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Estimating SpaceX's Reusable Rocket Cost Savings (theverge.com)

An anonymous reader writes: On Monday, SpaceX successfully landed its Falcon 9 rocket after launching a group of satellites into orbit. It's a huge breakthrough for the commercial space industry, because reusing rockets will dramatically reduce launch costs. The question now is: by how much? Elon Musk says it takes $60 million to build the Falcon 9, and $200,000 to fuel it. That's a big difference, but we can't expect them to immediately launch the rocket again after refueling it.

"The Falcon 9 experiences major temperature changes during its flights, as well as intense pressures and vibrations from the winds in the atmosphere. These all produce wear-and-tear on the vehicle's hardware — meaning the rocket might need repairs and updates before it can launch again." This kind of refurbishing is why the Space Shuttle ended up being way more expensive than expected. Fortunately, the Falcon 9 is not nearly as complex.

This is now the true test of SpaceX's design talents; if the rocket is built to be durable, then repairs and replacements could keep relaunch costs very low indeed. Steve Poulus, a former NASA project manager, suspects final costs could be driven below a million dollars. That figure would give SpaceX the capability of easily underbidding any competitor for government contracts, not to mention bringing it into affordability for any number of companies who'd like to put a satellite in orbit.

163 comments

  1. Reliability by Anonymous Coward · · Score: 2, Insightful

    Still, there are obstacles. SpaceX still needs to demonstrate the ability to consistently produce and launch rockets many times a year after the June accident caused an unexpected, six-month setback, something it will do with several flights planned for the weeks ahead.

    Just because it's relatively cheap to use Space X, if I have a 50-50 ( better or worse) chance that my $100 million satellite that took several years to design and build is going to get blown up, I'll pass.

    1. Re: Reliability by pr0t0 · · Score: 2

      Conventional lift systems also explode. It takes a fair amount of explosive power to put something into orbit, so the danger is ever-present. All payloads are insured as well. So given the choice, I'll go with the sub-million dollar launch.

      The money, while significant, is not the greatest cost of an explosion. It's the time it takes to build a new satellite and get in on the next launch window. That could potentially force you to miss your opportunity in the marketplace.

      First rule of government spending: why build just one when you can build two at three times the price?

      --
      I'm sorry, but your opinion seems to be wrong.
    2. Re:Reliability by beltsbear · · Score: 2

      Launch insurance. And their rate is much better then 50-50.

    3. Re: Reliability by Anonymous Coward · · Score: 2, Insightful

      Conventional lift systems also explode.

      Of course they do. But the point is how often. And Space X has a very small track record and as it stands now, it's dismal.

      It's the time it takes to build a new satellite and get in on the next launch window. That could potentially force you to miss your opportunity in the marketplace.

      That's dot com thinking. Businesses that are actually concerned with profitability and ROI think a bit differently. Meaning a couple of weeks - maybe months - late to market - assuming the Ruskies or the EU couldn't get me up there - is MUCH better than eating $100 million bucks and the years it took to develop the satellite.

    4. Re:Reliability by TWX · · Score: 4, Insightful

      Still, there are obstacles. SpaceX still needs to demonstrate the ability to consistently produce and launch rockets many times a year after the June accident caused an unexpected, six-month setback, something it will do with several flights planned for the weeks ahead.

      Just because it's relatively cheap to use Space X, if I have a 50-50 ( better or worse) chance that my $100 million satellite that took several years to design and build is going to get blown up, I'll pass.

      I fully expect that they'll have a tiered price structure. First, the cost of a brand-new launch won't have to be $60,000,000+ if they expect to launch the rocket again. Obviously it'll be the most expensive and will probably see the most use for the most critical launches and for manned-launches once they're man-rated, but if they expect to launch the same rocket assembly a half-dozen times then that launch might cost $20,000,000 or $30,000,000, or less than half of the cost of a one-flight rocket. Limited-reuse rockets might fetch $10,000,000 to $20,000,000 dollars for important but not absolutely critical launches where budget is important but so are timetables, and less than $10,000,000 for launches on older rockets where the loss of payload isn't that big of a deal, like replacing GPS satellites or dealing with routine communications satellite replacement over time.

      If this comes to pass, even if a customer insists on brand-new rockets for their launches, so long as there are customers interested in budget launches, the first launches will get cheaper.

      --
      Do not look into laser with remaining eye.
    5. Re: Reliability by SuricouRaven · · Score: 1

      Satellites don't have to deal with launch windows that much. That's more for interplanetary systems. Sats do have launch windows, they just come very frequently. Weather is more of a concern.

    6. Re:Reliability by zippthorne · · Score: 2

      How much does your $100 million satellite cost per-unit if you build five of them, instead? If a launch also costs $100 million, you might not bother, but if a launch costs $1million, would it be worth it to build enough to have a reasonable chance of success across several launches?

      --
      Can you be Even More Awesome?!
    7. Re: Reliability by Anonymous Coward · · Score: 1

      GEICO saved me 20% on my launch insurance

    8. Re:Reliability by Anonymous Coward · · Score: 4, Insightful

      Satellites don't inherently have to be that expensive, the only reason they are is that you can't afford to launch another one when the one you have fails. Because launches are so expensive it makes sense to sink money into making the sat as reliable and long living as possible. If launches were free you could whip up a functional comms sat for thousands or tens of thousand and if one fails just lob another one. The cost of payload depends on launch cost, with half the launch cost you can make the sat half as reliable, for half the cost and just lob two of them.

    9. Re: Reliability by Anonymous Coward · · Score: 2, Insightful

      You're gratuitously abusing statistics viz. track record, and you know it.

      SpaceX actually has a far better track record at this point in general rocket dynamics and development than NASA or Arianespace, and though I haven't checked, I am reasonably certain that is true for any of the various space transportation outfits that have ever existed in the entire (brief) spacefaring history of man.

      By the way, if you aren't willing to entrust your satellite to the tender mercies of the current state of technology, don't build it. There are always going to be significant risks in LTO from Earth's surface, similar ones in LTO from any body's surface, and other types of risks when injecting an object into orbit from microgravity environments. That's the way it is.

      Speaking only for myself, I'm glad you didn't bring that mentality to NASA or, indeed, any of the other spacefaring agencies. You wouldn't have made it past the Phase I interviews with your abilities in risk assessment.

      Happy Holidays from someone who works in space transportation. :)

    10. Re:Reliability by TWX · · Score: 1

      Yep. It's kind of like why nearly all cars in Singapore are high-end luxury cars- the parking spaces cost something like $150,000 a year. They're so expensive that if you can afford the parking space it's not an issue to put a $100,000 car in it. Same with upbuilding a limo- if it's $50,000 to cut up a sedan and turn it into a limo then there's not a lot of reason to start with a Chevrolet at $30,000 compared to a Cadillac at $50,000.

      --
      Do not look into laser with remaining eye.
    11. Re: Reliability by ArmoredDragon · · Score: 1

      Because his arguments match all of about 0% with reality he's probably one of those "I don't like the private sector because megacorps are evil and therefore the government does it best" types who have been reading too many cyberpunk novels in his parent's basement. They've been coming out of the woodwork a lot since SpaceX made a pretty historic spaceflight achievement.

    12. Re:Reliability by swillden · · Score: 3, Informative

      Just because it's relatively cheap to use Space X, if I have a 50-50 ( better or worse) chance that my $100 million satellite that took several years to design and build is going to get blown up, I'll pass.

      SpaceX has launched 20 times, with one failure. So, that's a 5% chance of loss, not 50%, assuming they maintain this success rate.

      --
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    13. Re: Reliability by Anonymous Coward · · Score: 0

      SpaceX actually has a far better track record at this point in general rocket dynamics and development than NASA or Arianespace, and though I haven't checked, I am reasonably certain that is true for any of the various space transportation outfits that have ever existed in the entire (brief) spacefaring history of man.
      [...]
      You wouldn't have made it past the Phase I interviews with your abilities in risk assessment.

      Happy Holidays from someone who works in space transportation. :)

      Since SpaceX is one of those companies where half the recruitment process is, "Do you drink the koolaid?" I'm going to take a good guess at where you work...

      By what ridiculous measure do you determine SpaceX to have "a far better track record at this point in general rocket dynamics and development"? Compared to the developments of the past century, SpaceX's incremental improvements are short chapters in a thick book. Its engineers have the potential to make a significant contribution to advancement of the art, but for now we have little more than a proprietary invention which has worked once.

    14. Re:Reliability by arth1 · · Score: 1

      Also, how much of the $60 million that the stage costs is due to the extra hardware/software and special parts needed for making it possible to land it again?
      And how much more fuel do you burn?
      And how much more expensive it is per unit when they build fewer units because they re-use them?

      The space shuttle program ended up being extremely expensive compared to rocket launches.

    15. Re: Reliability by Anonymous Coward · · Score: 0

      But the gecko died after reaching orbit.

    16. Re:Reliability by eth1 · · Score: 2

      Just because it's relatively cheap to use Space X, if I have a 50-50 ( better or worse) chance that my $100 million satellite that took several years to design and build is going to get blown up, I'll pass.

      Well, it kind of depends on your mission and payload. If you have a really expensive one-of-a-kind payload, I'm sure you can still specify you want a new boost stage. It will cost more, but since it can be recovered, probably still not as much as a throw-away one.

      On the other hand, say you're someone like, oh, Orbcomm, that's launching tons of tiny satellites in multiple launches. Over several launches required to get a constellation into orbit, the cost of a single lost payload might actually be less than saving $30 million or whatever on each of five launches.

