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Blue Origin Launches and Lands the Same New Shepard That Few In November (blueorigin.com)

MarkWhittington writes: The commercial space race between Blue Origin and SpaceX got more interesting on Friday. In November, Blue Origin launched its New Shepard booster on a suborbital flight, and then successfully landed it afterward. On Friday, Blue Origin relaunched the same New Shepard spacecraft to a height of 101.7 kilometers, and then landed it a second time. Blue Origin has therefore accomplished a first by flying a vertical takeoff and landing rocket into space twice in a row. The company has taken another step toward its goal of taking the rich and adventurous on suborbital jaunts for fun and profit.

132 comments

  1. Ummmm.... by click2005 · · Score: 4, Informative

    'Few in November'? lol

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

      Not being familiar with the subject, that threw me completely off when I read it.

    2. Re:Ummmm.... by SylvesterTheCat · · Score: 2

      Not being familiar with the subject, that threw me completely off when I read it.

      Are you sure it didn't "trew" you off?

    3. Re:Ummmm.... by Anonymous Coward · · Score: 0

      I think he meant 'phew' - as in being very relieved that it worked at all.

    4. Re:Ummmm.... by Opportunist · · Score: 3, Insightful

      Slashdot has turned from a labor of love (when we had good, topical stories that even had some background research now and then) to a cash cow and ad mouthpiece (when it was turned over to dice and we started playing the "spot the astroturf ad article du jour" game) to the current "we don't even give half a shit anymore" situation.

      Seriously. Be honest. Does anyone read the stories anymore before they get frontpaged? I get that suspicious feeling that if I could get a few /. trolls together we could easily get a Lorem Ipsum on the frontpage.

      --
      We used to have a Bill of Rights. Now, with the rights gone, all we have left is the bill.
    5. Re: Ummmm.... by Anonymous Coward · · Score: 1

      The people that used to come here in droves are still around. Someone should start a new /. with better quality control etc. That's what wrecked it for me and caused me come here rarely when before it was multiple times a day.

    6. Re:Ummmm.... by Gavagai80 · · Score: 2

      I started reading slashdot in '99. I can't recall a time when the editors ever appeared to read summaries before posting them. And before Dice and startswithabang, it was ohnoitsroland. All along people have been insisting that slashdot used to be great back in the day but the standards are gone. I don't believe there ever were standards. Take it or leave it. I still enjoy it.

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      This space intentionally left blank
    7. Re: Ummmm.... by caseih · · Score: 1

      What do you think of soylent news? When they started they billed themselves as continuing the ideal of what Slashdot used to be. Personally I don't find the stories and comments to be all that great on soylent. Slashdot still wins by a very small amount in my opinion.

    8. Re: Ummmm.... by Anonymous Coward · · Score: 0

      Sadly soylent news management has just as much of a social justice, shit-stirring, flame-baiting bent as slashdot.

    9. Re: Ummmm.... by MrL0G1C · · Score: 1

      And Slashdot looks nicer [ducks].

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      Waterfox - a Firefox fork with legacy extension support, security updates and better privacy by default.
    10. Re: Ummmm.... by Anonymous Coward · · Score: 0

      Hey Timothy,

      What's the secret to your job security? Do you at least get an unpleasant stare from your boss?

    11. Re: Ummmm.... by tehcyder · · Score: 1

      And Slashdot looks nicer [ducks].

      Soylent News looks like slashdot from the early 2000s, which I suppose some people think is cool.

      --
      To have a right to do a thing is not at all the same as to be right in doing it
  2. holy crap by p0p0 · · Score: 4, Insightful

    Timothy. Calm down. Take a deep breath. Spelling isn't that hard. It reflects really poorly on this site when the editors can't spell. This happened on the article just before this too.

    1. Re:holy crap by Anonymous Coward · · Score: 0

      Hey, Take it easy! The spell check said it was OK! POST EAT!!!

    2. Re:holy crap by elrous0 · · Score: 4, Funny

      In his defense, he's very drunk.

      --
      SJW: Someone who has run out of real oppression, and has to fake it.
    3. Re:holy crap by msauve · · Score: 3, Funny

      Elisa could pass the Turing test if the competition was timothy.

      --
      "National Security is the chief cause of national insecurity." - Celine's First Law
    4. Re: holy crap by Anonymous Coward · · Score: 0

      I think it's more of a typo than spelling error.

    5. Re:holy crap by Anonymous Coward · · Score: 3, Funny

      Hay, take it easily! The spiel chuck said it wash OK! PROUST EEL!

    6. Re:holy crap by Anonymous Coward · · Score: 1

      He is calm. Look, there's a certain honesty in showing that you really, truly, just don't give a shit. I almost admire Timothy for that. He's sitting there for every story and weighing up whether to spend the time reading the text before posting, or whether to just post it and have another donut instead, and the donut wins *every single time*. You can't buy consistency like that.

    7. Re:holy crap by Anonymous Coward · · Score: 1

      In his defense, he's very drunk.

      In my experience this line of defense only works if everyone involved is as drunk as you are or otherwise sufficiently medicated.

    8. Re:holy crap by aralin · · Score: 1

      I noticed quite a flew of those spelling errors.

      --
      If programs would be read like poetry, most programmers would be Vogons.
    9. Re:holy crap by hawk · · Score: 3

      >Spelling isn't that hard. It reflects really poorly on this site when the editors can't spell.

      You must be new around here . . .

      hawk

    10. Re:holy crap by Anonymous Coward · · Score: 0

      You would think they would at least pay attention to subject lines because they know that if they have to change those, it pushes another RSS article, which pisses off the ten remaining people who still use RSS to keep track of Slashdot. The worst part is that I learned this from TImothy himself at a Slashdot anniversary thing a few years ago.

  3. That Few In November? by Kneo24 · · Score: 1

    I just can't ignore the errors anymore. This is just stupidly bad.

    1. Re:That Few In November? by currently_awake · · Score: 1

      Spotting spelling errors and punctuation mistakes is a very useful trait for professional programmers, as it speeds up debugging.

  4. Blu Origins lunches and landz teh sam new chepard that phew in novemberer.

    FTFY

    1. Re:Few? by itsdapead · · Score: 1

      I could believe it if it was a SpaceX press release: I get so many emails from PayPal saying "Dear Mr spamtrap49 your accounting was using for suspicious transaction, and has be suspended. Please clicking here to conform your detail" that its clear Elon Musk can't spell. Yet the emails from Amazon telling me that I might be interested in books similar to the one I bought for my mum's birthday 5 years ago all seemed to be written in perfect English...

      --
      In a survey of 100 programmers, 111111 thought that duck-typing was a good idea.
  5. How do you "land rocket in space"? by Anonymous Coward · · Score: 0

    "Blue Origin had therefore accomplished a space first by flying a vertical takeoff and landing rocket into space twice in a row."

    1. Re:How do you "land rocket in space"? by U2xhc2hkb3QgU3Vja3M · · Score: 1

      Blue Origin had therefore accomplished a space first by flying a "vertical takeoff and landing" rocket into space twice in a row.

    2. Re:How do you "land rocket in space"? by Marginal+Coward · · Score: 1

      Or even: "Blue Origin had therefore accomplished a space first by flying a vertical-takeoff-and-landing rocket into space twice in a row."

  6. No comparison by Anonymous Coward · · Score: 5, Insightful

    How can anyone compare Blue Origin and SpaceX in the same paragraph while still mentioning that Blue Origin flights are sub-orbital? There's really little basis for comparison at that point between Blue Origin and SpaceX and more comparison between Blue Origin and Scaled Composites. Of course Scaled Composites *already* flew multiple sub-orbital flights with SpaceShipOne - who cares that it wasn't a vertical take-off and landing - it's *still* more comparable.

