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Russia Abandons Super-Rocket Designed To Compete With SLS

schwit1 writes Russia has decided to abandon an expensive attempt to build an SLS-like super-rocket and will instead focus on incremental development of its smaller but less costly Angara rocket. "Facing significant budgetary pressures, the Russian space agency, Roscosmos, has indefinitely postponed its ambitious effort to develop a super-heavy rocket to rival NASA's next-generation Space Launch System, SLS. Instead, Russia will focus on radical upgrades of its brand-new but smaller Angara-5 rocket which had its inaugural flight in Dec. 2014, the agency's Scientific and Technical Council, NTS, decided on Thursday, March 12." For Russia's space industry, it appears that these budgetary pressures have been a blessing in disguise. Rather than waste billions on an inefficient rocket for which there is no commercial demand — as NASA is doing with SLS (under orders from a wasteful Congress) — they will instead work on further upgrades of Angara, much like SpaceX has done with its Falcon family of rockets. This will cost far less, is very efficient, and provides them a better chance to compete for commercial launches that can help pay for it all. And best of all, it offers them the least costly path to future interplanetary missions, which means they might actually be able to make those missions happen. To quote the article again: "By switching upper stages of the existing Angara from kerosene to the more potent hydrogen fuel, engineers might be able to boost the rocket's payload from current 25 tons to 35 tons for missions to the low Earth orbit. According to Roscosmos, Angara-A5V could be used for piloted missions to the vicinity of the Moon and to its surface." In a sense, the race is now on between Angara-A5V and Falcon Heavy.

179 comments

  1. That's what happens by mozumder · · Score: 1, Insightful

    when your President steals $200 billion from your country's treasure and steals it for himself.

    Sucks to be you, Russia!

    1. Re:That's what happens by Anonymous Coward · · Score: 0

      Are you talking about Russia or US? must be Russia as currently politicians have stolen far more in the US.

    2. Re:That's what happens by khallow · · Score: 3, Informative

      He's talking about a single person, Putin not the whole nest of thieves. That's 10% of Russia's annual GDP. The equivalent in the US would be Obama making off with $1.6 trillion in assets just by himself.

    3. Re:That's what happens by Anonymous Coward · · Score: 0

      I agree with your statement, but, alas, ours has effectively thrown $8 trillion out the window... The SLS is gonna be put on the credit card, which sucks too..

    4. Re:That's what happens by blue+trane · · Score: 1

      You're dreaming. In the US, the Fed creates money to backstop banks, and contrary to quantity theory of money predictions, inflation decreases and the dollar gains strength. Now the Fed should create money and transfer it directly to individuals.

    5. Re:That's what happens by blue+trane · · Score: 2

      But the Fed is the issuer, and returns interest to the Treasury. Hence, zero cost funding.

    6. Re:That's what happens by Anonymous Coward · · Score: 0

      when your President steals $200 billion from your country's treasure and steals it for himself.

      Sucks to be you, Russia!

      I wish ours *only* stole $200billion, instead we wound up $trillions in the hole to the bankers. Although I hear some of the banks might be having layoffs, so there's a good chance a few dozen congress-critters might be out of a job once BOA, JPM, Citi, and GS eliminate them from their payrolls? Sounds like a plan anyways, if they're gonna be using my hard earned tax dollars to buy our politicians, at least they can hire competent ones rather than the current crew.

    7. Re:That's what happens by WGFCrafty · · Score: 1

      Maybe in a far more subtle manner...

      An analogy would be if Obama privatized the USPS and then split it up into companies he essentially gives to his friends turning them all into billionaires.

    8. Re:That's what happens by cheesybagel · · Score: 1

      That is only happening because the printed dollars aren't filtering down the market. If they did you would get inflation.

    9. Re:That's what happens by currently_awake · · Score: 1

      Prices have risen steadily the last year, also known as inflation. The government has a good reason not to admit to that though so don't expect to hear about it in the news.

    10. Re:That's what happens by cheesybagel · · Score: 1

      Well this year they can rely on the oil price drop to camouflage the effect.

  2. the Space Age is over by Anonymous Coward · · Score: 0

    Everybody back to beating each other over the head with clubs. Fight over scraps, stupid hairless monkeys. Don't forget to die on your pitiful lump of rock!

    1. Re:the Space Age is over by khallow · · Score: 1

      How can you have cavemen in space without the BFR?

