used for toughness is one less usable pound for payload.

      That's Shuttle-think: 'to minimize cost, everything must be as efficient as possible to get the maximum payload on each flight'.

      In reality, if making the engine 10% heavier would allow you reuse a stage twice as often before you had to throw it away, you'd probably find you saved money. In particular, the mass of the first stage engines has little impact on the payload, as they don't go anywhere near orbit.

    28. Re:Re usability by 0123456 · · Score: 1

      The SRBs were re-used as well as the engines connected to the Shuttle itself.

      The tin cans around the SRMs were reused. There's still debate as to whether it saved NASA any money, since most of the cost of the SRB was the SRM inside it, which had to be replaced every time.

    29. Re:Re usability by Anonymous Coward · · Score: 0

      Ability to survive an engine failure is only true for rockets designed to do so, such as the Saturn V and Falcon 9. The Falcon 9 added reinforced shielding between the engines to minimize the chance that an explosion would take out the nearby engines (some engine failures are more catastrophic than others). It also helps that the Falcon 9 uses nine relatively smaller engines rather than a few big ones like some rockets.

    30. Re:Re usability by I+will+be+back · · Score: 1

      Fuel is 5% of the cost, so calculate it yourself :)

    31. Re:Re usability by 0123456 · · Score: 1

      Reuse of the shuttle took several months of costly refurbishing for each launch, though.

      If I remember correctly, wasn't the fastest turnaround about six weeks between flights? I think that was two flights of the same payload, though, so they didn't have to change out much in the payload bay.

    32. Re:Re usability by cjameshuff · · Score: 1

      The solids were partially reused...they used heavy steel casings that survived recovery. You couldn't exactly say the same booster flew twice, though, and the casings were probably one of the cheapest components of the entire system (being steel drums wrapped around a low-performance solid rocket motor that just got the vehicle off the pad and was dropped off early in the launch). The Orbiter was heavily refurbished after each flight, but was reused. The external tank could have been brought into orbit and repurposed there, but NASA never mustered the ambition and focus to do so...they just dropped them to burn up in the atmosphere.

      SpaceX doesn't seem interested in burdening their spacecraft with wings, and they are very focused on cost reduction, so their eventual reusable upper stage (for the next rocket after the Falcon 9, most likely) will hopefully avoid the problems the Shuttle had.

    33. Re:Re usability by Noah+Haders · · Score: 1

      What kind of payload would be multi billion dollars?????

    34. Re:Re usability by Anonymous Coward · · Score: 1

      The mass of all stages matters. But I get what you are saying, if you increase the mass of the first stage while maintaining TWR, THEN it doesn't matter. But just increasing the mass always matters, and the first stage is where you fight the most gravity and the most wind resistance.

      The mass of the first stage in some ways is the most important for payload.

      It is almost like you have never played Kerbal Space Program.

    35. Re:Re usability by Megane · · Score: 1

      It is entirely possible that the number of customers requiring new vehicles (even if just NASA and other government agencies) could be more than enough to supply used-vehicle launches.

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    36. Re:Re usability by Ichijo · · Score: 1

      The shuttle, spaceplane aproach attempts to build something that is both a rocket and an airplane. The result may be both rocket and plane but it is neither a very good rocket nor a very good plane.

      It's worse than that. It's a rocket, an airplane, and an orbital re-entry vehicle. A suborbital craft is much better at being both a rocket and an airplane.

      --
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    37. Re:Re usability by Anonymous Coward · · Score: 0

      Space X current mission is low risk for that. They are just delivering food and equipment to the space station. If the first stage blows they can always find more food to send. special equipment can be rebuilt. No risk to the station with first stage. There is some risk to the launch site.. It will matter more with human payload. But I suspect they will only reuse rockets for the supply missions and satellites. A truck on the other hand puts at least one driver at risk.

    38. Re:Re usability by Anonymous Coward · · Score: 0

      The orbiter contained the main engines, which were re-used after refurbishing.
      The engines are the most expensive part of the rocket.

    39. Re:Re usability by Smidge204 · · Score: 1

      Except that the solid rocket boosters and fuel tanks were not reusable. Only the engines were re-used and that after expensive overhauls.

      The Shuttle's SRBs were reusable, and they reused them (or at least parts of them) pretty much every launch.

      The big orange liquid fuel tank was not reused, though.
      =Smidge=

    40. Re:Re usability by 0123456 · · Score: 1

      It is almost like you have never played Kerbal Space Program.

      In the real world, the mass of the first stage is usually mostly fuel, so a 10% increase in the mass of the engines doesn't make much difference to the amount of thrust you need to launch. This is why, for example, most of the weight-saving work to increase the Saturn V payload was in the second stage, where it made a much larger difference than the first.

    41. Re:Re usability by eth1 · · Score: 2

      I'm sure that customers with astronomically expensive or critical payloads will always have the option to specify a "new" booster if they're willing to pay more.