    17. Re: Reliability by Anonymous Coward · · Score: 0

      Boeing, Lockheed and others have been doing it before NASA even existed. It's impossible to dislike private sector involvement without having a problem with pretty much every single one of NASA's practical developments. It is definitely possible to think SpaceX's achievements are overrated, though.

    18. Re: Reliability by Anonymous Coward · · Score: 0

      How often have others done the same? Give the technology some time to mature. They are still trsting the concept and technology. If it works traveling becomes 100 times cheaper. That would be a huge improvement.

    19. Re:Reliability by multi+io · · Score: 1

      Still, there are obstacles. SpaceX still needs to demonstrate the ability to consistently produce and launch rockets many times a year after the June accident caused an unexpected, six-month setback, something it will do with several flights planned for the weeks ahead.

      Just because it's relatively cheap to use Space X, if I have a 50-50 ( better or worse) chance that my $100 million satellite that took several years to design and build is going to get blown up, I'll pass.

      So I'm guessing (and I'm more or less an interested layman here) it would depend o the cost of the payload. Even if reusable rockets turn out to be less reliable, they'd still open up new possibilities IF they're substantially cheaper. If cheaper launches become available, that opens the market up for new, less expensive types of payloads that nobody would've thought of before. If your payload costs two million dollars to build (and to build again if you lose one), you'd probably launch it with the one-million-dollars-per-launch vehicle that's three times more likely to explode. If your payload costs one BILLION dollars, you probably[*] launch with the 60 million per launch vehicle that's three times less likely to explode, because the launch costs are just 6% of your payload anyway. But the thing is, that 2 million dollar payload would not be launched AT ALL if the cheap launcher wasn't available (at least not if the payload is heavy enough so it can't be launched with 10 others on the same flight).

      [*] Even that's not an automatic no-brainer decision if you're thinking of buying one hundred one-billion dollar payload launches and want to have as many dollars in orbit per million dollars expended as possible -- in that case you might launch even the expensive payloads with the cheaper launcher.

    20. Re:Reliability by TechnoCore · · Score: 1

      How much does your $100 million satellite cost per-unit if you build five of them, instead? If a launch also costs $100 million, you might not bother, but if a launch costs $1million, would it be worth it to build enough to have a reasonable chance of success across several launches?

      Not only that, but the fact that it cost a fraction to launch will make make it worthwhile to build super cheap satellites, made of everyday junk electronics. The way it works today is like since it is so expensive to launch, you are basically forced to build a very expensive satellite to go with it. 1 million dollar launch means thousands of universities could send out space based telescopes, by them selves using off-the-shelf hardware.

    21. Re:Reliability by TechnoCore · · Score: 2

      That $100 million satellite is that expensive, since the launch cost has been so high. Because once you get the satellite up it has to work for years flawlessly or you cannot make up for that launch cost. If the launch cost is $1 million, you can launch all sorts of cheap hardware instead, since losing it means very little in comparison.

    22. Re:Reliability by ColdWetDog · · Score: 2

      I'm waiting for a 'slightly used' one to show up on e-bay. Then we'll know that the technology has arrived.

      --
      Faster! Faster! Faster would be better!
    23. Re:Reliability by ColdWetDog · · Score: 4, Insightful

      The space shuttle program ended up being extremely expensive compared to rocket launches.

      The Shuttle was the poster child for how NOT to do reusable. Government spec with 10 mission requirements orthogonal to each other, half of which are not technically possible at time of design while development is spread out over ever ZIP code in the country.

      Elon can't be dumber than Congress. Unpossible.

      --
      Faster! Faster! Faster would be better!
    24. Re:Reliability by ColdWetDog · · Score: 1

      Correction: Elon can't be dumber than Congress and the Air Force put together.

      I suppose, however, that this would be damning by faint praise.

      --
      Faster! Faster! Faster would be better!
    25. Re: Reliability by jrvz · · Score: 1

      For a while, customers will pay extra for a brand new booster. Eventually, SpaceX will have to offer a discount to persuade customers to trust their payload to a rocket on its maiden flight.

    26. Re:Reliability by Kjella · · Score: 0

      How much does your $100 million satellite cost per-unit if you build five of them, instead? If a launch also costs $100 million, you might not bother, but if a launch costs $1million, would it be worth it to build enough to have a reasonable chance of success across several launches?

      Depends on the nature of the satellite, I would think. Like the mirrors for space telescopes are ridiculously expensive high-precision work where building a spare just in case is out of the question. Other satellites are designed to be part of a series like the GPS satellites, where you're already doing some form of serial production and extras can be kept as spares or used to retire existing satellites early. And then you probably have some in between, where they're fairly ordinary but you don't really need more than one. But if you've kept all the documentation and extra parts where you have some kind of unique production run or setup/testing costs that you'd like to avoid doing again, the cost for creating another satellite on-demand could be quite reasonable.

      --
      Live today, because you never know what tomorrow brings
    27. Re: Reliability by Anonymous Coward · · Score: 0

      If SpaceX has been playing with 50-50 odds and succeeded 19/20 times, they should have gone to Vegas and put $100M on red a couple dozen times.

    28. Re: Reliability by MrLogic17 · · Score: 4, Informative

      [Citation Needed]
      Rockets are not coins. So far, the failure rate seems to be 5%. If the one failure was a statistically early event and/or the issue around that one failure is fixed, the true failure rate will be much lower.

      We need a larger data set to firmly set the real failure rate, but there is no evidence of 50/50.

      In fact, if a per launch odds really were 50/50, the probability of 19 successful launches would be 1/(2^n) or 0.00000190734 or 0.000190734%

      TLDR; you have no idea what you're talking about. Take a stats class.

    29. Re: Reliability by Anonymous Coward · · Score: 1

      Simple math:
      Either it fails, or it doesn't.
      That's a 50:50 chance.

      Wait....

    30. Re:Reliability by Dutch+Gun · · Score: 1

      Is a new rocket really the best option for a manned or otherwise critical launch? Wouldn't you rather be on the rocket's second or third ride up instead of the first?

      --
      Irony: Agile development has too much intertia to be abandoned now.
    31. Re:Reliability by Anonymous Coward · · Score: 0

      SpaceX should consider themselves successful in this ONLY if they can charge more for used boosters than for new ones. Who would want to use an untried one when you can fly a proven one? The first flight(s) of an airliner are 'worthless' in the sense that they don't put people on them. The hope is that it will become like that.

    32. Re: Reliability by Anonymous Coward · · Score: 0

      I am actually all for SpaceX doing what they are doing

      But posting something incorrect as facts is not going to help their case.

      They've tested their 1st stage to be good for about 40 times. Considering the costs for repair and testing this is not going to make things cheaper by 100 times.

    33. Re: Reliability by swillden · · Score: 2, Insightful

      Wrong. That is 5% failure over time. Each individual launch is still 50/50

      The probability that you got a good grade in your probability & statistics class is very low.

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      Note to ACs: I usually delete AC replies without reading them. If you want to talk to me, log in.
    34. Re:Reliability by CptJeanLuc · · Score: 1

      SpaceX has launched a previously launched vertically self-landing rocket exactly zero times, so statistics is not going to provide anything in the probabilities department. "Assuming they maintain this success rate" is a rather big assumption.

    35. Re:Reliability by demented_hedgehog · · Score: 1

      It costs you 100 million to make the first one. After that they should be pretty cheap. So make a few.

    36. Re:Reliability by crbowman · · Score: 1

      Yes, but at $1million are you still going to build $100 million satellites? Perhaps you'd build a 10x$1million satellites with an estimated life time of 2 years, and spend $1million every 2 years to replace it (presumably with a lighter better performing version?). I don't know what a launch costs for $100 million satellite but assuming the dedicated rocket costs $60million your total cost is $160 million. If you change this so the total cost is now $101 million, it seems to be that you launches don't have to be much more successful than about 2 out of 3 before the economics make sense.

    37. Re:Reliability by Anonymous Coward · · Score: 0

      Yes but your competitor with use reusable rockets and launch satellites that cost a fraction. They'll lose some for sure. Rockets will blow up, the satelites will stop working. But at the end of the day they may still have 10x the amount of birds in the sky you do for the same money. Who is going to stay in business?

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

      Satellites don't inherently have to be that expensive,

      If launch gets cheaper and they start lobbing up a bunch of 'disposable' satellites, then you'll have to start engineering replacements to withstand all the space junk that will be flinging around up there before too long.

    39. Re: Reliability by Anonymous Coward · · Score: 0

      You could at least try to get your facts right. Singapore requires a certificate of entitlement to own a car which was up to around $100k sing while I was there. So why buy an 8k car and be at 108k when you can buy a 50k car and be at 150k. Parking is only an issue in cbd.

    40. Re:Reliability by rasmusbr · · Score: 1

      It also makes sense to keep adding capabilities and longevity until your satellite costs a lot more than the launch price.

      A company that launches something into space faces the same sort of thinking that you face when you want to order something online when shipping isn't included in the price. If shipping is $15 you are probably not going to buy something that costs $30. If you really need to order the $30 item then you are going to be strongly tempted to order additional items that you think you might want or need until your total purchase is something like $150, or whatever you deem enough to make the $15 shipping negligible in comparison.

      I guess you might say that SpaceX is aiming to be to space what sub-$1 shipping would be to online retail.

    41. Re:Reliability by catchblue22 · · Score: 1

      Still, there are obstacles. SpaceX still needs to demonstrate the ability to consistently produce and launch rockets many times a year after the June accident caused an unexpected, six-month setback, something it will do with several flights planned for the weeks ahead.

      Just because it's relatively cheap to use Space X, if I have a 50-50 ( better or worse) chance that my $100 million satellite that took several years to design and build is going to get blown up, I'll pass.