    1. Re:No comparison by Anonymous Coward · · Score: 0

      That depends on what you consider to be the hard bit. Otherwise you're just complaining that this was a feat performed with a blue rocket rather than a green one.

    2. Re:No comparison by AJWM · · Score: 1

      SpaceShipOne isn't single stage, it needs a lift. In that arena, the X-15 takes priority. (Several X-15 flights earned their pilots astronaut wings.)

      --
      -- Alastair
    3. Re:No comparison by itsdapead · · Score: 3, Insightful

      That depends on what you consider to be the hard bit.

      I think you'll find that the "hard bit" is putting a payload into orbit and, for extra points, not needing twice as much fuel as a disposable rocket (which is why SpaceX are trying to land on a barge in the middle of the sea rather than flying all the way back to the launchpad).

      Otherwise you're just complaining that this was a feat performed with a blue rocket rather than a green one.

      Actually more like comparing a silver, red and blue rocket with an orange one.

      --
      In a survey of 100 programmers, 111111 thought that duck-typing was a good idea.
    4. Re:No comparison by Anonymous Coward · · Score: 0

      Why are these the hard parts of landing, please?

    5. Re:No comparison by Immerman · · Score: 5, Insightful

      They're not, technically. And SpaceX has already done *lots* of rocket landing with the Grasshopper test vehicle.

      The hard part is scaling the technology up enough to be useful - there's lots of non-linearities in the real world that confound such endeavors. Just a couple:

      Getting up to speed while carrying a second stage requires a LOT more fuel, meaning the difference between launch weight and landing weight are MUCH greater. To the point where the Falcon uses only one of its nine engines when landing, throttles it down as far as it can go, and still is producing too much thrust to be able to hover. And being able to hover makes a *huge* difference in ease of landing - just stop a few feet above ground and then ease yourself down, rather than having to time things perfectly so that you hit zero vertical speed just as you touch down. Stop a foot too high and you can't get down short of cutting the engines and falling, stop a foot too low and you get serious impact damage.

      Wind shear - thanks to the much taller profile, torques from ambient breezes are going to be much greater on the bigger rocket, increasing with roughly the square of height.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
    6. Re:No comparison by TWX · · Score: 3, Insightful

      And this is why Blue Origin's accomplishment, while interesting, is not as noteworthy as it initially sounds. If I understand right, they've sent a payload-less rocket up to the arbitrary border of space (ie, 100km) twice and landed it. As it was payload-less it didn't do any actual work.

      If the rocket doesn't do any actual work then it's not a lot different than my shooting-off model rockets. It's interesting, it's fun, but it's not accomplishing a goal other than shooting-off rockets.

      SpaceX has launched a payload for a customer and landed the rocket. Hopefully in their next few launches they'll land more rockets and be able to turn around and fly them again with more payloads. That would actually be a noteworthy accomplishment.

      --
      Do not look into laser with remaining eye.
    7. Re:No comparison by Anonymous Coward · · Score: 0

      Still, the fact is that a bunch of Musk fanboys had their asses burnt over this.

      Now they're all crying over it and claiming that Blue Origin really didn't do anything because there was no payload. That's like saying the Wright brothers never flew a real airplane because there weren't any passengers onboard.

    8. Re: No comparison by dunkelfalke · · Score: 1

      Same thing with the first American in space. Also just a sub-orbital flight.

      --
      "It's such a fine line between stupid and clever" -- David St. Hubbins, Spinal Tap
    9. Re:No comparison by Anonymous Coward · · Score: 0

      While it lacked a second stage, the Blue Origin launches were certainly not payload-less: both launches carried a prototype of BO's space tourist capsule, which parachuted down separately from the rocket itself.

    10. Re:No comparison by Anonymous Coward · · Score: 0

      And being able to hover makes a *huge* difference in ease of landing - just stop a few feet above ground and then ease yourself down, rather than having to time things perfectly so that you hit zero vertical speed just as you touch down. Stop a foot too high and you can't get down short of cutting the engines and falling, stop a foot too low and you get serious impact damage.

      When you put it like that, it sounds exceedingly fragile and unreliable. Do you really understand how it works?

    11. Re:No comparison by Anonymous Coward · · Score: 0

      Heck, Armadillo Aerospace also did this, just not as high. But the number of flights were far higher in numbers.

    12. Re:No comparison by Anonymous Coward · · Score: 1

      Not payload-less, but BO's capsule is estimated at around 10 tons while SpaceX's second stage + payload is 125 tons and separates at Mach 4.8.

    13. Re:No comparison by N3wsByt3 · · Score: 1

      Let's give this a rest. It sounds as immature as the "playstation vs. Xbox" flamefest-conundrums.

      As far as *the 1st stage* goes, both are sub-orbital. Yes, SpaceX' one gets further and faster and has a bigger one than Blue Origin. Fine, they win the d*ck-contest.

      The real point however, is that both are working on reusable vehicles, where none did before. (No, I'm not counting the spaceshuttle). There is nothing wrong with some good competitive tong(s)-in-cheek(s). I don't get why fanboys of either side are getting so riled up about. As far as I remember, Blue Origin has been working for the last 3 years on a much larger, orbital rocket based on the New Shepard, which probably we'll get some news of this year. So no doubt some are going to complain about who has the biggest rocket that does the hardest job then too, but in reverse... until SpaceX makes the second stage reusable. Rince, repeat.

      The whole "how dare they say they play in the same courtyard as us?!" is really absurd. They are both doing an admirable job.

      --
      --- "To pee or not to pee, that is the question." ---
    14. Re:No comparison by N3wsByt3 · · Score: 1

      Ermm... Everyone makes mistakes, but if you're going to base your whole reasoning and conclusion on an argument, you'd better be sure it's true.

      Alas, it ain't. It was not payload-less, and thus, following your own reasoning; it did do actual work. Ergo, it *IS* a lot different than your shooting-off model. Hence, it *IS* accomplishing a goal other than shooting-off rockets.

      The whole thing you said broke down, thus.

      --
      --- "To pee or not to pee, that is the question." ---
    15. Re:No comparison by N3wsByt3 · · Score: 1

      It's just exaggerated nonsense and hyperbole. I'm getting a bit fed up with all this fanboism on both sides.

      Yes, SpaceX has it harder, but not THAT much harder. The main systems and mode of operandi is largely the same for both rockets. There is nothing drastically and qualitative different between it, only quantitative. Blue Origin also has to compensate for winds, also has to make sure the avionics work perfectly, also has to see that the propulsion negates the downwards (falling) speed, etc. SpaceX has it *more*, but it's not like it's another beast altogether. No, it's the same kind of beast, only more ferocious. That's the gist of it.

      People who pretend it's *drastically* different just are spouting nonsense. It's like, otherwise, it would somehow diminish the accomplishment of Elon Musk and SpaceX. Which it doesn't. Both make great contributions in novel rocketry. I don't see the need of dishing someone to let another shine more. We're not in kindergarten anymore, I would have presumed.

      --
      --- "To pee or not to pee, that is the question." ---
    16. Re:No comparison by Bruce+Perens · · Score: 3, Insightful

      If it only carries its payload up and down without reaching orbit, it's sounding rocket. and It should be compared with Strypi in that case rather than Falcon 9.

    17. Re:No comparison by FirephoxRising · · Score: 1

      Can they not have one engine that's "special" and can throttle down further, maybe at the cost of some peak power? Or have two "specials" for redundancy. I suppose it would depend on whether they need every bit of thrust on takeoff for that mission. They could maybe have the "special" version of the Falcon9 for non-max-power missions for easier landings, and only use the standard rig Falcon for the heavy launches?