      On the other hand, if you need to launch a constellation of 20 satellites, it might be much cheaper to budget for 22-24 cheaper "used" launches than 20 more expensive but more reliable new ones.

    42. Re:Re usability by CrimsonAvenger · · Score: 4, Interesting

      Honest question: You have a ticket to the ISS. You can choose a rocket that just came out of the VAB* or one that recently launched and returned whole and was turned around for this flight. Which do you trust more?

      So, let's look at history for a (possible) answer. The Apollo flights were all "just came out of the VAB" flights. There were 40 of them, including a loong unmanned test series (17 manned flights). Counting Apollo 13, two of them failed. Which gives you 5% failure rate (including 13), or 2.5% failure rate (not).

      Shuttle had 135 missions, with two failures. Failure rate ~1.5%.

      So, shuttle, which "returned whole and was turned around for this flight" had a better safety record than Apollo, which "just came out of the VAB".

      Note that if you substitute Soyuz for Apollo, you get similar results. Yes, Soyuz had two loss-of-crew failures, just like Shuttle, but in fewer than 135 flights....

      --

      "I do not agree with what you say, but I will defend to the death your right to say it"
    43. Re:Re usability by Anonymous Coward · · Score: 0

      They're not just recovering the engines - they're recovering the entire first stage, as a whole unit, with the end goal being "re-stack, refuel, relaunch" stype reusability.

    44. Re:Re usability by Anonymous Coward · · Score: 0

      The only thing I can think of is the JWST, and I think that one's going up on a Delta IV.

    45. Re:Re usability by bledri · · Score: 2

      That was the first thing that jumped to my mind. Kind of reminds me of retread tires -- a lot of the truck tire fragments you see by the side of the road are from retread tires that self destructed. A lot of companies buy them because they're cheaper, but the chances that they'll fail is far higher.

      But the consequnces of your first stage failing are much worse than the consequences of your tire shredding on the freeway. And those are bad enough.

      Yes, rockets go through more extreme forces and environments, but that does not mean that rockets can not be made to safely survive multiple fights.

      It could be that due to the bathtub curve that some number of flights after the first flight are the most reliable. Right now every rocket flight is a maiden voyage (also known as a shakedown cruse). Brand new rockets fail on occasion.

      --
      Some privacy policy Slashdot.
    46. Re:Re usability by Anonymous Coward · · Score: 0

      KSP is nowhere near real world balance. Or real aerodynamic models.

      In the real world, dry mass is 1-5% of wet mass for fuel tanks + engines, and the fuel portion of the equation is pretty cheap compared to the cost of tanks/engines. Shaving a few percentage points off the mass of your tanks / engines, doesn't matter much in the lower stages.

    47. Re:Re usability by nitehawk214 · · Score: 1

      With a used rocket you risk faulty assembly as well. They have to take the whole thing apart and inspect every bit of it. But hopefully that inspection would reduce the wear and tear risk. As long as the recovery, inspection, and reassembly is cheaper than building an entire new rocket, everybody wins.

      It's just like when I work on my car, there are always a few bits left over...

      --
      I'm a good cook. I'm a fantastic eater. - Steven Brust
    48. Re: Re usability by Anonymous Coward · · Score: 0

      Yeah but even hungry people still need gold and diamonds

    49. Re:Re usability by confused+one · · Score: 1

      The vehicle is designed with engine out capability; so, if they lose one engine, it's not the end of the world. They put shields and baffles with Kevlar blankets between the engines so it's unlikely (but not entirely impossible) a catastrophic failure will harm an adjacent engine.

    50. Re:Re usability by Immerman · · Score: 1

      Firstly, the capsule is a tiny fraction of the cost of the launch - the vast majority is the rocket itself.

      And where the rocket is concerned, you currently have that whole "high-speed collision with the ocean" thing going on after every launch - you're not going to "out tough" that without taking drastic payload-robbing measures, so there's no point in trying. Once the whole "return and reuse" part is mastered though, then the economic incentives will shift dramatically. You have to be able to get a second use out of an engine before it's worth worrying about the third, but you'd best believe concern for the thirtieth use will follow close behind that.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
    51. Re:Re usability by Ungrounded+Lightning · · Score: 1

      The foam insulation would have off-gassed significantly and dumped all sorts of crap into your orbital environment, ...

      Originally they were to be painted with a coating that would have kept the foam together, etc.

      Then somebody looked at how much that coating weighed. (It comes right out of payload.) And they decided not to paint the tank after all and let the foam get shredded a bunch on the way up (after it wasn't really needed if you weren't going to re-use the tank for anything).

      They actually burn some extra fuel to be sure the tank goes back DOWN and crashes in a desired area, so it doesn't go into low orbit, become short-lived space junk, then later come down in some unpredictable place along that orbit after "space weather" - mainly the varying expansion of the upper atmosphere - causes the orbital decay to proceed at some varying and unpredictable rate.