      One could make the argument, especially during the earlier launches, that using a rocket that has been tested three or four times already might give more reliability, and not less. Time will tell.

      --
      This and no other is the root from which a tyrant springs; when first he appears as a protector - Plato (423 to 327 BC)
    42. Re:Reliability by Ol+Olsoc · · Score: 1

      Yep. It's kind of like why nearly all cars in Singapore are high-end luxury cars- the parking spaces cost something like $150,000 a year. They're so expensive that if you can afford the parking space it's not an issue to put a $100,000 car in it. Same with upbuilding a limo- if it's $50,000 to cut up a sedan and turn it into a limo then there's not a lot of reason to start with a Chevrolet at $30,000 compared to a Cadillac at $50,000.

      Your parking lot analogy has another facet. If we make satellites disposable, we better have good ways to get them out of the way if they fail. Because for as big as space is, orbital mechanics makes certain orbits, certain space real estate, very desirable, and you'll find them in those orbits. So if we're throwing up relatively unreliable sats, we better have a very reliable way to get them out of the desireable orbits when they quickly fail.

      Plus When you get outside of the earth's atmosphere, you really need well built devices just to function for much time at all

      --
      The shepherds did so well protecting the flock that the sheep no longer believed that wolves existed.
    43. Re:Reliability by Ol+Olsoc · · Score: 2

      How much does your $100 million satellite cost per-unit if you build five of them, instead? If a launch also costs $100 million, you might not bother, but if a launch costs $1million, would it be worth it to build enough to have a reasonable chance of success across several launches?

      Depends on the nature of the satellite, I would think. Like the mirrors for space telescopes are ridiculously expensive high-precision work where building a spare just in case is out of the question.

      What is not known by many, is that there is another, and rather flawless Hubble Telescope mirror made by Eastman Kodak.

      http://airandspace.si.edu/coll...

      It's an interesting subject. I could have found the problem with the Perkin Elmer mirror withan led and a 5 dollar home made tester. It was a shameful thing that the good mirror is sitting in a museum on earth, while the flawed one has cost so many millions to fix.

      --
      The shepherds did so well protecting the flock that the sheep no longer believed that wolves existed.
    44. Re:Reliability by swillden · · Score: 2

      SpaceX has launched a previously launched vertically self-landing rocket exactly zero times, so statistics is not going to provide anything in the probabilities department. "Assuming they maintain this success rate" is a rather big assumption.

      Did you read the thread? The claim was that there was a 50% chance of complete loss of the cargo. But SpaceX has launched 20 Falcon 9s, and only lost one. The fact that this is only the fourth time they attempted to land the first stage, and the first time they succeeded, is completely orthogonal to the question of cargo survival, because that has nothing to do with the landability of the first stage.

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    45. Re:Reliability by mcswell · · Score: 2

      IANARS, and I'm not denying you have a point, but I think there's a lot of vibration inside a rocket. Some of it chaotic, some of it periodic. Sooner or later that vibration's going to shake something loose. Could be a fuel line weld, could be a lot of things. The longer the rocket fires (and the more times it starts up), the more likely it is that something's going to break next time.

      There's also the issue of testing, because testing can cause something to break that was working before. That's what happened to Apollo 13.

    46. Re:Reliability by Anonymous Coward · · Score: 0

      Am in Singapore.

      Never heard that you have to "buy" or "lease" parking spots in that manner. But there is a Certificate of Entitlement which you have to bid for before you buy a car, and that can hit 60k~100k each.

      And that's why people rather buy a more expensive car, since the certificate to buy any car itself is so expensive.

    47. Re:Reliability by Sir+Holo · · Score: 1

      Satellites don't inherently have to be that expensive, the only reason they are is that you can't afford to launch another one when the one you have fails. Because launches are so expensive it makes sense to sink money into making the sat as reliable and long living as possible. If launches were free you could whip up a functional comms sat for thousands or tens of thousand and if one fails just lob another one. The cost of payload depends on launch cost, with half the launch cost you can make the sat half as reliable, for half the cost and just lob two of them.

      Satellites and their launches are expensive because they are expensive.

    48. Re:Reliability by Sir+Holo · · Score: 1

      The space shuttle program ended up being extremely expensive compared to rocket launches.

      The Shuttle was the poster child for how NOT to do reusable. Government spec with 10 mission requirements orthogonal to each other, half of which are not technically possible at time of design while development is spread out over ever ZIP code in the country.

      Elon can't be dumber than Congress. Unpossible.

      My family has had the same broom for five generations. We use it daily.

      Sure, we occasionally replace the bristles. And yes, other times, we replace the handle. But it is the same broom that my ancestors used!

    49. Re:Reliability by Gavagai80 · · Score: 1

      Also, how much of the $60 million that the stage costs is due to the extra hardware/software and special parts needed for making it possible to land it again?

      Must be a negligible amount, since they're the cheapest on the market already and the intent of reuse was built into their designs from the beginning.

      And how much more fuel do you burn?

      It's safe to assume the additional fuel cost in $ is 5 digits, so negligible compared to the other costs involved in space flight.

      And how much more expensive it is per unit when they build fewer units because they re-use them?

      Considering they're currently in a developmental stage where they're changing things all the time, and this was actually the first flight of a new configuration of Falcon 9, it's safe to say they will not be building fewer units -- the $60 mil, even though it's the lowest price out there, has been for an experimental evolving rocket rather than a mass production model. They're likely to need to build more units as lowered prices lead to more demand.

      --
      This space intentionally left blank
    50. Re:Reliability by Anonymous Coward · · Score: 0

      SpaceX did not fail, their supplier failed to create a critical component up to specifications.

      <TinfoilHat> Perhaps someone on the inside tried to kill the competition? </TinfoilHat>

    51. Re: Reliability by Anonymous Coward · · Score: 0

      The reason that satellite used such an expenisve mirror is that they wanted the best image quality at the lowest weight / launch cost.

      If launch costs were cheaper, we could toughen-up a ground-based telescope and launch it.

    52. Re: Reliability by Anonymous Coward · · Score: 0

      Now that SpaceX has a previously flown first stage to take apart and evaluate, they may get more reliable rockets than the super careful people who have never seen a previously flown stage that was recovered intact.

    53. Re:Reliability by Dutch+Gun · · Score: 1

      Yep, that's true. I suppose only time will tell if new rockets actually turn out to be more reliable than used, or even any statistical difference at all. The great thing about recovering the rocket like they do is that they can perform post-flight structural analyses on the entire system and strengthen / reinforce any components that appear to be suffering more stress because of the repeated launches.

      When safety is prioritized, humans can actually build highly complex machines that are put under significant stress and are still amazingly reliable - modern airliners are one example of this. I don't see any reason why we can't eventually achieve the same high levels of efficiency and reliability with rocket launches. It just requires a lot of engineering experience. Engineering is about pushing boundaries, making mistakes, analyzing *why* those mistakes occurred, and then correcting them in the next iteration.

      --
      Irony: Agile development has too much intertia to be abandoned now.
    54. Re: Reliability by Anonymous Coward · · Score: 0

      Would not the insurance premium adjust for the added risk, making it more expensive?

    55. Re:Reliability by CptJeanLuc · · Score: 1

      Yes, I can read. The idea about the (presumably randomly chosen) 50/50 number, should be that there may be a higher risk associated with a launch in which the first stage is reused (and thus perhaps less reliable if the landing damaged the stage in some way which is not correctly identified and/or handled in preparing it for reuse), rather than using a new one. If the first stage blows up before separation, the payload is lost. For an example, search for "Ariane 5 first launch".

      Kind of like you would not be able to use statistics that "out of 1000 apples sold in stores, x apples are rotten or unedible", as a reasonable predictor for claiming the same x/1000 ratio should hold for bananas. They are not the same fruit. Until technologically proven and properly tested, SpaceX launches with reused first stages are not the same as launches with new reusable first stages.

    56. Re: Reliability by Anonymous Coward · · Score: 1

      Yeah, he or she must be drinking kool-aid because they don't agree with you.

      Look at number of launch attempts vs failures for any rocket enterprise...the USA and Russians had an abysmal record early in their development...hell NASA has lost 17 astronauts which some would call the ultimate price. Granted SpaceX has has a mountain of previous experience to work with but for my money they are doing incredibly well given the requirements and time frames in which they have achieved what they have.

      Also landing a first stage as well as they did lately is more than an 'incremental improvement' if it proves a success, it's a real game changer.

      I haven't been this excited about the future of space travel since watching Columbia launch for the first time all those years ago and IMO SpaceX is the one to be watching for future developments.

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

      Even if it becomes 10x cheaper, it's still a huge milestone.

    58. Re:Reliability by Anonymous Coward · · Score: 0

      Down under we call it "Ned Kelly's axe"...

      its had 4 new handles and 2 new heads, but it's still Ned Kelly's axe! =D

    59. Re:Reliability by Anonymous Coward · · Score: 0

      But on the flipside, space-junk could become a real problem....IMO some judicious thought is required before allowing every man and his dog to have a satellite...after all these aren't smartphones, it's stuff zinging around in the space above the Earth...IMO if we wish to return to the Moon or even go to Mars the moderation of space junk is something which needs to be taken seriously.

    60. Re: Reliability by Anonymous Coward · · Score: 0

      Flight spares add about 2% to the final price for one-offs like science probes.

      This us obvious to anyone who realises that hundreds of test models and hundreds of man-years go into such missions. The actual hardware is a tiny part of the cost and it's like that because mission failure is not an allowable option .

      For common models your flight spare is just another item on the production line.