    18. Re:No comparison by Gavagai80 · · Score: 3, Informative

      It's hard to overstate the difference between 100km freefall tourism (without the tourists yet but let's presume they'll be easy to add) and putting payloads into orbit. The delta-v to orbit is about six times more.

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    19. Re:No comparison by Anonymous Coward · · Score: 0

      The booster SpaceX returns is also suborbital. It's the exact same accomplishment, there's just no second stage on the Blue Origin rocket.

    20. Re:No comparison by Dog-Cow · · Score: 1

      Maybe you should direct your question a rocket scientist. I think SpaceX has some.

    21. Re:No comparison by stevelinton · · Score: 1

      The key thing is mass budget. If it helps Blue Origin land more reliably to add a ton of structural bracing or whatever, it's no big deal. For SpaceX its a huge deal.

    22. Re:No comparison by N3wsByt3 · · Score: 0

      But it wasn't payload-less. Let's agree to that, at least. Making the argument into a 'sounding rocket' is another argument.

      In that case: the problem is, how you make the comparison. If you only take the part that actually returns - which makes sense, since it's that which all the fuzz is about - then one has to acknowledge the first stage of SpaceX ALSO only reaches a suborbital plane, and thus, is also nothing more than a 'sounding rocket'. The fact that the rocket in its totality wasn't, doesn't mean the stage that returns is any more than the equivalent of a sounding rocket.

      I'm not saying it's not harder for SpaceX, but I do find it annoying when people act as if it's something totally different. It ain't. It's difficult for the other stages, but for the first stage, which comes back, it has to do more or less (mostly more) the same as what Blue Origin does. there is no *intrinsic* difference between the two. For instance, you could launch the first stage od SpaceX on its own too, and it would almost be exactly the same as Shepard, then. The fact that it now has a second and third stage that manages to go into orbit, does nothing for the fact that the first stage, which is returnable and similar to that of Blue Origin, has the same basic features as the one of Shepard.

      I agree that it's more difficult, because of the fact they, indeed, have to put up the second and third stage too, but it's not like it's totally incomparable, as some seem to imply. The part that returns is what counts, and both were not payload-less, nd both can be considered sounding rockets, if comparing the recuperable parts.

      --
      --- "To pee or not to pee, that is the question." ---
    23. Re:No comparison by N3wsByt3 · · Score: 1

      Yes, but one has to be honest, here. The thing which is comparable, is the part that gets returned (aka, is recuperable). That's what all the fuzz is about. So, taken that it handles bout that part, it means comparing Shepard to the first stage of SpaceX. Not shepard compared to the whole rocket.

      In the end, it's not the first stage that puts up the satellite into orbit, but the second and third stage. The first stage, on itself, only manages to get into a suborbital plane too.

      Granted, it has to put more effort into it, *because* it need to lift the other stages, but it's not drastically different. IF you compare the comparable parts, that is.

      For instance, let's assume SpaceX gets into space-tourism too, and uses only its first stage for it. Well, than you get something which is more powerful, but not something drastically different than Blue Origin. It would still be suborbital, as 'sounding rocket', etc.

      I think much of the confusion stems from how one looks at it. If one does it from the point of the totality of the rocket, and see what it can accomplish, or if you just compare the part where the novelty and innovation is, namely in the recuperable part.

      --
      --- "To pee or not to pee, that is the question." ---
    24. Re:No comparison by Anonymous Coward · · Score: 0

      As far as *the 1st stage* goes, both are sub-orbital.

      The difference that you apparently refuse to acknowledge is that SX's rockets actually launch a real payload before attempting a landing. BO's was just a "HEY LOOK AT ME!" test flight.

      That's like saying "As far as *ejaculation* goes, both sex and masturbation get your rocks off."

    25. Re:No comparison by Anonymous Coward · · Score: 0

      "It's exactly the same thing, except for the lack of a second stage!"

      "Riding a bicycle with training wheels is exactly the same thing, except for those two extra wheels on the side!"

    26. Re:No comparison by Anonymous Coward · · Score: 0

      These kinds of comments are why we need another moderation level above 5. maybe one where when you get enough votes your post is automatically appended to the bottom of the article as a "Community highlighted comment". Just an idea.

    27. Re:No comparison by Bruce+Perens · · Score: 1

      Blue Origin will eventually have a two-stage rocket that can reach orbit (although they are planning on a much smaller payload than SpaceX for their first iteration). When the booster of that rocket lands without damage, they will duplicate what SpaceX has recently done, although in smaller scale.

      Blue Origin to SpaceX at present is a sort of bicycle-to-automobile comparison if you account for the tremendous difference in energy and the application. So, I think there really is an intrinsic difference between the two of them.

      If you want to say there's no intrinsic difference, then we need to look at Orbital's Stargazer and Pegasus, which have been carrying small payloads to orbit for years, and there's only been one Stargazer all of that time so there is no question that it's reusable. The only difference is that Stargazer lands horizontally.

      We can then look at the B-52 and X-15 combination, in which both stages were reusable, a human was the payload, and we're going back to the late 1950's.

    28. Re:No comparison by N3wsByt3 · · Score: 1

      I respectfully disagree, at least to some extent. The reason why we compare both things (the first stage of spaceX, and Blue Origin Shepard, is because they are similar. In both cases, the same principles apply, and the same mode of operandi is used. So the analogy would be rather be two cars. One could say one is a Polo Volkswagen (Blue Origin), and the other a Porche (SpaceX first stage), but no-one would claim they aren't both cars. EVEN when then saying "Ah, but the Porche is much faster, goes a longer way, has more comfort, is safer, etc. That may all be, but it's still an evolutionary, not a revolutionary difference. there is no way you would take one to be a bicycle, and the other a car - since those would be completely DIFFERENT systems, with completely different modes of operandi.

      Which why one does not compare that with , say, a winged vehicle. Because that IS a completely different kind of machine. Think about this yourself. If you really would want to put all these vehicles in groups, similar to species or families in biology, would one *really* place those two together? I don't think so. Idem with rockets, and any other vehicles for that matter. I can't imagine people saying a polo isn't a car because a porche is faster and can do more. Such an arbitrary distinction makes no sense. (Which doesn't mean the Porche isn't faster, btw, just like SpaceX first stage is, indeed, more powerful and ha to do more work. )

      Thus, similarly, it's obvious that, if you want to compare Orbitals' Pegasus, you'd compare it to virgins galactic White Knight Two and SpaceShipTwo. And I think almost everyone can see why: they're similar concepts. This would be true EVEN if spaceship two would be able to go in a low Earth orbit. Nothing *inherently* changes to the concept and method, after all. It's just more and better of the same. Yes, it reaches a new milestone, but that doesn't change the basic concept of it.

      Look at it this way: an airplane doesn't stop being an airplane because it can't break the sound barrier neither. Would one, thus, following the same (your) reasoning, claim it's like comparing 'a kite to an airplane', if it doesn't reach the sound of speech? Argue that an airplane that can't breach that barrier shouldn't be considered an airplane anymore, because it is *intrinsically different*?

      That sort of analogy doesn't make sense, if you look at it objectively.