      I recall space advocates being livid that the tanks were not being orbited and collected for orbital construction.

      --
      Bantam Dominique roosters crow a four-note song. Once you've heard it as "Happy BIRTHday" you can't NOT hear it that way
    52. Re:Re usability by Ungrounded+Lightning · · Score: 1

      the tanks themselves had nowhere near the shielding required to be used for human habitation (both radiation, and micrometeorite).

      So you collect them into a cluster and store consumables (like water) that perform shielding in the outer layers.

      Also: You really don't WANT shielding most of the time - unless you're up there for years. Primary cosmics mostly go right through you, while shielding produces lots of ionizing secondaries that tear you up. Then you need a LOT of shielding to block the secondaries. Its mostly the occasional solar storm that requires shielding.

      This was looked at in detail over the last several decades. The tanks would have been very valuable for a lot of stuff. But not to NASA programs. Lots of politics involved.

      --
      Bantam Dominique roosters crow a four-note song. Once you've heard it as "Happy BIRTHday" you can't NOT hear it that way
    53. Re: Re usability by WindBourne · · Score: 1

      Rated for 40 full ignitions. As such, they expect at least 10 safely. Also, remember, they have many sensors AND can deal with engine out.

      --
      I prefer the "u" in honour as it seems to be missing these days.
    54. Re:Re usability by Immerman · · Score: 1

      Is not the insulation *outside* the tanks? While any pressurized environment you wanted to create would be *inside* those tanks. You're not going to get any outgassing through the walls of an aluminum pressure tank. And if fuel the baffles and such outgassed - so what? You probably want to rip that stuff out and polish the tank clean before you move in anyway. Problem solved. Ditto if you were disassembling them for construction components - aluminum isn't going to absorb all that much gas, especially considering you've got hard vacuum ensuring pressures never get high enough to allow.

      And while they might not be suitable for human habitation as-is, I imagine they'd be just fine for laboratories, etc. that could be mostly automated - or you just wear your lead overalls in the lab. Or... you could strap a big honking pile of tanks together, and let those in the outer layers provide shielding for those at the center. Just how many Shuttle launches were there?

      On the other hand a parking orbit stable for several decades would have to be much higher than most launches ever went, and boosting the fuel tanks into it would probably have put a major dent in the payload. Meanwhile, it looks like the cost of launches may soon be falling to the point that boosting new, purpose built habitat components into orbit won't be prohibitively expensive, so it's hard to find too much fault with NASA for not being future-minded enough to leave a giant navigation hazard in orbit. But I reserve the right to mourn the giant orbital city/fuel-tank depository that never was.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
    55. Re:Re usability by drinkypoo · · Score: 1

      Actually you'd inflate a bag inside of them, and then you wouldn't have to worry about getting them surgically clean. But Bigelow thinks you can just use the bag, so perhaps the tanks weren't important.

      --
      "You're right," Fisheye says. "I should have set it on 'whip' or 'chop.'"
    56. Re:Re usability by Anonymous Coward · · Score: 0

      The Shuttle's SRBs were reusable

      There's no such thing as a reusable SRB. You build a brand new SRB inside a spent casing, at nearly the same cost as the original, plus all the overhead of recovery.

    57. Re:Re usability by Anonymous Coward · · Score: 0

      Plus sending scuba teams to retrieve components followed by massive refurbs are not what I consider truly reusable at least in the 747 analogy Musk keeps making.

      That's why they're spending so much effort on a pad landing.

    58. Re:Re usability by LordWabbit2 · · Score: 1

      Well hopefully they are better at working on their "car" than you are at working on yours. If you have bits left which are not the bits you replaced you start to wonder why there is a slight rattle coming from under the hood when you turn left on an incline (yes I also end up with bits left over).

      --
      There are three kinds of falsehood: the first is a 'fib,' the second is a downright lie, and the third is statistics.
    59. Re:Re usability by Smidge204 · · Score: 2

      Well, no. The Shuttle's SRBs were a lot more than just a tube full of explosives.

      They had thrust vector control; hydraulic power units, gimbal nozzles, control hardware. Electrical subsystems. Self contained navigation hardware. Range safety hardware. And of course everything was triple or quadruple redundant for reliability.
      =Smidge=

    60. Re:Re usability by Immerman · · Score: 1

      Why? You already have a tank designed to hold pressure, and they held hydrogen and oxygen, hardly high risks for incidental exposure. You'd want to make sure your welds were up to snuff, but that would be true for bag seams as well.

      And what Bigelow is working on are hardly "bags". Inflatable perhaps, but it seems like that's mostly a space-saving feature so that they can get a better surface(mass)-to-volume ratio on a module that can be sent up in one piece.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
    61. Re:Re usability by cjameshuff · · Score: 1

      Assuming the first flight is the most reliable one. They may instead start offering a discount to those willing to risk a payload on a vehicle that's never flown before.