      In both cases, lowering the launch cost is important but launchers aren't the majority of the final price. Labour costs are.

    61. Re:Reliability by TheReaperD · · Score: 1

      I wouldn't be surprised if 90%+ of SpaceX's problems have been trying to get suppliers to actually supply equipment at contracted specifications. Given how quick and sloppy that most manufacturers have gotten over the years, trying to get this level of precision must be a nightmare.

      --
      "Be particularly skeptical when presented with evidence confirming what you already believe." -
  2. Reliability of refurbished booster is unknown by Anonymous Coward · · Score: 3, Interesting

    The wear mechanisms are poorly understood and this compounds the difficulty of predicting the reliability of launches. Only time will tell if the Falcon technology can operate more reliably than the historic 1-2% failure rate. I am not optimistic. A 1% catastrophic failure rate is nothing to boast about, even for a reusable launcher.

    1. Re:Reliability of refurbished booster is unknown by XXongo · · Score: 4, Insightful
      Exactly. The question of how much reusability will lower costs depends critically on how expensive it is to refurbish, as well as how much performance you trade off to save delta-V for landing the stage.

      This is complicated somewhat by the fact that rocket engines have significant economy of scale in production: if you reuse each one, say, ten times, your production rate is ten times lower, so the engines are more expensive.

      So it's not completely obvious how much savings you get. It seems pretty clear you get some. But how much?

    2. Re:Reliability of refurbished booster is unknown by WindBourne · · Score: 1

      Reliability is unknown by YOU and I. BUT, SpaceX already has a clue of what it will take. The question is, have they over or under estimated. Keep in mind that Musk HAS actually under estimated before. His first rocket blew up for a reason. In addition, he thought that a simple parachute would enable him to capture the first stage. Both were failures. Thankfully, he changed his approach.

      I suspect that SpaceX has over estimated this and these will likely do at least 10 launches without much fix up. The question is, will they go further?

      --
      I prefer the "u" in honour as it seems to be missing these days.
    3. Re: Reliability of refurbished booster is unknown by Anonymous Coward · · Score: 1

      Landing in Salt water is bad for everything. Landing on the ground is going to be somewhat damaging for something as large as a first stage rocket. A little extra fuel is relatively cheap since parachutes have weight as well.

    4. Re:Reliability of refurbished booster is unknown by Anonymous Coward · · Score: 0

      SpaceX produces fewer than a dozen or so rocket stages per year right now (which is still more than most rocket makers). I think their plan is to be able to launch several dozen cores per year (including the 3-core Heavy version) without needing to scale up production. So the per-engine cost might be comparable to what it is today, assuming they can find enough customers for the higher flight rate. Or even if it's more expensive, you rarely have to replace engines; so what if you pay 2x per engine if you only need 1/10th the number of engines.

    5. Re:Reliability of refurbished booster is unknown by Anonymous Coward · · Score: 0

      This is complicated somewhat by the fact that rocket engines have significant economy of scale in production: if you reuse each one, say, ten times, your production rate is ten times lower, so the engines are more expensive.

      That's assuming demand is static. If you keep your production rate steady and use the higher launch capacity gained by reuse to lower launch costs then you drive demand for the service up. SpaceX would not have a goal of getting people to spend less on launches but to make the service more efficient to drive up demand and expand the industry. How that will turn out is yet to be seen but they certainly aren't trying to save anyone money to spend on something else they are trying to build their own business up.

    6. Re: Reliability of refurbished booster is unknown by Anonymous Coward · · Score: 0

      This logic is perfect...damn it we need a space elevator!

    7. Re: Reliability of refurbished booster is unknown by Anonymous Coward · · Score: 0

      well
      Said by a ULA troll

    8. Re:Reliability of refurbished booster is unknown by cpt+kangarooski · · Score: 1

      Why would you want to cut your production rate? Both reusability and economy of scale are essential in cutting launch costs. SpaceX ought to be working on internal projects that can use any excess launch capacity until there are enough customers, though, preferably ones that will help further the business. (Like electric space tugs and refueling / repair / refurbishment drones)

      --
      -- This and all my posts are in the public domain. I am a lawyer. I am not your lawyer, and this is not legal advice.
    9. Re:Reliability of refurbished booster is unknown by Anonymous Coward · · Score: 0

      And how many exploding 2nd hand rocket motors will it take to erase those savings?

    10. Re: Reliability of refurbished booster is unknown by billdale · · Score: 0

      You disparage SpaceX for not using parachutes-- yes, parachutes were used for smaller components-- mainly capsules-- during early missions with smaller craft, and with tiny model rockets, but if you do not understand the principle of "problems of scale", you need to look it up. The simplest example of a problem of scale would be that if you dropped a glass sphere one-tenth of an inch from a height of 10 feet onto a hard steel surface, it is likely to survive intact. If you drop a glass sphere 20 feet in diameter from a "height" of just one inch, you can be sure it will shatter to pieces. The Dragon booster rocket is more thanca dozen stories tall--the biggest ever-- and would definitely require a rocket firing to slow it down before hitting the ocean, even with a huge parachute, or the entire assembly would be crushed on impact with the water. You are better off doing it as SpaceX did it, landing softly on a pad. This guy succeeded in bringing this huge booster back intact--he does not warrant your sarcastic comments, but enthusiastic cheers for such an incredible feat. In the future 80 you do not have the slightest background in the subject at hand you are best not to be showing how foolish and clueless you are.

    11. Re:Reliability of refurbished booster is unknown by TheReaperD · · Score: 1

      Well, he's trying to find a way to reduce costs of space launches. That means testing the limits of what corners he can cut on equipment and still have the rockets complete their goals reliably. Except for the rocket that exploded on takeoff, all of the launch missions have been a success, it's just the after completion recovery tests were failures until now. Now they are taking apart the safely landed booster to see what damage it sustained during the round trip so they can see what they need to refurbish or replace to keep the cycle going in the future. If they can keep the cycle going and don't have to build new boosters each time, it will reduce the costs even further. By how much will be determined by how much they have to refurbish the booster each time.

      --
      "Be particularly skeptical when presented with evidence confirming what you already believe." -
  3. Let's make some assumptions... by CrimsonAvenger · · Score: 5, Interesting

    1) The first stage is 2/3 the total cost to launch. Which would be $40 million.

    2) They can renovate the first stage for $5 million.

    3) They can get five launches from a first stage (original plus four more).

    So, $60 million for five launches, plus the $20 million for the second stage x5.

    Which comes to $32 million per launch. A bit more than half the current price.

    Now, I consider those pessimistic assumptions.

    Alternately...

    If we replace (3) with 15 launches per first stage, we get $28M per.

    If we replace (2) with $1M per launch, we get $29M for five launches, $23.75 per launch for 15 launches.

    Big picture: reusing the first stage only will allow them to drop prices by 40-60%.

    Now, if they can reuse the second stage also, we're talking some real money....

    --

    "I do not agree with what you say, but I will defend to the death your right to say it"
    1. Re:Let's make some assumptions... by Xac · · Score: 0, Interesting

      Reusing the second stage will never be an option because it goes halfway around the world. We also have to assume loss of the first stage to be a common event, since they've only managed to do it once so far.

    2. Re:Let's make some assumptions... by beltsbear · · Score: 4, Interesting

      With SpaceX being allowed to land on actual land I think they will have nearly 100% recovery. The second stage probably won't be recovered but the distance is really not the issue. The weight of recovery equipment directly comes from payload capacity and so far there is no lightweight heat shield that can do the job. Once that secret sauce is found they can de-orbit the second stage wherever they want to.

    3. Re:Let's make some assumptions... by Anonymous Coward · · Score: 1

      "Big picture: reusing the first stage only will allow them to drop prices by 40-60%."

      Yeah. Only. Considering the sums, that's clearly small potatoes and hardly worth mentioning..

    4. Re: Let's make some assumptions... by gerf · · Score: 4, Interesting

      They plan on making every stage reusable. Musk's long range goals include sending someone to Mars. To do so, he wants to be able to send a lot of mass into upper orbits for as low of a cost as possible.

    5. Re:Let's make some assumptions... by photonic · · Score: 2

      Exactly this. What you are describing is the economic equivalent of Amdahl's law for speedup of using parallel computing: even with infinite parallelism (infinite reuse), theoretical minimal costs are dominated by non-parallelizable computation (per launch costs). Elon keeps repeating the talking point that fuel is cheap so launches can be 100x cheaper. This ignores recurring costs of launch operations, manpower, non recoverable 2nd stage, inspections and repairs. Still, lowering costs by a factor 2-3 would probably be enough to kill competition ...

      --
      karma police: arrest this man, he talks in maths; he buzzes like a fridge, he's like a detuned radio. [radiohead]
    6. Re: Let's make some assumptions... by Anonymous Coward · · Score: 0

      We cannot assume any kind of thing from such a fantastically-limited dataset.

    7. Re:Let's make some assumptions... by painandgreed · · Score: 2

      Reusing the second stage will never be an option because it goes halfway around the world.

      Ten years ago, I'd bet we'd say that recovering the first stage would never be an option. In another ten years, if everything works out, recovering the first stage is routine, and launches are as cheap as they can get, they'll start looking at recovering the second stage. Now I wouldn't be surprised if it eventually sprouts wings and flies back to its launch pad.

    8. Re: Let's make some assumptions... by Anonymous Coward · · Score: 0

      We can assume anything we want.

    9. Re:Let's make some assumptions... by fermion · · Score: 1
      The cost saving will only be determined with practice. One reason the Space Shuttle was a not as successful as hoped was because the SRB likely resulted in no cost savings because most parts did not survive, and the only thing that reused was the shell. Likewise the shuttle itself essentially had to be rebuilt.