      --
      --- "To pee or not to pee, that is the question." ---
    29. Re:No comparison by N3wsByt3 · · Score: 1

      ermm... errata: speed of sound. But I think you got that ;-)

      --
      --- "To pee or not to pee, that is the question." ---
    30. Re:No comparison by N3wsByt3 · · Score: 1

      ?
      Even when taking your example: one would be hard pressed, even when saying " the one feels far better and can get a woman pregnant while the other can't" to say one or the other *does not* involve ejaculation. ;-)

      But anyhow, a rather incorrect remark. I didn't refuse to acknowledge anything of the sort. Blue Origin had a payload, just like SpaceX. SpaceX had a far bigger payload, and put it far further, thanks to a second, non-recoverable stage.

      So?

      What I'm contesting here, is the fact that people act as if the two systems (the reusable part) are totally different concepts, and act as if the two can't be compared. They use arguments like 'it was a sounding rocket', and 'it was suborbital' to substantiate their claims. But the fact is, BOTH systems which are compared (aka, the returnable/reusable part, as THAT is what the fuzz is about), were suborbital and 'like a sounding rocket'. There isn't an inherent difference in it, thus, as far as the return-part is concerned. They both use the same basics, the same systems, and the same mode of operandi.

      This does not mean one doesn't acknowledge that SpaceX had to put more work into it and created a more powerful version - which was a strawman-fallacy of your part, since I certainly didn't say anything of the sort.

      --
      --- "To pee or not to pee, that is the question." ---
    31. Re:No comparison by N3wsByt3 · · Score: 1

      And when one can hold ones' balance and don't need the training wheels, it wouldn't matter, even if the extra wheels were still on it. It would still mean you could ride a bicycle.

      What you and your ilk are claiming, would be more akin to this: because one person carries another with him on his bicycle, that is considered 'riding a bicycle' (since he takes another person (aka payload), and even goes faster and further... while the other does not, because he doesn't carry a passenger and doesn't go as fast and as far.

      Clearly, such an arbitrary defining measurement is nonsensical.

      Riding a bicycle, thus, is not defined by the *existence* of the training wheels on itself, nor by carrying a person, or going faster or further. Similarly, a "reusable space-rocket" does not need to put something into orbit. It only has to demonstrate it 1) can reach space (which it did), and that it is 2) reusable (which it did).

      --
      --- "To pee or not to pee, that is the question." ---
    32. Re:No comparison by TWX · · Score: 1

      I don't think that the differences in the vehicles in your analogy reflects the disparity between the two rockets.

      I think Blue Origin is more like an electric city-car like the one Ford has based on the Focus, or the electric version of the Fiat 500. Very short range, no significant cargo capacity, can move a few people around a short distance and is severely range-limited. By contrast the SpaceX rocket is more like a small box-truck or large high-roof van. Certainly not the carrying capacity of a tractor trailer or a huge box truck, but suited to leaving the city and with several times the range of the electric.

      --
      Do not look into laser with remaining eye.
    33. Re:No comparison by N3wsByt3 · · Score: 1

      Well, it's a point of contestation I suppose, but certainly we seem to agree that they *are* both cars, then.

      Also... if one looks at the reusable part(s), the difference is mainly in weight-carrying capacity. More akin to an analogy where spaceX is a SUV which is carrying another small car, while the other is a normal city car. Now, the combination of the SUV + small car will far outweigh the city car and be able to go much further, but if one only compares the SUV with the city car, the discrepancy won't be *that* big. Sure, the SUV might still go a bit faster and a bit further, but not drastically so, at least not to the point where one would say they can't be compared with eachother anymore, or that it's like a 'bicycle versus a car', as some have put it. It doesn't mean the SUV isn't more powerful and can't carry more weight, because it certainly is and can, but it's perfectly fine to acknowledge both have improved the miles/gallon considerably.

      And if the city car was first to show it's possible to do 100miles a gallon, it deserves as much recognition as the SUV showing the same thing later on, even if it's about a SUV with more power and load-capacity, then.

      --
      --- "To pee or not to pee, that is the question." ---
    34. Re:No comparison by Big+Hairy+Ian · · Score: 1

      In their defense it got higher than Alan Shepard got when he became the first American in space

      --

      Build a Man a Fire, and He'll Be Warm for a Day. Set a Man on Fire, and He'll Be Warm for the Rest of His Life.

    35. Re:No comparison by Anonymous Coward · · Score: 0

      I suppose the issue is which element you consider more important, and which direction it's considered to be better. Shepard has a presumably "done" reusable rocket, but needs to up the throw weight to be useful. SpaceX has a useful rocket, but it's re-usability isn't quite there yet. Both are impressive in their own way. The trick is, what's easier - for Shepard to scale their reuse plan up to orbital throw weights, or for SpaceX to take their orbital throw weight and solve the landing issues?

      Personally, I think my money is on SpaceX - they're in a position to launch things *now*, and getting re-use is just a bonus to the bottom line. They can be making money on the venture today, and as the successful landing % goes up, they just make more money. But I'm glad to see both ventures working on it - little competition is good for the corporate soul.

    36. Re:No comparison by Immerman · · Score: 1

      Well said. I'd mod you up if I could.

      --
      --- Most topics have many sides worth arguing, allow me to take one opposite you.
    37. Re:No comparison by N3wsByt3 · · Score: 1

      Well, agreed, but only if you take the goal to be an orbital flight. If - as it is with Blue Origin - the goal is to get rich tourists go up into space at a reasonable price, then clearly *they* are much closer.

      For that goal, they just have to demonstrate 1)they can go into space (which is defined at reaching a height of 100km, NOT reaching low earth orbit), and 2)have a reusable rocket, so they can drastically lower the price. They have now shown to have reached those sub-goals, so they can now reach their (that specific) goal, and do sooner than anyone else.

      However, I largely agree with you, if one takes the long term goal, which is getting payloads into LEO, which, no doubt, Blue Origin will try too, sooner or later.

      Anyway, the problem I have with many comments, is that they tend to be derisive of one or the other. It's pretty silly, and reminiscent of the 'Xbox vs playstation' flamewars. It's silly and immature. As some journalists have pointed out, it's NOT about 'blue orgin vs spaceX', but about the new ideas versus the old. And Blue Origin and SpaceX are both in the camp of the novel and visionary ideas, which can potentially be a disruptive technology. Can't happen soon enough, imho.

      --
      --- "To pee or not to pee, that is the question." ---
    38. Re:No comparison by N3wsByt3 · · Score: 1

      I'm not even sure the parent poster is correct. As far as I have been able to research it, they say they needed to make the engine throttable, just because at full power it was too powerful. But they *did* make it throttable. No-where did I see that SpaceX still had the same problem with their engine being throttled to the lowest power.

      --
      --- "To pee or not to pee, that is the question." ---
  7. Read on by Anonymous Coward · · Score: 0

    It just gets better...
    "The company has taken another step toward its goal of taking the well off and adventurous on suborbital jaunts for fun and profit."

    Huh? I keep trying to interpret that.

    I think all companies should "take the well off" and "adventurous on suborbital jaunts'

    1. Re:Read on by TigerNut · · Score: 2

      It just gets better... "The company has taken another step toward its goal of taking the well off and adventurous on suborbital jaunts for fun and profit."

      Huh? I keep trying to interpret that.

      I think all companies should "take the well off" and "adventurous on suborbital jaunts'

      That's not so bad. You need to read it as The company has taken another step toward its goal of taking the well off and adventurous on suborbital jaunts for fun and profit.

      "the well off" and "adventurous" refer to people. "suborbital jaunts" is what they'd be taking part in.

      --

      Less is more.

    2. Re:Read on by reboot246 · · Score: 2

      "Well off" should have been spelled "well-off".

    3. Re: Read on by jofas · · Score: 2

      Should at least have used the correct "well-off". The whole blurb is a disaster of written "English".