    62. Re:Re usability by radarskiy · · Score: 1

      Clearly, you should take the option that has just crashed twice.

    63. Re:Re usability by nitehawk214 · · Score: 1

      I am hoping that if I working on my car a few more times I will end up with enough spare parts to build a second one.

      --
      I'm a good cook. I'm a fantastic eater. - Steven Brust
    64. Re:Re usability by nitehawk214 · · Score: 1

      Also I English good.

      --
      I'm a good cook. I'm a fantastic eater. - Steven Brust
  3. In other news for tomorrow .. by OzPeter · · Score: 1, Informative

    A hi-tech engineering company will continue on with its plans to test a well-engineered aspect of its product that, that after rigorous R&D, is expected to reduce the costs to end users.

    It's not Daring. Its business as usual for a company that is doing actual R&D on leading edge products.

    But that doesn't mean that I don't want to see it work. Vertical landing rockets are the next step to the world of Tom Corbett, Space Cadet

    --
    I am Slashdot. Are you Slashdot as well?
    1. Re:In other news for tomorrow .. by gstoddart · · Score: 5, Insightful

      It's not Daring. Its business as usual for a company that is doing actual R&D on leading edge products.

      In all honesty, from looking around me these days ... I conclude that doing actual R&D on the leading edge of stuff is itself daring.

      Increasingly, companies want to make a "me too" product or do things based on what focus groups tell them is good.

      Hell, even some tech companies seem to be retreating from meaningful R&D and focusing on "leveraging and monetizing their IP portfolio".

      Nobody is willing to invest in R&D any more unless it gets them a tax break. And in that case, they'll try to tell you to categorize a ton of unrelated stuff as part of the R&D effort so the accountants can maximize the write off.

      So, me, I'll still stick with daring. Saying you figure you have a less than 50% chance of success these days is pretty bold.

      --
      Lost at C:>. Found at C.
    2. Re:In other news for tomorrow .. by jbmartin6 · · Score: 1

      "Increasingly...","any more"...Why be such a downer about the present? Aren't you just describing the way things have always been? Otherwise Europe would have had stirrups long before Jesus

      --
      This posting is provided 'AS IS' without warranty of any kind, implied or otherwise.
    3. Re:In other news for tomorrow .. by 50000BTU_barbecue · · Score: 5, Insightful

      " I conclude that doing actual R&D on the leading edge of stuff is itself daring."

      In the 1960s, companies hired you and they paid YOU to do R&D.

      Today, universities are the R&D branch of corporations. Universities soak up public money (most of it funneled into textbook companies and top-heavy administration) and students pay the university,.

      Then the students can get some nice debt, and go begging for the few technical jobs left out there.

      --
      Mostly random stuff.
    4. Re:In other news for tomorrow .. by gstoddart · · Score: 2

      You know, I have personally watched tech companies become less willing to invest in pure R&D, less willing to make new things that someone hasn't already made, and be much more beholden to whatever the heck the CEO thinks is the Next Big Thing.

      I have been at companies where we went from being innovators to imitators, and where the CEO would routinely make moronic predictions which didn't happen based on what the trends were. And then in six months make an entirely new set of moronic predictions, based on whatever the trend was then.

      So, I don't know if this has changed in my lifetime (as I perceive it), or if it's cyclic, or what.

      If I could answer these questions ... well, I'd be charging vast sums of money for those answers. Like Gartner does.

      Only Gartner is just as full of shit as I am, so maybe I'm just doing it wrong, and need to find out how to charge people vast sums of money to identify emerging technologies which will never go anywhere.

      Because, I think that's where the real money is.

      --
      Lost at C:>. Found at C.
    5. Re:In other news for tomorrow .. by jythie · · Score: 2

      Sadly, we have only consumers to blame for this. Companies that invested lots of their resources in R&D tended to suffer in the market. Patents, which were designed to try to even things out, have become such a clusterexpletive that they are utterly failing at doing that.

      The money tends to go to the companies that focus on streamlining their production systems and leave the "research" up to their competitors. This kinda worked when there was lots of government funded research (which any company could benefit from) but that has been scaled back, twisted, and privatized so that it is not really making up the differnce either.

    6. Re:In other news for tomorrow .. by Nutria · · Score: 2

      Increasingly, companies want to make a "me too" product or do things based on what focus groups tell them is good.

      We won't mention that vertically-launched multi-stage rockets powered by RP-1/LOX are pretty "me too".

      --
      "I don't know, therefore Aliens" Wafflebox1
    7. Re:In other news for tomorrow .. by MozeeToby · · Score: 1

      Yep, that's why everyone lands their boost stage and cuts their costs by a significant fraction... right?

    8. Re:In other news for tomorrow .. by Kuruk · · Score: 1

      Very true. Our goals seem to the greed based now.

      The days of wonder and learning are too expensive for companies with shareholders to feed cash.