      This will be same thing. How much of the avionics, pumps, etc, can survive launch and landing. How much more does it cost to produce these items so they can survive. How much does it costs to repair and retrofit. The thing about these systems is that involve domains that we have little experience. We learn by doing, and theory does not always match what we see in the real world. One of incredible thing about the Apollo program is that we had to learn how to manufacture what we wanted, as mostly it had not been done before. The question is has 50 years of aerospace manufacturing given us the ability to produce a reusable rocket. We will see.

      --
      "She's a scientist and a lesbian. She's not going to let it slide." Orphan Black
    10. Re:Let's make some assumptions... by WindBourne · · Score: 1

      First off, I suspect that first stage is a LOT more than 2/3 of costs. Much larger size. 9 engines vs. 1. the CPU/software will be comparable, but it should be minor. Has a much bigger hydraulic system to handle the rudders and legs. So, that means that first stage is probably closer to 3/4 to 80% of the costs.
      In addition, Musk has said that these are designed to go for 10 launches. Assuming that they estimate that correctly, then saving are likely around 66-75%.

      --
      I prefer the "u" in honour as it seems to be missing these days.
    11. Re:Let's make some assumptions... by TechnoCore · · Score: 1

      Don't forget they are cutting costs of the booster all the time by improving on manufacturing techniques and researching new materials.

      Renovating the booster should not cost $5million. Their goal is to have it flyable within 24hrs, which means it can't cost much more than the overhead cost of having the infrastructure for a launch/landing site.

    12. Re:Let's make some assumptions... by Megol · · Score: 1

      Really? Landing a rocket (and a rocket stage is a rocket) have been tried for a long time so no, nobody with a hint of clue would say "never [be] an option" - just f***ing hard.
      And we already know it is f***ing hard - as the amount of failures are more than the amount of successes. Including for SpaceX.

    13. Re: Let's make some assumptions... by short · · Score: 2

      Musk in some video said that reusing the stage 2 would be definitely possible but that he does not plan to do that. That he has more interesting challenges ahead such as the Mars.

      That surprised me a bit, he employs engineers to implement the reusability.

    14. Re:Let's make some assumptions... by XXongo · · Score: 1

      Don't forget they are cutting costs of the booster all the time by improving on manufacturing techniques and researching new materials.

      The lower the cost of the booster, the less the financial incentive for re-use.

    15. Re: Let's make some assumptions... by Anonymous Coward · · Score: 1

      I think the plan is to work on second stage reusability for the much bigger "BFR" rocket where the payload margins aren't as tight.

    16. Re:Let's make some assumptions... by Anonymous Coward · · Score: 0

      Apparently some relatively unknown government agencies from America and Europe concluded booster reusability is uneconomical.

      I have more faith in "chief designer" Elon Musk though. After all, Elon is a economics major in college.

    17. Re: Let's make some assumptions... by Anonymous Coward · · Score: 0

      100x is theoretical maximum assuming resource prices being the same. His point is that there is huge unused potential and he will try to make it work.

    18. Re:Let's make some assumptions... by darkmeridian · · Score: 1

      I would bet that the second stage would be recovered somewhere else, not near the launch site. By the time the second stage booster completes its burn, it's already very, very far away and going very, very fast. It would make more sense to try to land it in Africa or Europe or the Pacific rather than to make it fly back to the launch site.

      --
      A NYC lawyer blogs. http://www.chuangblog.com/
    19. Re:Let's make some assumptions... by Gavagai80 · · Score: 1

      It might be practical to give the second stage a full orbit to return to where it launched from. The problem is how to get it down without it burning up, since it'll be going I believe ~5x faster than the first stage.

      --
      This space intentionally left blank
    20. Re:Let's make some assumptions... by eric_t_duckman · · Score: 1

      According to his wikipedia page, he has a BS in physics and a BS in economics. Only one of those degrees is in a real science, the other is just more bs.

    21. Re:Let's make some assumptions... by Anonymous Coward · · Score: 0

      Maybe the "secret sauce" is to aerobrake slower in the thin atmosphere for several orbits and slowly come down so heat doesn't build up as badly? Burn a few times vertical at periapsis while horizontal motion decays into a suborbital trajectory, then aim retrograde using rcs and deploy a hypersonic drogue chute. Once speed is down to 1st stage velocities, then release the drogue and land exactly the same.

      Elon, you hiring?

    22. Re:Let's make some assumptions... by Anonymous Coward · · Score: 0

      OMG, someone thought of this 23 years ago.

      Hire that guy instead.

    23. Re: Let's make some assumptions... by Anonymous Coward · · Score: 0

      What about the cost for ground ops?

      What about liability insurance?

    24. Re: Let's make some assumptions... by Anonymous Coward · · Score: 0

      Since the first stage falls back to earth and is lost otherwise, it makes sense to recover it. However, considering that the second is already in orbit, would it make more sense to push it into a "junkyard" in space (maybe a Lagrange point) so that we can reuse the parts/ materials there?

    25. Re:Let's make some assumptions... by solartear · · Score: 1

      The boost stage is roughly 70% of the cost of a launch. So, if we're able to reuse it and refly it with minimal work between flights, and customers are comfortable with that - and it might take a few years for customers to get comfortable with that - then obviously there's as much as - ultimately - a 70% reduction from where things are today. - Elon Musk

      http://shitelonsays.com/transcript/spacex-press-conference-at-the-national-press-club-2014-04-25

    26. Re:Let's make some assumptions... by WindBourne · · Score: 1

      70% of the cost of the launch is not the same thing as 70% of the costs of building it.
      So, we have been looking at this first stage costing 70% of $60 million. However, Musk may have been referring to 70% of $140 million, which is the TRUE LAUNCH COSTS. If that is the case, then a 70% reduction on this is HUGE, since it means that a launch will then be less than 40 million instead of 140 million.

      --
      I prefer the "u" in honour as it seems to be missing these days.
    27. Re:Let's make some assumptions... by rpstrong · · Score: 1

      How much of the avionics, pumps, etc, can survive launch and landing.

      If they didn't survive the launch, the missions would have ended before orbit. And the beauty of the rocket powered, vertical landing is that the booster is being subjected to the same forces that it was designed to handle during launch - a kick in the tail, producing compressive loads. Those systems have essentially proven themselves even on the 'failed' attempts.

    28. Re:Let's make some assumptions... by fermion · · Score: 1

      Survive may have been imprecise.The difficulty, as shown with the Shuttle SRB, is knowing what is going to function well for a 2nd launch. Due the human safety factor, all components of the SRB was replaced after each launch. The challenge in this case will be to predict which components are degraded enough to require replacement, and which do not. Obviously failure is very costly, so these stoichiometrics are going to be what makes or breaks the reusability scenario.

      --
      "She's a scientist and a lesbian. She's not going to let it slide." Orphan Black
  4. Still a lot to learn by Anonymous Coward · · Score: 3, Interesting

    The wear mechanisms are poorly understood, and this compounds the launch risk. After decades of engineering work, heavy lift boosters still have about a 1% failure rate, If SpaceX can't beat that, then there is no glorious future for manned spacefight.

    1. Re:Still a lot to learn by beltsbear · · Score: 4, Interesting

      With low enough cost 0.1% is not a problem so long as the escape systems work. They can get there.

    2. Re:Still a lot to learn by saigon_from_europe · · Score: 4, Insightful

      The wear mechanisms are poorly understood

      Yes, they are, because until Monday, we had exactly 0 (zero) first-stages that have returned from their missions. Thing will change now.

      --
      No sig today.
    3. Re:Still a lot to learn by Anonymous Coward · · Score: 3, Insightful

      After decades of engineering work, heavy lift boosters still have about a 1% failure rate, If SpaceX can't beat that, then there is no glorious future for manned spacefight.

      Why not? It is a 1% failure rate without reusability. A 10% failure rate but with reusability means that you beat the cost of 1% failure rate by magnitudes.
      Then there is the way the Indian space programs does it. Cut down the cost enough to afford ten launches for the same cost as NASA has for one launch. With an 80% failure rate you still get more stuff up.

      Zero-tolerance is a great way to spend a lot of money without getting the results you pay for.
      I'm not saying that you want a 10% failure rate or even that 1% is good enough. But I know that the ideal failure rate you want is more than 0%. If you achieve 0% then you are not getting the most out of the money you put in.

    4. Re:Still a lot to learn by Anonymous Coward · · Score: 0

      A 10% failure rate but with reusability means that you beat the cost of 1% failure rate by magnitudes.

      It also means you're ten times as likely to lose your customer's payload. If a customer has a $100 million satellite to put up, and you've increased his risk by 1000%, being able put his gear up for $5 million instead of $50 million isn't quite the value proposition it might have been otherwise.

    5. Re:Still a lot to learn by Anonymous Coward · · Score: 0

      If it's only a $100M satellite, a 10% failure rate for $45M savings is still a win (expected loss value = $10.5M per flight, you could probably get insurance for $12M or something).

      Right now, many satellites cost more than $100M so the industry would have to shift to cheaper sats (it's already happening, but slowly). There's also the time/business cost of having to wait for a relaunch, exacerbated by the fact that SpaceX is currently the only provider that will be able to launch this cheaply for the near future, and failures are likely to ground the rocket for months pending investigation (although it should hopefully lead to bringing the failure rate down in the long run).

      In any case, risk-adverse customers will probably still be able to pay for a brand new rocket for less than the cost of most of SpaceX's competitors.