    4. Re:Read on by NEDHead · · Score: 1

      or 'rich'

    5. Re: Read on by Anonymous Coward · · Score: 0

      Well, it ain't rocket science, you know...

    6. Re:Read on by N3wsByt3 · · Score: 1

      True. That said, most with a grain of of intelligence and being able to read comprehensively, would have gotten that.

      --
      --- "To pee or not to pee, that is the question." ---
    7. Re:Read on by Anonymous Coward · · Score: 0

      or "the 1%" or "your masters"

  8. Grue Orange Haunches? by mveloso · · Score: 1

    Grue Orange Haunches and Hands the lame few leopard that true in lavender?

  9. Altitude only first by AJWM · · Score: 4, Informative

    The "first" here is that New Shepard made it to the altitude arbitrarily defined as "space". The first launch and landing of a VTOL rocket that had previously flown was back in September of 1993 with DC-X's second flight (first was 8/18/93). Sure, it only went up a few hundred feet ... then stopped dead, hovered, translated sideways another couple of hundred feet, then landed. (I was present for that one. Frickin' awesome!) It flew yet again less than three weeks later.

    On June 7 and 8 of 1996, it flew twice within 26 hours. That second flight reached an altitude of 10,300 feet (its record). Nowhere near space, but the DC-X program was more about the control software and reusability than going for altitude (it was a one-third scale prototype of the proposed Delta Clipper). And they were doing it with what is now over twenty year old technology. (Actually older, the thrusters were modified RL-10s from the 60s, much of the flight control avionics was off-the-shelf units that McDonnell-Douglas used in its jet aircraft.)

    So, kudos to Blue Origin for reaching the edge of space with a previously-used rocket (something nobody else has done with the arguable exception of Shuttle, which was really never the same twice). But let's put the "first" emphasis where it belongs. (And it is significant -- it doesn't really matter how many times you can re-use a rocket if it won't get you to space in the first place.)

    --
    -- Alastair
    1. Re:Altitude only first by Anonymous Coward · · Score: 0

      The "first" here is that New Shepard made it to the altitude arbitrarily defined as "space".

      I don't think anyone was claiming anything other than this.

    2. Re:Altitude only first by Anonymous Coward · · Score: 0

      https://en.wikipedia.org/wiki/North_American_X-15#Record_flights

    3. Re:Altitude only first by AC-x · · Score: 1

      So, kudos to Blue Origin for reaching the edge of space with a previously-used rocket (something nobody else has done with the arguable exception of Shuttle, which was really never the same twice).

      Actually Scaled Composites performed the same feat over 10 years ago, don't you remember the X-Prize? They use different launch and landing methods, but right now Blue Origin is at the same point that Scaled Composites were back in 2004.

    4. Re:Altitude only first by Anonymous Coward · · Score: 0

      That's like comparing the wright flyer to a paper airplane.

    5. Re:Altitude only first by PvtVoid · · Score: 1

      That's like comparing the wright flyer to a paper airplane.

      Which is a pretty excellent comparison actually.

    6. Re:Altitude only first by Anonymous Coward · · Score: 0

      Thanks for sharing the link. As a kid, I was always fascinated to read about the X-15 (not old enough to have been alive when it ffew). I had forgotten that it qualified for spaceflight with even two flights meeting the international definition of 100km. Interesting that after 50 years, we are applauding a similar achievement.

      However, a quick read on the technology at the time (avionics, propellants, etc.) show significant progress, although nothing at the pace of rocketry in the 1920s through 1960s. Maybe the biggest delta now is that the economics are now at a point that private enterprise finally retook the innovation mantle from the government. With SpaceX, Blue Origin, and others, we are seeing the transition from the amateur (e.g. Goddard) to governments to business. Interesting times again for spaceflight.

    7. Re:Altitude only first by AJWM · · Score: 1

      As I mentioned in another post, the Scaled Composites achievement was first accomplished by the X-15 back when. SpaceShipOne didn't make it to space entirely under its own power, it had a lift from a carrier aircraft, just like X-15.

      Cool yes, but not what Blue Origin did.

      --
      -- Alastair
  10. Welcome aboard, Mike Tyson by Anonymous Coward · · Score: 0

    Dice got some class in the editor department.

  11. Space Race! by WindBourne · · Score: 4, Insightful

    Hopefully, this leads to a bit of a space race.

    However, to be fair, SpaceX is a LONG LONG ways ahead of everybody. They already have an orbital craft. They are able to land their first stage. They will likely re-use it in production sometime next year.
    FH will launch in April.
    Dragon v2 for human launches, will be end of year.
    Raptor is supposed to be finished and fully tested around early 2017.
    And that is on-top of MCT being developed.

    OTOH, ULA, Airbus, O-ATK, Russia, etc will feel the heat shortly.

    --
    I prefer the "u" in honour as it seems to be missing these days.
    1. Re:Space Race! by WindBourne · · Score: 5, Insightful

      LOL.
      They already comply with NASA and DOD standards and still their prices remain a fraction of ULA, Airbus, etc.
      And as to extracting money from the feds, ULA is nearly 100% dependent on the feds, while less than 1/3 of SpaceX are from govs.
      And when it comes to getting 'subsidies' from the feds, they take in a FRACTION of what ULA, Boeing, L-Mart, Airbus, BAE, etc take in. Hell, in all of these other companies, they require the feds to pay costs+, which is ALWAYS outrageous profits, while with SpaceX, the feds have paid only a fraction of the price. SpaceX continues to pour their profits into R&D.

      Finally, if they are so far behind that they are only 50's tech, then what companies are ahead of them and how much lower costs are they?

      --
      I prefer the "u" in honour as it seems to be missing these days.
    2. Re:Space Race! by turbidostato · · Score: 1

      "if they are so far behind that they are only 50's tech, then what companies are ahead of them"

      You already mentioned them: Boing, Airbus, BAE, Lockheed Martin...

      "and how much lower costs are they?"

      As long as what they do is looked after and they have no competitors they have no need to lower their costs a dime, so they don't. Maybe in the future SpaceX will change this, maybe not. Time will say.

    3. Re: Space Race! by WindBourne · · Score: 2

      Not a single one of those companies/groups are ahead of spacex. All of them require massive crews to launch their systems. Spacex requires a fraction. Why? Heavy automation. About the only thing that they 'behind' in, is the engine, and that was on purpose for low costs.

      --
      I prefer the "u" in honour as it seems to be missing these days.
    4. Re:Space Race! by Areyoukiddingme · · Score: 1

      spaceX is way ahead of the real players ... in the 1950's. SpaceX is 100% focused on extracting money from the government with gimmicks. Once required to say, actually comply with aerospace engineering practices and government contractor business processes (you know, that oversight thing) their prices will be just the same or higher (much more musk ego to pay for than boeing exec ego).

      Says the butthurt ULA employee.

      Don't worry, the welfare for mediocre engineers will continue. It's not like they were paying you for what you could do to begin with. They'll just stop having you pretend to make rockets.

    5. Re:Space Race! by WindBourne · · Score: 1

      actually, ULA has some decent engineers.
      The real problem is that they are loaded with overhead management and almost all of them are MBAs. Even now, bruno has NOT done a decent job. He simply replaced one group of fat cats with another.

      --
      I prefer the "u" in honour as it seems to be missing these days.
    6. Re:Space Race! by TWX · · Score: 1

      spaceX is way ahead of the real players ... in the 1950's.

      Given how the vision of launching, landing, and re-launching a rocket became widely popular in the fifties, and only now are we on the cusp of seeing it really work as described, that kind of makes all other expendable launch systems look like something even more retrograde than SpaceX's...