    9. Re:In other news for tomorrow .. by dcollins · · Score: 1

      A lot of that's true, but I'm not sure how you think public money passes through universities to textbook companies? (In reality, it's students paying textbook companies directly.)

      --
      We know where leadership by an anti-intellectual "strongman" who scapegoats minorities and likes boisterous rallies goes
    10. Re:In other news for tomorrow .. by slew · · Score: 2

      A lot of that's true, but I'm not sure how you think public money passes through universities to textbook companies? (In reality, it's students paying textbook companies directly.)

      In reality, public money passes through government default subsidized student loan programs to allow students to borrow money at favorable interest rates to allow many students to pay textbook companies that otherwise could not afford to pay textbook companies. But I digress...

      Fortunately, student funding/debt has very little to do with how most universities are funding their research. In actuality, most prestigious research universities are pretty much directly funded by public money (including private institutions in the USA) in the form of research grants. The tuition they charge their student (esp at the undergraduate level) generally is a small part of a typical schools budget and generally could easily be covered by a fraction of their endowment income. Most grant money *includes* overhead for operations.

      However, student funding has very much to do with how universities fund their non-research operations that aren't covered by grant overhead. This is especially true at institutions that do no research at all and of course most acute at diploma mills.

      The reason that prestigious research universities charge students so much is that it conveys a sense of value to the education they are providing and is easy to get the students to take out loans (esp publically subsidized loans) for their education and once they max out loans, they often discount the remainder to cover the difference. The reason less prestigious universities charge so much is that more prestigious universities set the price point high (basically a type of comparative level-set pricing collusion).

      Sadly, the way it is set up now, by making it so easy to borrow, the government is essentially tax/spending the students future income to transfer this wealth to universities. Is it fair that only students are burdened with this "tax" rather than the public at large? The universities are charging more because it's easy for the students to borrow the money and the students are caught in the middle. Why is the government making it so easy for students to go into massive debt (esp for diploma mill paper)? Well that's a political question...

      Textbook money is also a drop in the bucket at any research university. Other than undergrads, who's using textbooks for research anyhow? Instead, researchers are reading and writing papers for journals that are probably 10x worse at gouging money than the worst offending textbook companies.

    11. Re:In other news for tomorrow .. by slew · · Score: 1

      Yep, that's why nobody lands their boost stage and cuts their costs by a significant fraction... right?

      FTFY. Might be true someday, but not today...

  4. How to launch "tomorrow" when you're 25 days late by Anonymous Coward · · Score: 0

    Use overflowing hours! Jan 6 620am = Jan 31 8pm.

  5. It will fail by Anonymous Coward · · Score: 0

    This attempt is probably going to fail. But that is OK. SpaceX isn't risk adverse so failures don't send the organization into a tailspin.

    Go SpaceX!

    1. Re:It will fail by HangingChad · · Score: 2

      This attempt is probably going to fail.

      You're probably right but they have data from two other water landings, so it's not like this is completely cross your fingers territory.

      It's still amazing and I hope they pull it off. Elon Musk is the man.

      --
      That's our life, the big wheel of shit. - The Fat Man, Blue Tango Salvage
    2. Re:It will fail by Guspaz · · Score: 1

      The water landings had accuracy measured in miles, while this landing will require accuracy measured in feet. They hope to achieve that accuracy using the new fins, which have never been used at hypersonic velocities before. There's a lot of never-been-done-before for SpaceX going into this launch.

    3. Re:It will fail by Anonymous Coward · · Score: 0

      ...which has been extensively simulated and tested in wind tunnels.

      Of course this is the real all-up test and a failure is possible - a lot of things have to go right, in order, with no second chances, but I honestly think the odds are higher than the conservative wild-guess 50-50 that has been quoted.

  6. Other planets by MobyDisk · · Score: 1

    Is this maneuver easier or harder to do inside the atmosphere of Mars, as compared to Earth? It sounds like a possible plan for return trips from Mars, if the rocket is re-usable.

    1. Re:Other planets by Fire_Wraith · · Score: 2

      They've already managed a vertical takeoff/vertical landing on the ground: www.youtube.com/watch?v=ZxKWh7kLDzw

      Most likely this is a step towards general reusability from a cost perspective, as there are advantages to doing recovery on water (generally less problems if you somehow screw it up I would think).

    2. Re:Other planets by necro81 · · Score: 1

      Easier on Mars, because you generally don't have to worry about strong winds. The gravity is lower, so it requires less thrust. For some rocket engines, this is actually difficult, because you have a limited throttle range; the Merlin engines have been designed for this.

      Also in your favor on Mars, your landing pad isn't pitching up and down on waves. On the other hand, the ground is not necessarily a smooth, flat, level pad. SpaceX has demonstrated the ability to hover, so as long as you have decent fuel reserves, you should be able to spend some time searching for a good spot.