    6. Re:Still a lot to learn by trout007 · · Score: 1

      I disagree. The fatigue and fracture mechanics needs to be well understood just to get to this point. Now that they have recovered one that knowledge will be much better since they can inspect to see how close their analysis is. Not only will this be important for reusability but overall reliability and performance by giving better data on loads. For example Atlantis was 5-10% lighter than Columbia because of advances and lessons learned.

      --
      I love Jesus, except for his foreign policy.
  5. Elon Musk is pulling off impressive feats by TheReaperD · · Score: 5, Insightful

    Elon Musk and company have been making huge achievements and seems one of the few people in industry to take the long view of things and it's likely to pay off in the end even though the MBAs hate him at the moment.

    I, for one, welcome our new Martian overloard!

    --
    "Be particularly skeptical when presented with evidence confirming what you already believe." -
  6. What does it cost to just risk it? by Anonymous Coward · · Score: 2, Interesting

    Pretty much every mature industrial process takes a certain loss into consideration. If you know that 5% of manufactured goods fail then it might be cheaper to just make more of them and throw a few away to get to the desired amount rather than improve your manufacturing process.

    If you are just going to use the rocket to send supplies then the cost of the payload might be insignificant.
    At that point it might be worth to consider if it is cheaper to just risk it and reuse the rocket without checking it over. As long as you have a new one ready to be put to use you might end up being better off by just going for it.
    It seem to me that the main expense when it comes to space projects is the 0-tolerance for failure. If you accept that 80% of the missions fail you might be able to do it at 10% of the cost.

  7. Either way... by Anonymous Coward · · Score: 0

    this doesn't help humanity. It only helps corporations.

    1. Re: Either way... by Anonymous Coward · · Score: 0

      Exactly. The government-subsidized "science" is ruining this country. It harms so many families. We need to go back to a time before the Republicans destroyed this country.

    2. Re: Either way... by Anonymous Coward · · Score: 1

      And hurts children. Hurts children.

  8. The break down of 60 million is the key. by 140Mandak262Jamuna · · Score: 3, Interesting

    The 60 million cost includes the cost of manufacturing the components, inspecting them thoroughly, assembling them and inspecting and passing the assembly. They went for proven technologies and cheap materials, says the article. The rocket shell is relatively simple. The cost is in the rocket motor, the nozzle that holds the combustion products in plasma state, its cooling mechanism, pumps and controls. I am not sure how much of it can be inspected and re validated without extensive disassembly. I suspect most of the cost is in the inspection and certification of the vehicle rather than in the cost of individual components or the cost of assembling them.

    --
    sed -e 's/Chuck Norris/Rajnikant/g' joke > fact
    1. Re:The break down of 60 million is the key. by tlambert · · Score: 3, Interesting

      The cost is in the rocket motor, the nozzle that holds the combustion products in plasma state, its cooling mechanism, pumps and controls. I am not sure how much of it can be inspected and re validated without extensive disassembly.

      I keep waiting for them to replace the nozzle with an experimental version that uses a linear aerospike. The April 10, 2001 patent will be expiring in just about 5 1/2 years now...

    2. Re:The break down of 60 million is the key. by Anonymous Coward · · Score: 1

      If they have to take it apart, then they might as well not recycle at all, cost ends up the same. But they are actually aiming to have 0 overhaul between flights maybe wash the shoot off, but that's it. Simply eyeballing the rocket from outside to make sure there is nothing obviously damaged and going for another round. The engines should enable this, they have tested them on the ground for 40 some flights without maintenance in between and they did play around with grasshopper, so they probably are not bluffing here. Structure should also be eighter good to go or obviously damaged, so no disassembly or maintenance to be done there.

    3. Re:The break down of 60 million is the key. by Arnold+Reinhold · · Score: 4, Informative

      The Space Shuttle Main Engines, which push the envelope far more than SpaceX's Merlin, were reused up to 19 times. According to the Wikipedia article: "After each flight the engines would be removed from the orbiter and transferred to the Space Shuttle Main Engine Processing Facility (SSMEPF), where they would be inspected and refurbished in preparation for reuse on a subsequent flight. A total of 46 reusable RS-25 engines, each costing around US$40 million, were flown during the Space Shuttle program, with each new or overhauled engine entering the flight inventory requiring flight qualification on one of the test stands at Stennis Space Center prior to flight." There is also a chart of which engines were used on which flight. Musk and his team seem to have a clear engineering vision. This first landing of an orbital booster is just the beginning, but the potential for cutting cost to orbit through reusability is enormous.

    4. Re:The break down of 60 million is the key. by anon+mouse-cow-aard · · Score: 1

      It is a launch cost, not a total cost. It makes no sense to estimate the cost of the rocket to be divided equally among the two stages. SpaceX doesnt build the payloads, it isnt their cost. The payload is almost certainly not included in the 60M$ launch costs cited. So The main cost of the stages is the engines. there are nine in the first stage, and only one in the second. I imagine the breakdown in costs is proportional to that, rather than the 50:50 breakdown proposed above. The motor is a little different, being optimized for lower atmospheric pressure, but thats just a difference not an added cost, the only added complication in the second stage is the carbon fibre fairing... everything thing else is payload. so I expect that even if we say only 40 M$ is the vehicle itself, then probably 36 M$ or thereabouts is the first stage. So yeah... 10:1 on the vehicle... results in going from 60 M$/launch to 24 M$/launch... or 2/3rds cheaper.

    5. Re:The break down of 60 million is the key. by ravenshrike · · Score: 2

      No, they were completely overhauled each time with a large amount of parts replaced. Pretending it was some sort of cost effective refurbishment a la SpaceX is laughable.

    6. Re:The break down of 60 million is the key. by Sir+Holo · · Score: 1

      The cost is in the rocket motor, the nozzle that holds the combustion products in plasma state, its cooling mechanism, pumps and controls. I am not sure how much of it can be inspected and re validated without extensive disassembly.

      I keep waiting for them to replace the nozzle with an experimental version that uses a linear aerospike. The April 10, 2001 patent will be expiring in just about 5 1/2 years now...

      Aerospike? What about the Marlinspike? I hear it's got real Moxie.

  9. Don't confuse SpaceX and Blue Origin. by Futurepower(R) · · Score: 3, Insightful

    A quote from an NBC News story about Blue Origin, a company founded by Amazon CEO Jeff Bezos, shows one of the differences between SpaceX rockets, which go into orbit, and Blue Origin rockets, which don't orbit:

    SpaceX is working to reuse rockets that are returning from the higher altitudes and faster speeds of orbital missions. "It is ... important to clear up the difference between 'space' and 'orbit'," Musk posted on Twitter. ... A rocket needs to be traveling about three times the speed of sound, or Mach 3, to reach space, but orbital missions require speeds about Mach 30, Musk said.

    1. Re:Don't confuse SpaceX and Blue Origin. by goodmanj · · Score: 3, Insightful

      Absolutely. The scale gap between suborbital and orbital rockets is so huge, Blue Origin and Virgin Galactic might as well be building hot-air balloons.

    2. Re: Don't confuse SpaceX and Blue Origin. by jrvz · · Score: 1

      The energy required to lift a spacecraft to 100 km altitude is about hg=100 km*10 m/ s^2=10^6 J/kg. for orbital velocity you need an additional 1/2 (7 km/s)^2 = 26*10^6 J/kg. So maybe the SpaceX problem was 27 times harder. Except we should be multiplying by the mass of the payload. What was the payload for the Blue Origin demo flight?

  10. Re:My estimate by TWX · · Score: 1

    You are all cows. Cows say mooo. Mooo! Moooo! Mooo cows mooo! Moooo say the cows. YOU ESTIMATED COWS!!!

    Is that like the engineering joke with the punchline, "it works, but only for spherical cows in a vacuum"?

    --
    Do not look into laser with remaining eye.
  11. Should slow down by Anonymous Coward · · Score: 0

    Not go so fast. What's the rush? Take it easy. Come on baby!

  12. Re: My estimate by Anonymous Coward · · Score: 0

    Merry moomas to meeeeeeeee!

  13. economic case with different assumptions... by XXongo · · Score: 5, Interesting
    Suppose:

    1) The first stage is 2/3 the total cost to launch. Which would be $40 million.
    2) They can renovate the first stage for $5 million.
    3) They can get five launches from a first stage (original plus four more).
    So, $60 million for five launches, plus the $20 million for the second stage x5.

    Which comes to $32 million per launch. A bit more than half the current price.

    Now, I consider those pessimistic assumptions.

    Interesting numbers. Let's try a variant case. Suppose in addition:
    You're assuming that the non-reusable launch vehicle cost per launch is $60M. OK, let's start out by assuming 1/3 of that is fixed costs and operations costs, and 2/3 the vehicle cost, which is split evenly between the two stages (first stage is larger, but not proportionately more expensive). So, of the $60 million, $40 million is spent even if the vehicle first stage was free.
    Now assume that re-usability increases the launch cost by, say, $5 million (launch operations are expensive! and the cost is not entirely the vehicle).
    Assume that all the stuff needed to make the first stage reusable increases the stage cost by 25%, from $20M to $25M.
    And assume that the delta-V and the added mass to do the fly-back decreases payload by 10%, and that the price you sell the launch for decreases a similar percentage (some payloads won't care, but some will.)

    economics are much less clear now. The first stage cost drops with refurbishment from $20M to $6M, but the total launch cost only drops from $60M to $51M, whereas the price you can sell the launch for drops from $60M to $54M.

    Still an economic advantage... but only a few percent advantage.