      --
      Do not look into laser with remaining eye.
    7. Re: Space Race! by Anonymous Coward · · Score: 0

      They aren't behind on the engine, either; quite the opposite in fact.

      The latest Merlin 1D "full thrust" has the highest thrust-to-weight ratio of any liquid fuelled engine that has ever flown, as far as I can tell. At 348s, it's vacuum specific impulse (fuel efficiency) is close to the theoretical maximum of ~360s for RP-1 (kerosene) powered engines. It's reusable, air-startable, and can be restarted multiple times in flight. It must also be impressively cheap to build, given SpaceX's prices.

      The *only* meaningful way in which the Merlin 1D is inferior to (some) competing engines, is its relatively poor sea level specific impulse. (This is a limitation of the engine cycle used, if I recall correctly.) This matters much less than you might think, though - for any orbital launcher, over 80% of the rocket's acceleration occurs in air thin enough that only the vacuum fuel efficiency actually matters.

      (Some people will try to claim that liquid hydrogen is a "more advanced" fuel, because of its naturally higher specific impulse. However, its very poor density and extreme temperature requirements cause a substantial part of the gains to be wasted on the heavier fuel tank required. In practice hydrolox is clearly superior only for Earth departure burns, which the commercial satellite market has little use for.)

      CAPTCHA: vacuum

    8. Re: Space Race! by WindBourne · · Score: 1

      Actually, H2 IS superior in nearly every way, EXCEPT for economics. It burns cleaner. It can be manufactured in space relatively easy. In the end, it is economics that makes it a poor choice for most issues.

      --
      I prefer the "u" in honour as it seems to be missing these days.
    9. Re:Space Race! by Anonymous Coward · · Score: 0

      I can tell you from first person perspective that we got severe congressional pressure to pencil whip SpaceX's certification. We were told that they'd get certified even if they presented blueberry pie wiped on a napkin. Further, they are not compliant with FAR required business processes and accounting processes.. They've gotten a deviance mandated from above. SpaceX is crony capitalism at it's worst, and the progressives are the loudest cheering for it.

    10. Re:Space Race! by Cochonou · · Score: 1

      You know, the rocket engineers working at SpaceX did not come out of nowhere...

    11. Re: Space Race! by cbhacking · · Score: 1

      Isn't H2, even liquefied, a lot less dense than RP-1 or even (liquid) methane? Lower density means more volume for the same mass. Sufficiently lower density that even with H2's increased efficiency (i.e. you need less mass of it) you need more volume.

      While that's irrelevant in space, it's very relevant for getting *to* space. More volume means you need a bigger rocket, with more air resistance, more metal (increasing both materials and manufacturing labor costs), more windage if you try to land it, and so on.

      --
      There's no place I could be, since I've found Serenity...
    12. Re: Space Race! by Megane · · Score: 1

      H2 is also a pain in the ass because of its "spin isomer" problem. When you cool it down enough to make it liquid, the normal ortho- form changes to the para- form with an exothermic reaction, providing enough heat to boil it back to a gas!

      --
      #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
    13. Re: Space Race! by WindBourne · · Score: 1

      sure, but again, H2 is superior in every way, EXCEPT, the economics, which is what you speak of.

      --
      I prefer the "u" in honour as it seems to be missing these days.
    14. Re: Space Race! by Anonymous Coward · · Score: 0

      1) SpaceX is a business - I considered it a given that something that is:

      superior in nearly every way, EXCEPT for economics

      is actually inferior.

      2) Density is not just about "economics" (except in the sense that everything in engineering is "economics"). Lower density fuels require larger tanks, which means heavier tanks and higher aerodynamic drag. It also increases the moment of inertial of the rocket (all else being equal), which means that more control authority is required (via a higher gimballing range or larger attitude control thrusters, either of which will increase dry mass), and more fuel must be allocating to exerting it.

      3) H2 is not meaningfully more environmentally friendly than kerosene, in practice, due to the way that H2 is typically produced, and the inefficiencies inherent in its use. It does eliminate the deposition of soot inside the engine itself, but obviously SpaceX has that problem pretty well under control since their engines have better reusability than any H2 engine ever flown.

  12. Cut the blog spam by arielCo · · Score: 3, Informative
    --
    This post contains no rudeness or derision of any kind. All arguments are friendly. Terms and exclusions may apply.
  13. Just goes to show by Anonymous Coward · · Score: 0, Funny

    America has become so cheap it has to reuse its rockets!! DAM OBAMA !!

  14. Vertical Landing Rocket Economics 101 by Marginal+Coward · · Score: 1

    I'm assuming that any rocket which lands vertically must carry twice the fuel to achieve a given altitude: one dose to accelerate to the altitude and a second dose to decelerate back to zero. This is in contrast to a space plane design like the Space Shuttle which dissipated the deceleration energy as heat and radiation. So, a vertically landing rocket would have to be much larger than its space-plane equivalent to carry the same payload to the same altitude.

    Presumably, this would counteract some of the economics of rocket reuse - though perhaps it might still be cheaper overall due to the reuse of the (twice as large?) engine. Therefore, it isn't the panacea that it would at first appear. In fact, I suspect that the reason it wasn't done in the past was primarily that the economics wasn't actually all that compelling compared to one-time-use rockets, though it is also undoubtedly technically difficult.

    Have I got all that right, or am I missing something?

    1. Re:Vertical Landing Rocket Economics 101 by Anonymous Coward · · Score: 2, Insightful

      Honestly, you got it almost completely wrong - you don't need to scale the engine at all (you rather lose some payload to orbit) - and the fuel you need to lift the rocket (full, heavy) is magnitudes higher than you need to land it back again - SpaceX uses 9 engines on the Falcon 9, and has "engine-out" capability, where one (or even two, if the right ones fail) engine can get inoperative and the rocket will compensate with a slightly longer burn to still achieve orbit. For doing so, you have to take the fuel for that "slightly longer burn" with you anyway - even if you don't need it. This very fuel will then be used for a landing burn if everything goes smoothly - the rocket either turns around (now nearly empty, and only ~20 tons) and burns toward the LZ, or follows a more or less parabolic arch to a waiting ocean barge (for high-performance launches) to land, where only the last 100m/s or so have to be killed via propulsive landing, the rest is bled of in the atmosphere (terminal velocity etc.) - we are talking about a ton or two of fuel here, which is nearly nothing compared to the rest of the rocket.

      The same goes for propulsive Landing on Dragon btw. - you have a Launch Abort System onboard which needs fuel, that you have to carry anyway - if the launch goes smoothly, you take that fuel back with you - and use it for propulsive landing (with parachute backup if something happens - you need that one for the launch escape scenario anyway).

      Hope that clarifies it a bit...

    2. Re:Vertical Landing Rocket Economics 101 by CSG_SurferDude · · Score: 4, Insightful

      It's not twice the fuel. It takes most of the fuel to get to speed. At that point the booster is SIGNIFICANTLY lighter, so it takes (again with that word) SIGNIFICANTLY LESS fuel to slow down, and then to land.

    3. Re:Vertical Landing Rocket Economics 101 by N3wsByt3 · · Score: 1

      Mostly true, but every kg that is needed to land, needs about many times as much for it to get lifted off in the first place. This is why it gets increasingly difficult to do the same for the second and third stage. (And a 'completely reusable rocket' is what Musk said he wants).