      However, in the case of using this technology to land on Mars, there is a significant difference: you would be using it to land a rocket (first stage and all) on the planet after having done a long coast from Earth and a violent re-entry. That is definitely more difficult than returning a first stage to the ground after lift off.

    3. Re:Other planets by CrimsonAvenger · · Score: 1

      This is almost meaningless in terms of Mars. Mars surface gravity is low enough that, for instance, a Falcon 9 first stage could land from orbit and take back off without even having to refuel.

      That said, you probably want a different shape to your rocket on Mars - shorter and broader across the base, to minimize surface area per unit volume. It's not like air resistance there is enough to need the skinny pointy things we use here....

      --

      "I do not agree with what you say, but I will defend to the death your right to say it"
    4. Re:Other planets by Anonymous Coward · · Score: 0

      SpaceX currently relies on the drag of the atmosphere to slow the rocket down to terminal velocity. The atmosphere on Mars is drastically thinner (0.6% of Earth) so a rocket needs to rely much more on retropropulsion to slow down and land.

      The biggest problem, then, is fuel. You need a huge rocket to bring a tiny payload to Mars, not including the fuel for a return trip. The more fuel you bring, the more mass you need to slow down for a landing (you might be able to leave some of it in orbit and have a separate lander). That's why many proposals for a Mars return trip call for either sending a large number of fuel supplies on unmanned ships in advance of a manned mission, or relying on in-situ resource extraction (ISRU) to generate methane on Mars by extracting CO2 from the atmosphere combined with lightweight hydrogen carried from Earth (requires an extended stay, or automated ISRU rovers sent in advance).

    5. Re:Other planets by Gavagai80 · · Score: 1

      The reason for doing recovery on water is that when you launch eastward from Florida the rocket will come down over water unless you expect a ton of fuel to get back to land.

      --
      This space intentionally left blank
  7. A great idea, but... by Diddlbiker · · Score: 3, Funny

    Once SpaceX has worked out the kinks and has implemented this as a good way to reduce costs, some patent troll will step forward showing that he patented the very concept of this in 1998. "Elon Musk stole my invention".

    The lawsuit will of course be filed in the court of East Texas.

    1. Re:A great idea, but... by Megane · · Score: 1

      Well, at least it's not too bad a drive from McGregor.

      --
      #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
    2. Re:A great idea, but... by Anonymous Coward · · Score: 0

      Blue Origin actually has a patent on sea landing of a rocket. SpaceX has filed a preemptive lawsuit that seems likely to succeed since there is substantial prior art.

    3. Re:A great idea, but... by Anonymous Coward · · Score: 1

      they already did, Jeff Bezos' blue origin claimed a patent for sea landing a first stage

      Elon called bullshit and sued for 'prior art' of which there are MANY examples

      http://www.geekwire.com/2014/elon-musks-spacex-challenges-patent/

    4. Re:A great idea, but... by EnsilZah · · Score: 1

      Jeff Bezons' Blue Origin is already suing SpaceX based on a patent for landing a rocket on a sea platform.

    5. Re:A great idea, but... by Anonymous Coward · · Score: 0

      False. Blue Origin does have the patent but SpaceX has already pre-emptively filed for it to be tossed and piled on prior art.

      Blue Origin has not (yet) sued SpaceX for anything. In theory they might first thing tomorrow once the stage is on the barge, but...

  8. The sea isn't very stable. by Nutria · · Score: 3, Insightful

    Trying to balance a big pencil on a postage stamp that's moving unpredictably and simultaneously in 4 axises (pitch, roll, yaw, altitude) doesn't seem to have very high odds of success. And the worse the sea is running, the lower the odds.

    If it works, though, count me really impressed by what would surely be a Crowning Moment of Awesome.

    --
    "I don't know, therefore Aliens" Wafflebox1
    1. Re:The sea isn't very stable. by Anonymous Coward · · Score: 0

      They're using thrusters from an offshore rig to stabilize the platform.

    2. Re:The sea isn't very stable. by Anonymous Coward · · Score: 1

      There are actually six degrees of freedom, but who's counting? The problem won't be a moving pitching platform. Active position control of such vessels surprisingly good. The question is whether the rocket will have the steering authority to converge on the barge location with the minimal fuel it has. My guess is no. But I give SpaceX credit for trying.

    3. Re:The sea isn't very stable. by Anonymous Coward · · Score: 0

      It's just he inverted pendulum undergrad control lab in a few more dimensions and a much larger budget. Seems do-able to me, but I got my pendulum to stand up too... :)

    4. Re:The sea isn't very stable. by gman003 · · Score: 1

      The sea platform isn't the end-goal. This is just to prove that they can safely land it, so they can be approved for it to return to US airspace for a ground landing.

      It only has to work a few times, then it'll get mothballed. Or maybe shelved, to use whenever they need an emergency landing platform for some reason.