    1. Re:economic case with different assumptions... by dlapine · · Score: 4, Insightful

      Interesting numbers. Let's try a variant case. Suppose in addition: You're assuming that the non-reusable launch vehicle cost per launch is $60M. OK, let's start out by assuming 1/3 of that is fixed costs and operations costs, and 2/3 the vehicle cost, which is split evenly between the two stages (first stage is larger, but not proportionately more expensive). So, of the $60 million, $40 million is spent even if the vehicle first stage was free. Now assume that re-usability increases the launch cost by, say, $5 million (launch operations are expensive! and the cost is not entirely the vehicle). Assume that all the stuff needed to make the first stage reusable increases the stage cost by 25%, from $20M to $25M. And assume that the delta-V and the added mass to do the fly-back decreases payload by 10%, and that the price you sell the launch for decreases a similar percentage (some payloads won't care, but some will.)

      First off, the current cost of the rocket already includes the costs to do reusibilty, so the cost of the first stage will not increase- it is designed be reused up to 10 times right now with no change in hardware.

      Secondly, the cost of the 2 stages are not even remotely close to equal; the first stage has 9 Merlin engines, the second stage only has 1. An estimate of 6 to 1 (first to second) for costs would be more reasonable.

      Thirdly, the payloads currently quoted already include reusability (16MT to LEO and 4.5MT to GTO). No loss of earnings there.

      So none your variant assumptions are useful for this discussion.

      Let's look at some other factors you haven't considered.

      Like the space shuttle, SpaceX now has a rocket for examination that has flown a full mission and hasn't had a 6G salt water landing. This means that they will be able to do full engineering analysis on what stresses the rocket actually experienced during a flight event that increase all steps necessary for re-use. The results of that analysis will allow them to determine what parts of the rocket need to be enhanced or reduced to meet the 10 tens re-use goal. SpaceX has the luxury of being to make changes to their rocket without Congressional approval, so this information can be used immediately to improve the vehicle. The design goal of the Falcon is that the rocket need not be "refurbished" after every flight, just put through some standard flight maintenance tests. Having the flown stages available for analysis will help them to meet this goal.

      Additionally, SpaceX currently has launch costs based on 6 launches a year. As they have already demonstrated the ability to launch with a cadence of 2 weeks several times, being able to increase their launch rate to a minimum of 1 a month will cut their overall costs per launch.

      Let's assume that a slight redesign based on analysis of real-world data let's them increase reliability of the Falcon 9 to 1 in 100 and increase the payload by 1MT to GTO. At 5.5MT to GTO, this let's them handle 90% of all GTO launches (6MT is at the current top end for commercial satellites to GeoSynchronous orbits) with the reuable design. 5MT is compable to $137M Ariane 5 capbility or $132M for an Atlas 5 launch for NASA with both the throw weight and reliability requirements necessary to get these flights.

      $60M to launch the current, reusable Falcon 9 1.1FT.
      33% is launch cost. - $20M
      56% is first stage - $34M
      11% is the second stage $6M

      Assumption 1: increase in flight rate reduces launch costs by 25%
      Assumption 2: landing/recovery/flight readiness check costs $5M a launch
      Assumption 3: 10 flights reuse of the first stage = $3.5M a launch

      Under these assumptions:
      Launch cost $15M
      Landing/recovery/checks $5M
      First stage $3.5M
      Second Stage: $6M

      Total: $29.5M

      I'm OK with those numbers given what they can charge and how quickly they can do regular launches. Where they will really rake in the cash is for a Facon Heavy launch (same vehicle with 3 first stages instead of 1) with 56MT to LEO for an asking price of $110M and a cost, by these assumptions of $35M. They could even reduce their price after a few launches of the Heavy to $56M, and start launching bulk cargo to space at a rate of $1000/Kg

      --
      The Internet has no garbage collection
    2. Re:economic case with different assumptions... by XXongo · · Score: 1
      You are stating assumptions that are plausible... but you don't actually know any of those things. You are making figures up, based on some very non-technical press-release figures. What you are making up is plausible. But it is still guesswork.

      As with most things, the devil is in the details... and you don't have the details.

      You are right, however, that with different (but also plausible) assumptions, you can come up with very different results.

    3. Re:economic case with different assumptions... by dlapine · · Score: 2

      Actually, I do know these things, but didn't bother to include all the sources, given it being Christmas and all. Since you are so insistent about it though...

      Points 1 & 3 are taken from direct quotes by Elon Musk
      Point 2 is taken from the design of the Falcon 9, available at spacex or nearby wikipedia.
      "re-use without refurbishment" another direct E. Musk quote.

      Spacex current launch rate (6 per year) and cadence and published launch costs and satellite weights for commercial space companies are just a google search away. Try this excellent site: http://www.spacelaunchreport.c... for starters

      A very informative and useful place to find much of this information and discussion by knowledgeable space experts and enthusiasts is at: http://www.nasaspaceflight.com...

      The rest is just simple math.

      To sum up, I do have details, I'm not guessing, and I note where I make assumptions. Find fault with my assumptions if you like, but please explain why those assumptions are flawed with specifics, not generalities.

      --
      The Internet has no garbage collection
    4. Re:economic case with different assumptions... by Anonymous Coward · · Score: 0

      "re-use without refurbishment" another direct E. Musk quote.

      Spacex current launch rate (6 per year) and cadence and published launch costs and satellite weights for commercial space companies are just a google search away. Try this excellent site: http://www.spacelaunchreport.c... for starters

      The Merline engines, surely the most expensive components in the launcher, can be re-used up to 40 times. Or so claims SpaceX.

      What isn't known is how well the rest of the launcher will hold up. Structural integrity, metallurgy, there are likely a few pitfalls.

      The re-use may take other forms in practice. Let's say they can use the engines in 30 launches but the launcher body and other subsystems make it practical to launch the rocket body 5 times.

      So you'd have sets of Merlin engines (in groups of nine) that are first-gen (0 flights, suitable for human cargo), second-gen (1-5 flights), third-gen (6-10), etc.

      And the bodies of the Falcon rockets might be similarly aged.

      SpaceX was producing 5 Merlin engines every 2 weeks earlier this year. That is enough for a dozen Falcon-9's per year. They have plans to ramp up to almost 400 engines, enough for 40 new rockets, per year. It has been their business plan all along.

      Musk is trying to build the Model T of space. He's building up a production facility to match the demand. Not the biggest or the fanciest launcher but something that drastically reduces the cost of going to space with payloads with the intent of capturing 60%-70% of launches around the world. This is how commercialization of space will have to happen unless we are willing to pay ridiculously high launch costs forever.

      You have to admire his vision. He's not just a rich dude with even richer (Google) backers. He is a man with a Vision, who wants to do Big Things.

    5. Re:economic case with different assumptions... by Anonymous Coward · · Score: 0

      You have to admire his vision. He's not just a rich dude with even richer (Google) backers. He is a man with a Vision, who wants to do Big Things.

      It's not just his vision; it's his ability to execute. The dude is raising 5 boys, actively running 2 companies and chairing a 3rd, while traipsing around the world giving talks. There's probably less than a hundred people in the world who are even capable of that and so far, exactly ONE who's managing to do it.

    6. Re:economic case with different assumptions... by solartear · · Score: 1

      The boost stage is roughly 70% of the cost of a launch. So, if we're able to reuse it and refly it with minimal work between flights, and customers are comfortable with that - and it might take a few years for customers to get comfortable with that - then obviously there's as much as - ultimately - a 70% reduction from where things are today. - Elon Musk

      http://shitelonsays.com/transcript/spacex-press-conference-at-the-national-press-club-2014-04-25

      So even with launch and other non-stage-specific costs factored in, the first to second stage cost ratio is no where near 6-1.

  14. What a relief! by Anonymous Coward · · Score: 0

    Well, that's settled then. Somebody tell Elon that it's been decided.

  15. Not really by Maury+Markowitz · · Score: 4, Interesting

    "This kind of refurbishing is why the Space Shuttle ended up being way more expensive than expected"

    It was fully expected to be that expensive, the upper management simply ignored it.

    At one point when they were still considering fully reusable designs, the Phase II' candidates, management put the cost of the system at something like $100 per pound to orbit. However, they had already estimated the staffing at the Cape to be on the order of 25,000 people, which meant the payroll alone was about $500 a pound. Most estimates put the absolute lowest cost at $1000/pound. After Challenger it was over $2500, making it the most expensive launch system in US history.

    So why was management saying $100 until the end? Because the entire justification for the Shuttle was that it would be lower cost than any other system. And because of that, everyone would move their cargos to it. And since everyone moved their cargos to it, it would be launching all the time. And because it was launching all the time, the embedded payroll per launch was lower. Even then it didn't look like it could match Scout, so they came up with the Getaway Specials to try to take those, and then cancelled Scout.

    Now it was clear to everyone, including the very detailed CBO report, that if they didn't get every single payload out there, then there was no way to get the launch rates they needed to make the payroll costs go down. And as the CBO report noted, if any of those assumptions failed, it would end up being more expensive than systems like Titan. And they went on to point out that many of the payloads NASA assumed would move to the Shuttle never even existed in the first place (modular telcomsats for instance, which they just made up).

    So management lied, fully aware there was no way they could meet the numbers. And it was this precise attitude that caused the Challenger Disaster, where bad news numbers were simply ignored and replaced with ones that met political or economic criterion.

  16. Then what was the point, Elon? by Anonymous Coward · · Score: 0

    At some time, all the protons in the universe will have decayed.

  17. Heavy Lift version even more so by Anonymous Coward · · Score: 0

    The Heavy Lift version uses 3 Falcon 9 rockets so consider the savings on that bad boy compared to the competition. Something to keep our eyes and ears on for sure. Way to go Mr Musk.

