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World's Most Powerful Rocket Ready In 2012, SpaceX Says

Velcroman1 writes "Elon Musk, the millionaire founder of private space company Space Exploration Technologies Corp (SpaceX for short) said the long-planned Falcon Heavy vehicle would be ready for lift off at the end of 2012. The rocket, which he called the most powerful in the world, would be capable of taking men to the International Space Station, dropping vehicles and astronauts on the moon — and maybe even cruising to Mars and back."

43 of 251 comments (clear)

  1. Leave it Fox.. by Necron69 · · Score: 2, Interesting

    What an amazingly inaccurate summary. The rocket will be left to fall back into the ocean/atmosphere, while it has enough cargo capacity (2X that of the space shuttle to LEO) to launch something that could, conceivably, go to Mars and back.

    Personally, I'm expecting Bigelow to be the first customer.

    Necron69

    1. Re:Leave it Fox.. by usul294 · · Score: 4, Informative

      I don't see how it's Fox's fault, all TFA said was that Elon Musk said the craft could be used to complete the Mars mission. Summary was way off from reality, but the article seemed to be done without hyperbole or bias.

    2. Re:Leave it Fox.. by 517714 · · Score: 3, Funny
      Title: "World's Most Powerful Rocket Ready in 2012, SpaceX Says"

      Last Sentence: ""First launch from our Cape Canaveral launch complex is planned for late 2013 or 2014,” Musk said."

      Apparently their reporters have a very short attention span.

      --
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    3. Re:Leave it Fox.. by ravenspear · · Score: 3, Informative

      That is the first launch from Canaveral.

      The first launch will be from Vandenburg, which he stated would likely be in early 2013.

    4. Re:Leave it Fox.. by Wyatt+Earp · · Score: 3, Informative

      Apparently you didn't read the article.

      The rocket will be ready by late 2012 from Vandenberg (which is California), Canaveral (which is Florida) launches by late 2013.

    5. Re:Leave it Fox.. by RM6f9 · · Score: 2

      Rocket may be ready well in advance of available launch schedule dates/permits/etc..., - ?

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    6. Re:Leave it Fox.. by ravenspear · · Score: 4, Informative

      He stated that the rocket will be ready i.e. ready to launch by the end of 2012.

      But the actual launch would probably be in 2013 depending on final regulatory hurdles plus any final technical issues encountered with the pad integration.

    7. Re:Leave it Fox.. by DrJimbo · · Score: 3, Funny

      Always better to have the rocket ready *before* the first launch rather than after.

      --
      We don't see the world as it is, we see it as we are.
      -- Anais Nin
  2. "maybe" cruising to mars? by tulcod · · Score: 5, Funny

    How can one not know whether his/her rocket is capable of making it to Mars? Are we talking superpositions here or what?

    1. Re:"maybe" cruising to mars? by ByOhTek · · Score: 5, Funny

      Maybe part of his team is using metric, and another part is using imperial?

      --
      Self proclaimed typo king, and inventor of the bear destroying coffee table (patent not pending).
    2. Re:"maybe" cruising to mars? by osu-neko · · Score: 3, Insightful

      How can one not know whether his/her rocket is capable of making it to Mars? Are we talking superpositions here or what?

      No, we're talking about reality. In reality, unlike in theory, it takes a lot more to get a rocket to Mars than engineering and sufficient power and fuel. It takes massive funding, political will, and the sustained support of both for several years. There's no engineering equation you can use to calculate if you'll make it to Mars -- the equation will only tell you whether you can do the easy part...

      --
      "Convictions are more dangerous enemies of truth than lies."
    3. Re:"maybe" cruising to mars? by Nyeerrmm · · Score: 4, Insightful

      Because it depends on the engineering of what goes on top of it. The Falcon Heavy wouldn't actually go to Mars, it just has the heft to potentially launch a vehicle that could go there and back again in one shot.

      However, since no such vehicles exist or are far enough along in planning to have really believable numbers for mass and capabilities, its hard to say for sure.

      Add in that uncertainties in practical engineering for the launch vehicles certainly exist and its a very reasonable statement.

    4. Re:"maybe" cruising to mars? by FleaPlus · · Score: 4, Interesting

      No, we're talking about reality. In reality, unlike in theory, it takes a lot more to get a rocket to Mars than engineering and sufficient power and fuel. It takes massive funding, political will, and the sustained support of both for several years. There's no engineering equation you can use to calculate if you'll make it to Mars -- the equation will only tell you whether you can do the easy part...