    5. Re:The sea isn't very stable. by cmcqueen1975 · · Score: 1

      They want to land on the sea platform, refuel from fuel tanks on the sea platform, then take off again and fly back to the launch location. http://www.nasaspaceflight.com...

    6. Re:The sea isn't very stable. by cmcqueen1975 · · Score: 1

      Actually, maybe I'm jumping to conclusions. It's possible they may want to land on land (not a sea platform; maybe an island) downrange, refuel at that location, and then fly back to the launch location. Anyway, the main point being that there's a land-and-refuel step before flying all the way back to the launch location.

    7. Re: The sea isn't very stable. by WindBourne · · Score: 1

      I suspect that long term, they will move abandoned oil rigs into positions for landing.

      --
      I prefer the "u" in honour as it seems to be missing these days.
    8. Re:The sea isn't very stable. by Anonymous Coward · · Score: 0

      Luckily empty rocket stages are ridiculously bottom heavy. Also the new grid fins help a lot.

    9. Re:The sea isn't very stable. by Anonymous Coward · · Score: 0

      SpaceX is looking into using the Autonomous Spaceport Drone Ship (aka Barge) as a long term solution for Falcon Heavy center core recovery - it would fly so fast and so high that returning it to launch site may cause too large performance penalty (aka fuel use) and landing it downrange would work better.

      F9 first stage and side cores of Heavy are planned to return to launch site as soon as the process is tested and deemed safe. NASA and USAF do not want errant stages dropping on nearby launch pads or the VAB at the Cape and all that... :)

  9. Obligatory Python Variation by R3d+M3rcury · · Score: 5, Funny

    "We've been able to soft-land the rocket booster in the ocean twice so far," says Musk. "Unfortunately, it sort of sat there for several seconds, then tipped over and exploded. [...]"

    "Everyone said I was daft to land a rocket in the ocean, but I did it all the same, just to show them. It sank in the ocean. So I built a second one. That sank in the ocean. So I built a third. That burned down, fell over, then sank in the ocean. But the fourth one stayed up!"

    I think I'll go for a walk now...

  10. Other planets by Anonymous Coward · · Score: 0

    I don't think the landing maneuver itself is difficult, they've successfully tested it twice. The hard part is getting it to land in a predetermined area only a few hundred feet across. On most other planets that wouldn't be much of an issue as there are large swaths of barren land, on Earth you generally have either trees, water, property considerations, safety considerations, etc to deal with.

  11. Our capsule got wet, get the towels!! by deodiaus2 · · Score: 1

    Somehow, I think that a component that pulled a 10 G when launched, went through a massive deceleration while being super heated and exposed to corrosive water and oxygen isn't going to be significantly damaged if it splashes down in the ocean?
    That and the fact that landing on a carrier is not always going to be cushy and might miss during a wave swell?

    1. Re:Our capsule got wet, get the towels!! by Anonymous Coward · · Score: 0

      The salty air is a concern, but yeah, a 10-story building falling over into the water will probably break it. The loads it's designed for aren't 10g, and are optimized for one axis only, not impacts to the side. A beer can, if scaled up to the size of a rocket, has thicker walls than rockets do.

    2. Re:Our capsule got wet, get the towels!! by Anonymous Coward · · Score: 0

      they have no choice
      Falcon Heavy launches from the coast will require a place for the center stage to land downrange...in the ocean or on a barge take your pick.
      Once qualified 'safe' SpaceX will land the side stages of FH on land, as well as singl stages from F9R but only after they can prove the tech over water.
      Theres always a plan in place when SpaceX, Tesla, Solar City does something, just look for it.

    3. Re:Our capsule got wet, get the towels!! by Anonymous Coward · · Score: 0

      SpaceX is landing them on the ocean currently, but they aren't even attempting recovery from there, it's just for the sake of testing landing in a safe area. Post-splashdown recovery is not their goal and they haven't build the first stage to survive it.

      SpaceX aside, weren't shuttle SRBs recovered after splashdown? Pretty sure they weren't recovering them from dry land.

  12. What is "620 am"? by Anonymous Coward · · Score: 0

    Oh, wait... Americans.

    1. Re: What is "620 am"? by Anonymous Coward · · Score: 0

      Yes, but which Americans? The ones 5 hours behind proper time, or the ones further west? They don't give any clues about what time they speak. The only way to know what time Americans really mean is to look up the event they're talking about. In this case 11:00 UTC seems to be launch time.

  13. The sea isn't very stable. by Anonymous Coward · · Score: 0

    Your analogy is a bit harsh. First off while the booster may look like a pencil it is very bottom heavy due to the weight of the rocket motors and remaining fuel. A better analogy for it would probably like the cardboard tube inside of a paper towel roll with a large marble and some fins glued to the bottom of it. Also the postage stamp is 300ft wide compared to the base of a rocket only 12' wide, A better analogy there would be a napkin. The only major difficulty is that it is being dropped from an extreme height and very little propulsion to get itself to the napkin.