      This is not about the cost of the fuel, which is only a minor part of the costs, but, as you correctly point out, a loss of capacity for the maximum payload. To propel 1 pound of mass would require 9.39 pounds of propellant. This means, that if you need 35000 kg extra to land the thing (which is what SpaceX needs), you'll need 9 TIMES as much to get it up. That's why, if one didn't realise this, that SpaceX never lands the first stage when it has to deliver a heavy geostationary satellite in orbit: it's because they need all the fuel to get their payload up there. Ergo, the fuel they spend on it, needs more fuel to lift it, and that inveriably reduces the amount of weight of the payload they can send up. There is no way around this.

      And that is only for the first stage. The second stage - and if they want to be 'like airplanes', you'll need to recuperate all stages - is going to be much, much more difficult to recuperate. But worse, this, in turn, will need, again, extra fuel, to transport the fuel tht will be needed to land it. WORSE STILL: since now the second stage is much heavier, that weight will need to be lifted by the first stage too, so that will need even MORE fuel, which in turn will need 9 times more fuel to lift this up too. Then we come to the third stage. Rince, repeat. It needs extra fuel to land, thus it gains weight, thus the second stage needs ectra fuel, plus it needs extra fuel to lift that extra fuel, plus the third stage who has to lift all the other stages up needs extra fuel to do so, and it needs extra fuel to lift that extra fuel.

      Ergo: it gets exponentially more difficult to launch a rocket where all stages are recuperated. Or let me refrase that: it becomes exponentially more difficult for it to be economically viable, compared to a system where you'll only need a fraction of the mass to put the same payload into orbit.

      That is why, as I said in another post, there is definitely an economic point to be made to use other systems, like that of Adeline. ( http://www.space.com/29620-air... )

      Of course, that doesn't mean that 10 years from now, one already has far better systems to land the whole stages. It just means the current system (using engines/fuel) isn't probably going to cut it in the long run compared to systems that don't use this approach, economically speaking.

      --
      --- "To pee or not to pee, that is the question." ---
    4. Re:Vertical Landing Rocket Economics 101 by N3wsByt3 · · Score: 1

      My response, which is also relevant to what you say: http://science.slashdot.org/co...

      --
      --- "To pee or not to pee, that is the question." ---
    5. Re:Vertical Landing Rocket Economics 101 by fox171171 · · Score: 1

      It's not twice the fuel. It takes most of the fuel to get to speed. At that point the booster is SIGNIFICANTLY lighter, so it takes (again with that word) SIGNIFICANTLY LESS fuel to slow down, and then to land.

      True.

      However, you still have to remember that most of the fuel is used to lift the weight of the fuel.

      Take the weight of the fuel required for the landing (plus the weight of the part of the rocket that contains that fuel that had to be added).

      Now figure out how much additional fuel will be required to lift that. How much will the additional fuel (and additional rocket weight to contain the additional fuel) weigh? How much additional fuel will be required for that? And so on? And so on? It adds up.

    6. Re:Vertical Landing Rocket Economics 101 by Anonymous Coward · · Score: 0

      The second and third stage are much smaller than the first stage, so the extra fuel to land them is also much less. However, the main thing that you're not taking into account is that the fuel costs are a tiny part of the total launch costs (just a few percent) while the cost of the rocket itself is most of the cost even with disposable rockets. EVEN IF the fuel needed for an easily reusable rocket cut the payload by half, that would still drop launch costs by 10x or more. In fact not nearly as much fuel as that is needed.

      The same problem that you point out applies even more so to rocket stages that land like airplanes do like Adeline. The extra hardware to make the plane landing possible adds a lot of weight and complexity and all of that weight has to be launched with the rocket. That adds complexity and cost and that's why this obvious approach hasn't worked so well in the past. The problem is that it was not clear that landing a rocket stage safely with just its own engines was even possible for a large rocket stage, but now we know that it is after SpaceX did it. Of course it's possible that Adeline will work much better than previous attempts with that approach, so that it also becomes 10x+ cheaper, and that would certainly be great, but it's not clear that that is very likely.

    7. Re:Vertical Landing Rocket Economics 101 by currently_awake · · Score: 1

      The economics depends on what is cheaper, the fuel or the space plane. Currently the fuel is cheaper, so the Space Shuttle cost more than the Saturn 5.

    8. Re:Vertical Landing Rocket Economics 101 by gumpish · · Score: 1

      Please take a few minutes and think about how it doesn't make sense to talk about something having *less* of some property (cost, temperature, speed) as being some positive multiple of said property with regards to whatever it's being compared to.

      "A is 10 times slower than B" No. Speed is a measurable phenomenon. "Slowness" is not.

      "A is 10 times thinner than B" No. Thickness is what is measured. "Thinness" was invented by marketers.

      "A is 10 times colder than B" No. A's temperature is 1/10th B's temperature.

    9. Re:Vertical Landing Rocket Economics 101 by Dog-Cow · · Score: 1

      Please take a few minutes to learn about English. Details such as the fact that it's a living language which contains phrasings that are not mathematically correct, but are never-the-less comprehensible to those that aren't pedantic bags of shit.

    10. Re:Vertical Landing Rocket Economics 101 by N3wsByt3 · · Score: 1

      FOR FUCK SAKE! Do you even read what was written?!

      You say now:

      "However, the main thing that you're not taking into account is that the fuel costs are a tiny part of the total launch costs (just a few percent) "

      While I said in my original post:

      "This is not about the cost of the fuel, which is only a minor part of the costs, but, as you correctly point out, a loss of capacity for the maximum payload."

      WHAT did you not understand? It's NOT about the cost of the fuel. I've EXPLICITLY said that, and yet you glance over that and STILL use that false counter-argument. In essence, saying the same thing as me, but wrongly asuming it was part of my argumentation.

      And thus: no, it doesn't mean the same for systems like Adeline. Did you even bother to read the link? Adeline is estimated to need 2000 kg of fuel, SpaceX needs 35000 kg. The wings only marginally make it more heavy, just as the wings/rods of SpaceX or Shepard. Ego: it still means the first stage is a multitude times more heavy with spaceX. And it's the weight that counts, since the cost is the ratio of useful weight (aka, payload) vs total cost to send it somewhere.

      In the long run, whether they want to recuperate the whole stage or not, they'll need another system then the engine/fuel-burning one they have now.

      --
      --- "To pee or not to pee, that is the question." ---
    11. Re:Vertical Landing Rocket Economics 101 by N3wsByt3 · · Score: 1

      Sigh. No, it's not.

      I don't know why so few people grasp this.

      It's NOT about the cost of the fuel itself; that's only a minor part. What IS of importance, is, that any additional fuel for landing means additional weight, which cuts back on the maximum amount of payload you can get up in a given orbit.

      The spaceshuttle was extremely complex and needed far more maintenance than expected, and THAT was the reason it wasn't economically viable. If your refurbishing costs are about as much as building a new one, than obviously, you don't make a good economic case.

      But for any given rocket (returning stage) vs spaceplane (or system like Adeline) where the refurbishing costs are similar, the spaceplane/adeline system will ALWAYS be economically more advantageous. Simply for the fact it doesn't need the fuel to land (nor the 9.23 as much fuel to lift that fuel up), and thus, for the same type of rocket/power, you can get MORE payload into the same orbit.

      --
      --- "To pee or not to pee, that is the question." ---
    12. Re:Vertical Landing Rocket Economics 101 by Megane · · Score: 1

      Even more so when you *cough* launch an actual second stage to orbit *cough*.

      --
      #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
  15. Re: Obvious by oobayly · · Score: 2

    That's because BO had the luxury of being able to hover as desired, pick the landing spot and descend. The first landing had it skating all over the place.

    The Falcon 9's single merlin engine produces too much thrust to hover, so it has to burn to hit 0m/s at 0ft. This is due to it needing the engines to lift an actual payload into orbit, as opposed to simply going up and down.