      Actually, SpaceX's first demo launch of the Falcon Heavy in 2013 doesn't have a customer and they're self-funding it, so if they want to they can send it to pretty much anywhere in the inner solar system that they want. Heck, Elon Musk could even get part of his team to assemble his old Mars Oasis greenhouse project and try to land it on Mars if he wanted. Since it's self-funded, it's purely an engineering problem (perhaps with some PR thrown in for good measure).

    5. Re:"maybe" cruising to mars? by GooberToo · · Score: 2

      No, we're talking about reality. In reality, unlike in theory,

      Right there you just lost many a slashdot reader. I'll say no more else their heads may explode.

    6. Re:"maybe" cruising to mars? by killkillkill · · Score: 5, Funny

      To be fair, that error actually got NASA closer to Mars.

    7. Re:"maybe" cruising to mars? by FleaPlus · · Score: 2

      > Oh yes, if he can fund a test launch, he can surely fund a trip to mars to set up a greenhouse. That makes total sense.

      If he wants to, pretty much, yeah. The work SpaceX has already been doing with heat shields, solar power, and propulsive landing potentially makes it even more feasible now than it was back when Musk would have had to start from scratch. The biggest barrier he faced back in 2001 was the cost of launch. Here's a more recent (2009) recollection of Musk's about the Mars Oasis project:

      http://spectrum.ieee.org/aerospace/space-flight/risky-business/0

      At first, I thought I'd use some of my PayPal money to popularize the idea of life on Mars. I settled on a mission called Mars Oasis, which would land a small robotic greenhouse that would establish life on another planet and show great images of green plants on a red background. It would get the public excited, and we'd learn a lot about what it takes to sustain plant life on the surface of Mars.
      I quickly found that the biggest obstacle was the cost of the launch. A U.S. Delta II rocket would cost $60 million, while a refurbished Russian intercontinental ballistic missile would cost $10 million -- without the necessary third stage.
      I gathered a group of engineers from the space industry to find a way to get the launch cost down. We determined that we could do it by optimizing the design for cost and by making the rocket reusable. Of course, we also had to ensure that it performed at least as well as other available rockets. I dropped the greenhouse idea; my goal now was to make it technically and financially possible to extend life to Mars. In 2002 I founded Space Exploration Technologies.

  3. But smaller then the Saturn V from the 1960s by LWATCDR · · Score: 5, Interesting

    Call me when we have something that can out lift the Saturn V. Yes I know they say this will cheaper but still I expected us to be much farther along than we are.

    --
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    1. Re:But smaller then the Saturn V from the 1960s by avgjoe62 · · Score: 3, Insightful

      I'm glad someone else noticed this. The Saturn V had a payload capacity of 260,000 pounds and peak thrust of at least 7,500,000 pounds. They may be saying that this is the biggest thrust and payload among operational rockets, but I'd still like to see the ratio of (thrust/payload)/cost. That is where I'd really like to see improvement.

      --

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    2. Re:But smaller then the Saturn V from the 1960s by ceoyoyo · · Score: 2

      Why? We're much better at orbital assembly now so we don't need the giant, all-the-eggs-in-one-basket rocket anymore. Cheap is MUCH more impressive.

    3. Re:But smaller then the Saturn V from the 1960s by digitalnoise615 · · Score: 2, Informative

      I'm glad someone else noticed this. The Saturn V had a payload capacity of 260,000 pounds and peak thrust of at least 7,500,000 pounds. They may be saying that this is the biggest thrust and payload among operational rockets, but I'd still like to see the ratio of (thrust/payload)/cost. That is where I'd really like to see improvement.

      Estimated to be around $1,000/ton to orbit. Nothing comes close at this point to that figure, and it's all down-hill from there once it's reached. The Saturn V was/is a beautiful machine - but it was rather inefficient.

    4. Re:But smaller then the Saturn V from the 1960s by ravenspear · · Score: 4, Informative

      $1000/lb not $1000/ton.

      But yes this is MUCH cheaper than the Saturn V, Shuttle, or anything else really.