  14. You hit the nail on the head... by Anonymous Coward · · Score: 0

    "throwing away a 747 jet after a single transcontinental flight."

    Did we learn nothing from the shuttle? The engines in these things operate not terribly far from the limits of materials technology - Sure the shuttle was "reusable" whereby "reusable" meant "It cost more to recondition the thing to fly again than it would've cost to build a big dumb booster."

    If the 747's turbines had to be pretty much completely taken out and sent back to the factory to be rebuilt after every single flight (like the shuttle's RDd did), and the rest of the airframe and components had to go through a many weeks long long overhaul just to make sure it hadn't managed to shake something to death (which it dearly tried to do, twice, on every single flight)... YES, you'd be stupid to not build disposable ones. Like the Soyuz... fifty years and as cheaply indestructible as ever.

    1. Re:You hit the nail on the head... by Guspaz · · Score: 1

      SpaceX's goal isn't to be merely reusable, it's to be fully and rapidly reusable, with no refurbishment. If they require a substantial amount of refurbishment betwen launches, they will consider themselves to have failed.

    2. Re:You hit the nail on the head... by Anonymous Coward · · Score: 0

      Ah, but computers and 3D printing have changed the game , you Luddite!

    3. Re:You hit the nail on the head... by Gavagai80 · · Score: 1

      The engines in these things operate not terribly far from the limits of materials technology

      The whole Space-X strategy from the start has been to use a lot of little less complicated interchangeable engines instead of a big one. A Falcon 9 is 9 engines, the heavy is 27 engines. And because there's so many of them, they don't have to be used at a full burn. It appears likely to be a lot easier to recover and reuse these.

      YES, you'd be stupid to not build disposable ones. Like the Soyuz... fifty years and as cheaply indestructible as ever.

      The Soyuz accident rate is worse than the shuttle, and it costs more than even the current non-reusable Space-X flights.

      --
      This space intentionally left blank
  15. shuttle by Mr.+Slippery · · Score: 1

    . "Reusability is the critical breakthrough needed in rocketry to take things to the next level."

    What an amazing unprecedented breakthough idea.

    --
    Tom Swiss | the infamous tms | my blog
    You cannot wash away blood with blood
    1. Re:shuttle by cheesybagel · · Score: 1

      Except it wasn't really much of a reusable.

    2. Re:shuttle by Guspaz · · Score: 1, Insightful

      The shuttle was a complete failure in terms of reusability. It was supposed to cost $657 per pound to launch, and be refurbished for launch in two weeks. Instead it cost $27,000 per pound, and the speed record for refurbishment after Challenger was 88 days.

      It ended up costing more than expendable launch systems.

  16. That's not the approach you want to take for Mars. by Anonymous Coward · · Score: 1

    You want most of your return to Earth fuel to remain in Mars orbit. Do a powered descent with the Dragon Capsule, and return to orbit with Dragon under its own power to rendezvous with the upper stage that will bring it back to Earth. There's no reason to land a large, heavy upper stage on Mars just to launch it back into orbit again. You want just enough fuel aboard Dragon for the descent and ascent (plus contingency allowance).

  17. Funny description by myid · · Score: 1

    This article has a funny way to describe the attempt to soft-land on a floating platform:

    ... SpaceX acknowledges that the maneuver won't be a slam-dunk. Maybe it'll just be a slam. Or a dunk.

  18. Awesome by easyTree · · Score: 1

    Kinda obvious but awesome nonetheless. I guess that's why Musk makes the big bucks?

    These are the cost-saving insights that can be leveraged when one doesn't have a vested interest in wasting as much cash as possible; *cough* ASNA.

  19. not quite accurate by WindBourne · · Score: 1

    Skylon will have similar numbers to F9. In fact, possibly better. But as you point the heavy r&d costs will end up like Concorde. By the time that skylon flies, not only will f9 and FH be flying with all development costs paid for, but very likely, MCT will be flying and close to paying off its costs. And the MCT should make FH look positively expensive.

    --
    I prefer the "u" in honour as it seems to be missing these days.
  20. Rockets on Holiday by Anonymous Coward · · Score: 0

    Unfortunately, it sort of sat there for several seconds, then tipped over and exploded.

    Sounds like the first stage landed on a popular tourist destination in the middle of season, hoping to get some Mojitos and not burn.

  21. Re:That's not the approach you want to take for Ma by necro81 · · Score: 1

    Do a powered descent with the Dragon Capsule, and return to orbit with Dragon under its own power to rendezvous with the upper stage that will bring it back to Earth

    Dragon does not have enough fuel to both land and launch again. SpaceX hasn't demonstrated that it has sufficient capacity to even do a powered landing. I'm not saying itcan't, but you can't look at a Dragon capsule and consider it a vehicle capable of powering itself to orbital launch velocity, even on Mars.