    BO also had the luxury of choosing their launch time and location without commercial constraints. The F9 launch had a 30 second window, so to delay because of the fog (which Musk alluded to causing the ice buildup) wasn't an option.

  16. reusability: economic case? by N3wsByt3 · · Score: 1

    I said this before with the SpaceX story not long ago (and got some pretty nasty responses by fanboys), but the question remains whether IN THE SHORT RUN and *only comparing the current whole-1ste-booster stage return versus partial systems* like Adeline ( http://www.space.com/29620-air... ) or that of the ULA don't make more *economic* sense.

    Do note the domain where I'm talking about (capital letters/ asterix). I'm NOT comparing a "rocket that is like an airplane" (costwise) with a one-time usable rocket.

    Now, I'm looking pretty favourable at newcomers like SpaceX and Blue Origins, and I think it's great what those companies do, and their CEO's are visionaries imho. But still, that doesn't mean one should be blind to other things. One can say it's because the others are 'getting behind' and try to dish a potential threat, but I think it's more than that. I might be they have a point, especially for rockets that have to get into an orbit. It's exponentially difficult to get the second and third stage to be 'recoverable' as well, and, certainly with the current system of using the engines (and thus fuel), it doesn't seem viable in an economic sense, compared to Adeline-esque systems.

    NOT because of the cost of the fuel, as so many think I'm arguing (but which is a relative minor cost), but because it reduces the maximum payload. It's all there in the link, so please read *before* giving ignorant replies, thank you.

    --
    --- "To pee or not to pee, that is the question." ---
    1. Re:reusability: economic case? by stevelinton · · Score: 1

      Falcon 9 is actually just a two stage rocket, so the second stage ends up in orbit. Recovering it would mean using fuel to deorbit and having a heat shield capable of withstanding reentry. Even just recovering the engine would be a pretty major operation.

      If you wanted to avoid wasting this element then lifting it a little higher into a stable orbit (perhaps via an ion drive tug) and then making use of it for something there would make more sense.

    2. Re:reusability: economic case? by N3wsByt3 · · Score: 1

      Mayhaps. But after a while, when 10, 20, 100 stages are up there, what would you use it for? I'm not certain there is such a big market for booster parts. Not on themselves. And if you put a payload them, it just gets more expensive and heavy.

      Anyway, I don't think you can keep the current method (burning of fuel by engines) and still be economical viable in the long run, compared to alternative systems.

      Even if - in fact, especially when- we're talking about the second stage, there is need for such an alternative system. They have to figure out something which makes use of the atmosphere: parachutes that can withstand hyperspeeds, or inflatable heatshields, or wings that can withstand extreme heat, etc. So that the weight/lift ratio gets better.

      How impressive it may be, and even if it's an economic advantage compared to one-time-usable rockets, I don't think this system will be economical viable to systems that don't use this kind of engine/fuel related re-entry method.

      --
      --- "To pee or not to pee, that is the question." ---
  17. slashot vs blue origin vs space x by 140Mandak262Jamuna · · Score: 2
    Space X landed a 55000 lb LEO payload capable rocket vertically once

    Blue origin landed a suborbital rocket twice!

    Slashdot thinks Flew and Few are one and the same.

    --
    sed -e 's/Chuck Norris/Rajnikant/g' joke > fact
  18. Well, go on then! by Threni · · Score: 2

    Fix the fucking glaring typo, you barrel of twats. And while you're at it, fix the mobile bug where I get told I have 5 moderator points which expire 5 days ago. And why am I never logged in automatically like on other sites? To look at it, you'd think this was someone's first site circa 1995.

  19. um, both good, and non-overlapping by Anonymous Coward · · Score: 0

    Blue Origin is planning to go orbital at some point but is currently on the Von-Braun's V-2, Virgin Galactic, model of (mostly) straight-up and then straight-down. They are mastering the launch, land, re-use model with the aim of short-term revenue from "space tourism". Meanwhile, they are also working on the ability to do a larger rocket capable of the huge horizontal velocity required for orbit. Eventually, they will master all the required tech and be flying payloads to orbit on a re-usable orbital launch vehicle. Nobody is paying Blue to do this, so they are moving in the logical way beginning with small steps and gradually stretching their legs in the direction their business model takes them.

    SpaceX also initially did suborbital flights and re-use experiments with a modified Falcon 1st stage called the "grasshopper" and while they HAVE re-landed an launch vehicle first stage from an orbital launch (a much harder task) they have done it with a lot of money from federal government contracts and have not yet re-flown one. SpaceX will certainly master the tech and will be flying payloads to orbit on a re-usable orbital launch vehicle. Remember: SpaceX had government contacts, and therefore a HUGE incentive, to keep moving on the orbital flights fitting-in re-use experiments along the way.

    Blue is right to be proud of what they have done. Musks's grasshopper never flew more than several thousand feet and never with a payload. Blue launched a payload (a capsule designed to hold passengers) into space (though NOT into LEO) on both flights. Neither company is duplicating the other's work and the "firsts" from both should be celebrated. In the end, it looks like we will get to highly-competent and capable competitors in the marketplace and they are going to end-up fueling the eventual congressional inquiries into why the traditional defense contractors never tried to innovate to lower their launch prices (congress will pretend, like Rick in the Casino to be "shocked" that their "cost plus" DoD launch contracts meant decades of incentives to NOT innovate).

  20. Error by Anonymous Coward · · Score: 0

    There was another first, which you missed and which DC-X never attempted:

    Jeff Bezos's team [1] deployed a payload [2] into space. You are right about #2 just being about altitude, since his current launcher cannot push anything to orbital velocity, but you missed #1. That altitude is very significant, just ask any model rocket builder about the difference between his Estes-powered cardboard tube and something that goes up 100km. There are all sorts of static and dynamic structural and control issues that arise when you need to scale-up enough to haul the fuel and oxidizers required to reach those altitudes. The payload, however, is even bigger and something you missed. Bezos launched and re-launched the spacecraft too. As it is, right now, Bezos COULD sell brief suborbital flights providing a couple minutes of weightlessness for automated manufacturing experiments etc in one of his capsules, and right now he might well be ahead of Virgin Galactic in letting tourists repeat the Al Shepard suborbital flight.

    well done, Blue Origin.

  21. that few in November what? by Anonymous Coward · · Score: 0

    that few in November cared about?

  22. What % of Blue Origin was new parts on 2nd flight? by EricTheO · · Score: 0

    I wonder what the service and Q&A was like on Blue Origin after the first flight? How many components needed repair or replacement? That is why Space X is taking care with it's first reflight after successful return landing. I'm sure they learned much from their first success.

    --
    -Eric
  23. Re:What % of Blue Origin was new parts on 2nd flig by tbq · · Score: 1

    I wonder what the service and Q&A was like on Blue Origin after the first flight? How many components needed repair or replacement? That is why Space X is taking care with it's first reflight after successful return landing. I'm sure they learned much from their first success.

    According to the Blue Origin site, "Data from the November mission matched our preflight predictions closely, which made preparations for today’s re-flight relatively straightforward. The team replaced the crew capsule parachutes, replaced the pyro igniters, conducted functional and avionics checkouts, and made several software improvements, including a noteworthy one."

  24. Back and forth by jlv · · Score: 1

    November 2015: "Now safely tucked away at our launch site in West Texas is the rarest of beasts—a used rocket,” said Jeff Bezos.
    December 2015: Elon to Jeff: "Mine is bigger than yours"
    January 2016: Jeff to Elon: "I can get mine up again, can you?"