    5. Re:But smaller then the Saturn V from the 1960s by sandytaru · · Score: 2

      "Musk also claimed the Falcon Heavy would cost a third per flight than the Delta IV rocket, and sets a new world record for the cost per pound to orbit of around about a thousand dollars." Not an apples to apples comparison, but if he's claiming a new record, then it is pretty impressive. Any direct comparisons to the Saturn V would also need to take into account inflation, as the 1965 dollar was about six times as valuable as today's dollar. Ah, Wiki says: " In 1969, the cost of a Saturn V including launch was US $ 185 million (inflation adjusted US$ 1.11 billion in 2011)." Yikes.

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    6. Re:But smaller then the Saturn V from the 1960s by khallow · · Score: 3, Insightful

      Call me when we have something that can out lift the Saturn V. Yes I know they say this will cheaper but still I expected us to be much farther along than we are.

      Why? The Space Shuttle sucked the oxygen out of the room for large rocket development and Griffin, the previous NASA administrator, followed up with an incompetent, underfunded attempt. As I see it, 53 metric tons to LEO at SpaceX prices is a far better deal than making some ludicrously expensive Saturn V class rocket.

      Keep in mind also that SpaceX's designs scale quite nicely to Saturn V class level. I'd rather give them the chance to prove themselves with smaller rockets first than get pouty because SpaceX doesn't meet somebody's overblown expectations.

    7. Re:But smaller then the Saturn V from the 1960s by Confusador · · Score: 3, Informative

      And then they promptly refused to fund it.

    8. Re:But smaller then the Saturn V from the 1960s by mdielmann · · Score: 3, Insightful

      Even Amazon does, nowadays. What do you think a virtual server is?

      --
      Sure I'm paranoid, but am I paranoid enough?
    9. Re:But smaller then the Saturn V from the 1960s by edremy · · Score: 3, Informative
      You're making the mistake of assuming that all high tech equipment improves at the same rate as microprocessors.

      The basic physics of rocket engines hasn't changed much at all, and can't given the limitations of the chemical fuels they use.

      • The F-1 engine on the first stage of the Saturn 5 had a specific impulse of 263 seconds, burning kerosene and LOX
      • The Merlin 1C engine on the first stage of the Falcon 9 has a specific impulse of 304 seconds, burning kerosene and LOX
      • The Space Shuttle main engine? 363 seconds, but it uses hydrogen and LOX

      That's not a lot of improvement in 40 years. Sure, there are some materials improvements and better, lighter avionics, but that doesn't buy you the massive improvement you see in other high tech areas

      --
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    10. Re:But smaller then the Saturn V from the 1960s by LWATCDR · · Score: 3, Interesting

      The Saturn V was produced in small numbers and using 1960s cost was no option development. Using modern production methods the cost should be much lower if they produced it today. Frankly the only parts I would keep from the old Saturn program would be the F-1A which they never flew and the J-2 which we just developed new versions of. Use LiAL for the tanks and user modern electronics and it could cost a lot less.
      The Falcon 9 Heavy is really cool. It is the hype that is rubbing me the wrong way.

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    11. Re:But smaller then the Saturn V from the 1960s by TheEyes · · Score: 2

      Choose your shipping method:

      [ ] Ground
      [ ] Air
      [X] Semiballistic

      When you need it halfway around the world in less than an hour, choose SpaceX Freight!

    12. Re:But smaller then the Saturn V from the 1960s by FleaPlus · · Score: 2

      It'd be interesting to hear the number of launches they need to make a profit at that price. I'm assuming the price is based on an average price, which in turn is calculated by assuming the fixed costs of development can be spread over some minimum number of launches.

      If the number of paying launches were, say, *1*, I doubt very much they'd be able to make money at that price.

      If I recall correctly, the break-even number stated during the press conference was 4 Falcon Heavies (and presumably 4 Falcon 9's) a year. The capacity they're presently aiming for is 10 FH's and 10 F9's.

      I assume this also doesn't include SpaceX's quest to reuse the first stages and accompanying engines. Since the side-mounted stages actually separate earlier, reuse will hopefully be easier to accomplish with the FH than the F9.

  4. His designs are in NASA archives at Marshall SFC by alispguru · · Score: 4, Informative

    Urban legends aside, NASA did not throw the plans for the Saturn V away.

    Falcon Heavy is cool, but it's still a factor of two away from the LEO capacity of a Saturn V.