  18. How I see it by Anonymous Coward · · Score: 1

    First some background. The engineers behind modern rockets have throughout the years gotten pretty good at designing rockets that can launch successfully. Unfortunately, we haven't been able to evaluate a launched rocket to see how the predictions of the stresses have effected the rockets. This is the first orbital booster that has been successfully re-landed.

    What SpaceX is likely to do is take one of these returned boosters, strip it down, and evaluate how the stresses from launch/return have effected the rocket body and motors. They'll then determine which parts are over/under engineered. They then make some design changes to ensure that every part of the first stage can be reused with minimal or no refurbishment. This is what they are aiming for aircraft like re-use (pre-flight inspection and periodic maintenance/rebuilds). Move the first stage to the VAB, add the second stage/payload, roll out to the pad, re-fuel, and launch.

    As the re-usability of the boosters increases, the operational overhead of launches will come down. Right now they have to pay for a large team to handle rocket prep and launch control even though there are fairly infrequent launches. So these people likely have a fair amount of time where they are not performing at peak efficiency from a ROI perspective. This will improve when the greater number of launches keeps them fully utilized.

    If you assume that based on testing the booster can be reused 12 times before retirement/major rebuild (yet to be proven) with an initial manufacture, transport (across country), fuel, launch cost of $60M and $300k transport (short distance), fuel, launch cost. I'm ignoring staging assembly at the VAB and launch operation control costs here (would vary by mission/payload). You get an average of $5.275M/launch. Average costs can be driven down further if a rebuild/refurbishment can extend the number of launches. i.e. $10M rebuild after 12 launches and then it can then do another 12 for $300k per gives an avg of $3.2M per launch. This can of course vary in that if a launch customer insists on a first/early use booster they may pay more for it front-loading the costs and reducing the costs of later launches.

    So, if SpaceX attempts to aggressively drive down launch costs then the cost of the first stage could be cut eventually by a avg. factor of ~20x. Or SpaceX can itself use recovered boosters at cost to launch orbital refueling stations, components for it's mars ambitions, etc, paving the way for deep space missions.

  19. Too many satellites in orbit? by Anonymous Coward · · Score: 0

    Isn't it possible for space to be TOO accessible? If it becomes too cheap to put a satellite into orbit, and every Joe Blow with a million dollars can do it, doesn't that make it more likely that space will become overcrowded, causing hypervelocity satellite collisions increase in frequency, bringing us ever closer to ua Kessler Syndrome scenario?

    Space will need to be regulated more than it currently is in order to keep that from happening.

    1. Re: Too many satellites in orbit? by Anonymous Coward · · Score: 0

      Nah. If it's too cheap, we'll build a ring around the equator and have geosynchronous satellites at LEO altitudes.

      They'll simply latch on, find a power socket and be billed for net power usage.

    2. Re:Too many satellites in orbit? by Anonymous Coward · · Score: 0

      SpaceX and the satellites they launch are already regulated by US government regulations and treaty requirements. I believe one of those requirements is that they minimize the creation of space debris including those from the launch vehicle and the satellite either via deorbiting at the end of its use or transfer to a graveyard orbit. Cheaper access to space may also encourage cleanup efforts, one of the major limitations to those efforts are the cost of space access. With lower costs governments/satellite companies may begin launching cleanup craft to remove the debris already in orbit. If those cleanup satellites are small enough it may be possible to simply piggyback them on the spare payload capacity of other space launches.

  20. Instant relaunch times! by Anonymous Coward · · Score: 0

    No, not because fast repairs. Simply have 10 rockets, and if repairs take 9 days, you will always have 1 ready to launch each day. Or produce as many as days it takes.

  21. The environmental cost of low-cost satellites by Anonymous Coward · · Score: 0

    Whast about the cost of putting too mnay satellites in orbit? Dont' we also hear about how much junk is floating around in space too? If the cost goes much lower lowering the barrier of entry for satellites, won't we end up having an orbiting ring of junk around the planet?

  22. The cost is per pound to orbit. by Anonymous Coward · · Score: 0

    I'd bet half next year, tapering to 1/10 in the next year or two.

    There are two things going on here. The cost, and making space no-big-deal.

    Must have the normal launch crowd interested/concerned/looking at time to retirement.

    SpaceX did seem to loose composure in the middle of the delivery mission when the booster landed.
    This is understandable and no harm done, but they need to stay focused then party.
    Another time it may matter.

    1. Re:The cost is per pound to orbit. by Anonymous Coward · · Score: 0

      "Another time it may matter."

      I found the "party atmosphere" in/near the control room somewhat annoying but after the rocket had left the ground I don't know how it could affect the outcome of the mission in 99% of emergency cases. I don't know if there has been a single case in the history of the rocket launch industry where a quick decision from ground controllers was the determining factor in correcting an error during earth to orbit launch. Even in the case of an engine failure the craft automatically recalculates the necessary changes to the flight profile.

    2. Re:The cost is per pound to orbit. by eric_t_duckman · · Score: 1

      I'd hope the person with their finger near the "destruct" button stays focused on their job, because an out of control rocket could hurt somebody on the ground.

  23. Refurb Cost Less Than Build Cost ? by Anonymous Coward · · Score: 0

    Refurbing the first stage will need to he much much less, and doable many times to save on the build cost.

    If refurbing takes the same people as the build and if the reusable number is not much greater than 2, then the "savings" margin will be very small. Also, if a refurbed stage 1 fails on the second flight, also causing the loss of the pay-load, then the reland-ability becomes an expensive option greater than "build to throw away"!

    It may all come down to "inventive" accounting.

    I.E. SpaceX will have to "Inventively" account so that SpaceX and Musk technically owes no taxes to the IRS. This is the option that Al Capone enjoyed in Chicago in the 1920s.

    Ha ha

  24. Problem of production by downix · · Score: 1

    The big reason why Falcon costs only $60 million is due to the production volume. Reuse slashes production volumes, which means the cost to produce will soar. 10 launches of disposable Falcon rockets means 100 engines built, while 10 launches of a reused Falcon will only result in 19 engines built. Cutting production volume means higher costs, so it is not a slam dunk for SpaceX.

    --
    Karma Whoring for Fun and Profit.
    1. Re:Problem of production by Anonymous Coward · · Score: 0

      Nope, PROVIDED the risk pays off they are likely to be handling maybe 90% of payloads. Almost everything but non-US 'sensitive stuff'.

      And if they drop costs, there's more will be launched. It's like the early days of the automotive industry, Henry Ford changed the game with serious production capacity and increased volume. That's why the gamble is worth it, there's a BIG multiplier if it comes off.

      Pete
       

    2. Re:Problem of production by Anonymous Coward · · Score: 0

      Le sigh.. You're basing that conjecture on that a company that could (potentially) do launches a lot cheaper and just as reliable as their competitors would only ever get to do 10 launches.. *ERROR* *ERROR* Does not compute.

      If you _really_ want to find a challenge for them, it would probably be, as the new data comes in and they hone their design, to keep enough commonality to keep the benefits of scale.

  25. Fact check by VikingNation · · Score: 0

    There is a lot being made about SpaceX re-using the rocket for future launches. Hasn't NASA been re-using solid rocket booster for decades?

  26. I imagine... by Anonymous Coward · · Score: 0

    ...that all SpaceX flights with people will use First-Time boosters and they will be refurbished for unattended missions. At least I hope so.

    1. Re:I imagine... by rpstrong · · Score: 1

      I would hope not. Would you sooner take off in a brand new Cessna, fresh off the factory floor, or in one that had actually been flight tested? Do you want to beta test a new booster?

      [Kind of reminds reminds me that while the early bird gets the worm, it is the second mouse that gets the cheese.]

  27. Just return third stage to earth by Anonymous Coward · · Score: 0

    Perhaps in the future, they can make the third stage returnable, so that if the 1st stage blows, the payload is saved.

  28. He had a vid up that shows recovery of all stages. by Anonymous Coward · · Score: 0

    He had a vid up that shows recovery of all stages.

  29. Space X,put,your money where your mouth is.. by Anonymous Coward · · Score: 0

    Space X last I heard had 8 billion dollars worth of launches on their manifest. Companies do their due diligence and consider Space X reliable and competent.they clearly do not read the drivel on this slash dot about the reliability or competency of Space X from the armchair loons writing with zero knowledge of this company. Looking at the inventiveness of their engineers and the minor reasons for their launch failures which have always been fully understood within days of the engineering error and resolved on essentially newly designed and engineered rocket motors and on the total assembly they are hugely ahead of the curve. Their use of extremely r dundant systems are of the highest quality. I have watched rocket development for 60 years and personally attended launches from the 1950s onward and I can assert that the engineering inventiveness even to the means they use to structure the rocket on the launch stand put them ten years ahead of any other company. Next year they will begin testing the largest launch vehicle ever assembled. This is no mean feat. You naysayers do not understand what you are of seeing as Space X will go down in history as an original the way Northrop was in the aircraft world...they are an original and they will make a lot of money to carry the ideals on Mr.Musk to his publicly stated goal..Mars. He is not kidding.

  30. Going forward by billdale · · Score: 0

    Just as the reusable booster is a strategy to reduce costs, they will he looking at other cost-savers. The Dragon launch system is the largest ever built, plus by using super-cooled, denser fuel, they can put more hardware in orbit than anyone could before them. One strategy they may employ would be, as they could have done on this last momentous launch, was to have put a full 12 satellites in orbit rather than just 11 plus one dead weight for balance. When the first of those satellites does go haywire, that 12th satellite could be taken out of hibernation to fill the slot of that first dead satellite. And, going forward, using all excess launch potential to put "spares" in orbit that hibernate until needed.