    --

    To a Lisp hacker, XML is S-expressions in drag.
  5. Details from press conference by FleaPlus · · Score: 4, Informative

    The Fox article is a little sparse on info, so for the curious, there was some pretty good liveblogging (live-foruming?) of the press conference here. You can see official details (and a neat video) on SpaceX's site here.

    Looking through the forum and the website, here's a summary of all the most interesting stuff:

    • Falcon 9 (F9) able to lift much more than estimated with engine upgrades, Falcon Heavy (FH) estimates upgraded
    • FH: 3 nine-engine cores attached to each other
      paying development costs internally, strong commercial + gov customer interest
    • FH will arrive at Vandenberg pad in 2012, launch in early 2013
    • testing upgraded engines now at McGregor facility
    • estimating 117K lbs (53mt) to orbit for FH, possibly >120K lbs
    • double payload of Shuttle and Delta IV Heavy
    • launching from Vandenberg and Cape Canaveral
    • once in full operation expecting ~10 F9 flights a year, ~10 FH flights a year
    • increasing rate of engine production to 400 each year (currently 50/year)
    • FH price sets new world record at $1000/lb
    • first rocket in history to feature propellant crossfeed, allowing for earlier separation of emptied side boosters (== much more efficiency)
    • multi-engine-out capability for more reliability
    • meets published NASA human rating standards, not sure yet about "unpublished" standards
    • lower cost than current EELVs could save DOD alone $1.7B-$2.2B each year
    • could do Mars sample return mission in a single flight
    • payload to Mars 1/4 LEO payload, so 30K lbs to Mars
    • could go to Moon or NEO with only 2 launches
    • could do lunar flyby with a single launch of Dragon capsule
    • in response to Q&A, mentioned follow-up design capable of >150mt (Saturn V was 119mt)

    As an aside, it'll be quite fascinating to see what impact this has on the heavy-lift debate currently going on in Congress. For those unfamiliar with it, Congress is currently trying to pressure NASA to spend several billion dollars of its funding over several years into building a 70mt rocket from shuttle-legacy components/infrastructure. It's now looking like SpaceX will build a rocket with nearly the same capability using its own funding, which will be ready to launch several years before the Congress-mandated rocket. Hmm.

    1. Re:Details from press conference by harperska · · Score: 5, Insightful

      Unpublished Standard #1: Components must be built by companies that contribute to politicians on the committee to decide the standards.

      Unpublished Standard #1: Components must be built by ATK.

      Congress doesn't really care about 'shuttle derived technologies' and costs are a straw man. But ATK in particular, who makes the shuttle SRBs, holds some pretty strong sway over certain congress-critters. That's why the Ares 1 first stage was just a scaled up shuttle SRB even though SRBs are a pretty dumb idea for a human-carrying rocket and completely idiotic as the sole first stage, as they can't be effectively throttled or shut off after being lit.

  6. Re:His designs are in NASA archives at Marshall SF by ravenspear · · Score: 2

    It actually makes it somewhat easier to get to the moon though, since 2 launches of the Falcon Heavy (what you need to get enough mass for a moon landing) are going to be cheaper than one Saturn V.

    You could launch the capsule with one launch and the EDS/lander with a second one, then rendezvous in orbit.

  7. A game changer, if they can get it to work. by khallow · · Score: 3, Informative

    This is about half a Saturn V class rocket in terms of payload. Development costs are likely to be remarkably low, around a few billion dollars (Elon Musk has claimed $2 billion before to develop a Saturn V class rocket which would be larger than the SpaceX Heavy). What is interesting is that they seem intent on developing the vehicle using the current Merlin engines rather than than a new F-1 class engine (the rocket engines used on the Saturn 5, five on the first stage and one on the second stage). A cluster of 27 engines (!) will power the first stage. This technique of small rocket clusters is known to have caused trouble for the Soviets when they tried it (four launch failures in a row). With modern technology, the odds are probably better, both because an engine failure that is about to wipe out some of its neighbors can be detected and a shutdown attempted. Second, control systems are much more sophisticated. One can design a system with random engine outs (that is, engines that aren't firing for some reason) that can still fly. We'll see if that's good enough.

    The interesting thing from a development perspective is that this means a good portion of the testing is already done since the Merlin engines have been successfully flown on four flights (two Falcon I and two Falcon 9). They already claim that they are the top manufacturer of rocket engines by number (though I don't know if they are by total thrust). They also have some success firing Merlin engines in clusters and on the successful Falcon 9 flights. They'll probably have to make a more sophisticated avionics and control system, plumbing/pumping to supply the much larger engine cluster, and the vehicle frame, but I suspect that they won't have to do much more than that. My guess is that the 27 engine cluster and its plumbing will be fairly tricky as will the control system (which has to be able to handle several engine outs), but the rest won't be.

    Now compare it to the Shuttle derived Space Launch System (SLS) that Congress wants NASA to research. For one or two years of funding of the SLS (and incidentally, about the same amount of funding just to maintain the current Shuttles!), SpaceX probably can develop the SpaceX Heavy. It doesn't have quite the capability that the SLS would have (at least on paper!), payload is a bit over 50 metric tons to LEO (low Earth orbit) while even a minimal SLS design is required to be able to carry 70 metric tons (at least as NASA read the Congressional directive) to LEO) Yesterday, there was gnashing of teeth because the last Space Shuttle was coming up with a possible end to the US's space program in the works. Now we have a rocket that not only would be vastly cheaper, but capable of carrying far more payload than the Shuttle. This may be our chance to get our space program back on track from when it derailed in the 70s.

    1. Re:A game changer, if they can get it to work. by kaiser423 · · Score: 2

      That crossfeed is really where they get a good chunk of their performance numbers from. I expect 15-20% increase from doing that....but it does make the plumbing pretty expensive and complex :)

      For those whom aren't familiar with crossfeed, the outer-tanks keep the main tank topped off during flight, so that at liftoff you get thrust from all engines, but when seperation time comes, the stage seperates, but your main core is still full of fuel. It's almost like launching a Falcon 9 from halfway outside your gravity well. You get good performance :)

      As far as I know, it's never been done before due to certain complexities with pressures, sloshing, pogo-ing, etc. It would be quite the revolution if they could pull it off reliably.

    2. Re:A game changer, if they can get it to work. by trout007 · · Score: 2

      The Shuttle Cross Feeds. The engines are on the Orbiter and the fuel is in the External Tank. It's not exactly the same because you aren't switching the engines from two different tanks which is what will have to happen on the Falcon 9 Heavy. It's the switch that may be tricky.

      --
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    3. Re:A game changer, if they can get it to work. by DerekLyons · · Score: 2

      What is interesting is that they seem intent on developing the vehicle using the current Merlin engines rather than than a new F-1 class engine (the rocket engines used on the Saturn 5, five on the first stage and one on the second stage).

      Saturn V had five F-1 on the first stage, five J-2 on the second, and one J-2 on the third.
       
      That being said - using smaller, existing, engines is a way to cut development costs and to bring the booster to market early. (I.E. pretty much standard corporate behavior, but a behavior we've all seen go badly wrong before.)
       

      A cluster of 27 engines (!) will power the first stage. This technique of small rocket clusters is known to have caused trouble for the Soviets when they tried it (four launch failures in a row).

      It's also known to be wildly successful for the Soviets too. The N1's problems were less due to clustering than due to lack of proper engineering and testing and a deeply flawed assembly, checkout, and launch flow.
       

      They'll probably have to make a more sophisticated avionics and control system, plumbing/pumping to supply the much larger engine cluster, and the vehicle frame, but I suspect that they won't have to do much more than that.

      Wow... It's only April and that's pretty much a shoo-in for the "Understatement Of The Year" award.
       
      Between now a flying rocket there are a number of significant hurdles to jump...
       
      They'll have to develop a complex and sophisticated thrust structure that can take the thrust and (when maneuvering) side loads of all those engines without having any nasty vibration modes. (And it has to handle a large number of arbitrary modes where one or more engines are shut down.) Making that job even harder is the need to route a complex and sophisticated piping system to deliver the fuel and oxidizer in the required quantities without flow problems or their own nasty vibration modes through that thrust structure. And the piping system has to handle startup transients gracefully, fail gracefully when engines shut down in arbitrary numbers and locations, and handle shutdown transients at end of burn gracefully regardless of how many engines are running and in what locations.
       
      All of that's going to be a tall order indeed. I'm not saying it's impossible mind you, just that you vastly underestimate the issues.
       
      And that's without even mentioning the vast issues the engine and flight control systems will have of their very own.
       

      Now we have a rocket that not only would be vastly cheaper, but capable of carrying far more payload than the Shuttle.

      It might be vastly cheaper, it might not be. It might be capable of carrying far more, or it might not be. It's a paper rocket, and paper rockets are always wonderful. There's a lot of really big "if's" and unknowns both known and unknown between here and there.
       

      This may be our chance to get our space program back on track from when it derailed in the 70s.

      There's two huge unspoken assumptions buried in that statement:
       
      First, that there's some preordained or ideal course for our space program.
       
      Second, that choosing a course based on political expediency back in the 60's and abandoning slow step-by-step development in favor of Big Stunts (I.E. the course you want to return to) wasn't itself a derailment of a reasonable space program.

  8. Re:New To Space Vehicles by Confusador · · Score: 3, Informative

    What you're looking for is not a capability of the Falcon Heavy, but their Dragon spacecraft which launches on the Falcon 9. They recovered it from orbit in December, so I'll let them show it to you: Specs, Mission update. Short version is that it's your basic capsule design with water landing, they're hoping to have the next version be a rocket landing on ground, using the abort motors.

  9. Re:Vaguely remember... by IICV · · Score: 5, Informative

    ...but NASA also needed $12 billion and a decade to make a pen that worked in 0 gravity... and the Russians just used a pencil, classic.

    There's pretty much nothing true in that statement besides the claim that "the Russians just used pencils" - NASA did too, until after Fisher developed the space pen (without government funding) and asked NASA to try it. In fact, after NASA adopted the space pen, so did the Russians.

    And there's problems with using pencils in space - wood pencils are flammable, and the graphite in mechanical pencils can snap off more easily and damage vulnerable equipment (it's conducive, after all) or the astronauts themselves, if they accidentally inhale it.

  10. Re:His designs are in NASA archives at Marshall SF by Burdell · · Score: 4, Insightful

    Yep. My father worked on every Saturn (guidance and control, especially the LVDC on the IU) except SA-1 (and then Shuttle, X-33, and now Ares). He retired from civil service a few years ago and now works part-time for a contractor, but if Congress/Obama can't get a budget passed and Dad goes home for a while due to a shutdown, he might not go back. There aren't many others left around from that era.

    Even if you had the knowledge and the people, you wouldn't build another Saturn V anyway. You couldn't rebuild the same computers, so you'd update the computers and programs, at which point you might as well upgrade the engines, which leads to changes in the structure (since you have to build new dies and jigs anyway), etc. The test a few weeks ago at Marshall showed that the consensus for structural strength (that even SpaceX and such have used) was off by about a factor of 2 (the rocket structure was about twice as strong, and thus as heavy, as it needed to be).

    Even the second run of Saturn V vehicles (if they had been built) would have been different, with upgraded engines (the J-2X was developed during the Apollo program, and then pulled out for Ares I), similar to the changes the Space Shuttle underwent during its 30 year run.

  11. And it can lie on its side, too by Animats · · Score: 2

    I'm impressed that the Falcon-9 rocket can lie on its side, supported at only two points. Many large US rockets don't have enough strength in torsion for that, and must be assembled vertically.

    This reduces cost. The thing can be built in a factory bay of reasonable size, then barged and/or trucked to the launch site. There's no need to do final assembly near the launch pad.

    This is a good sign. One of the big problems with US rocketry has been that fanatical weight reduction resulted in overly fragile vehicles. This thing looks tougher.

  12. Re:Elon Musk by jnaujok · · Score: 2

    Then he would have been stuck in a dead-end position as a glorified draftsman being told by his superiors that, "you can't do that." His econ degree let him see how to make PayPal work, his dabbling in physics inspired him to go ask "why not" when told it couldn't be done. The money he made from PayPal let him put his arguments to the test (his money where his mouth is.) Had he gone into technology... we would still be buying stuff on ebay with money orders, and the Constellation project would be $15B over budget and 8 years late.

    --
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  13. Not the world's most powerful rocket by Snarky+McButtface · · Score: 2

    SpaceX stated it was the most powerful rocket since the Apollo era. They also said a larger rocket would be needed for a Mars mission. http://www.bbc.co.uk/news/science-environment-12975872