    2. Re:the Space Age is over by Anonymous Coward · · Score: 1

      With all the posts available to comment on, you chose to post one of your own only so you could go on a rant. Seriously, you have issues. Big issues. You even bring up space nutter stuff on non-space related topics and threads only so you can rant. Get some help. You're losing your grip on reality. Sooner or later you'll be thinking about your "Day of Retribution" and then go on a (mostly failed) killing spree.

    3. Re:the Space Age is over by Anonymous Coward · · Score: 0

      This troll is very weak poop.

    4. Re:the Space Age is over by Tablizer · · Score: 1

      Fight over scraps, stupid hairless monkeys

      Hey, I am not hairless, Gorn!

    5. Re:the Space Age is over by Anonymous Coward · · Score: 0

      Right, so the guy who talks about us beating each other over the head with clubs, and dying on "this rock", because someone isn't launching a rocket, he's not the one with problems.

      I am.

      Gotcha.

    6. Re:the Space Age is over by Anonymous Coward · · Score: 0

      Bitter much bro?

    7. Re:the Space Age is over by ColdWetDog · · Score: 1

      You will be. You will be.

      --
      Faster! Faster! Faster would be better!
    8. Re: the Space Age is over by Anonymous Coward · · Score: 0

      No, you are because YOU posted the original and THEN replied. Schizophrenia is a known disorder. Get help. Now.

  3. size matters by Anonymous Coward · · Score: 0

    fuck that, bigger is better

    roscosmos consumes 35 tons of grain alcohol weekly

  4. hydrogen not an improvement. by Anonymous Coward · · Score: 5, Informative

    SpaceX found that hydrogen fuel is not an improvement over methane when you include all the extra complexity (and weight) of dealing with super cold and very small atoms, both resulting in brittle metals. SpaceX does intend to switch to methane, which is a small improvement over kerosene, and unlike kerosene does not leave difficult to clean residue in pipes and engine parts.

    1. Re:hydrogen not an improvement. by K.+S.+Kyosuke · · Score: 3, Interesting

      Hydrogen, even used chemically, could be quite useful (especially with detonation based rockets (constant volume combustion)) for large interplanetary spacecrafts once you have them in orbit. But NOT until we have them. For a launch vehicle? That doesn't make much sense. The tankage size and T/W requirements (pumping power proportional to pV!) speak against it.

      --
      Ezekiel 23:20
    2. Re:hydrogen not an improvement. by taiwanjohn · · Score: 4, Interesting

      At about 10m15s in this press conference, Elon calls hydrogen a "pernicious molecule" while fielding a question about fuel cells. He also mentions some other drawbacks, such as its being odorless and invisible (so you can't smell when it's leaking), and it's extremely flammable... and burns with an invisible flame.

      Hydrogen is very efficient as a rocket fuel, which is why it's used. But liquid methane is pretty good too, and has a lot fewer "issues" to deal with.

      --
      XML is like violence. If it doesn't solve your problem, you're not using enough of it. --AC
    3. Re:hydrogen not an improvement. by ShanghaiBill · · Score: 1

      Hydrogen, even used chemically, could be quite useful (especially with detonation based rockets (constant volume combustion)) for large interplanetary spacecrafts once you have them in orbit.

      Once you are in orbit, wouldn't it make more sense to use an ion engine?

    4. Re:hydrogen not an improvement. by K.+S.+Kyosuke · · Score: 1

      It depends on what for. Trans-Martian injection of a crewed vehicle (especially a large one), for example, would be problematic with an ion engine. How much time would you want to spend in the radiation belts? ;-)

      --
      Ezekiel 23:20
    5. Re:hydrogen not an improvement. by Megane · · Score: 1

      Sure, if you don't mind waiting for it to get there. For a manned mission, probably not so much.

      --
      #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
    6. Re:hydrogen not an improvement. by Anonymous Coward · · Score: 0

      As long as it takes to generate some fantastic mutations with bendy arms and ability go naked among the Martian public, unseen.

  5. Re:And in the US by khallow · · Score: 2

    we get to launch rockets without having to have a profit requirement for it!

    You say that as if it were an advantage. Interesting.

    That's why the US gets to launch big expensive, and awesome science projects like Hubble, Cassini, Voyager, Apollo, etc.., while Russia is stuck with shitty Space-X sized rockets that only has commercial appeal.

    NASA doesn't currently have a way, aside from the commercial launchers, to launch those various probes you mentioned. NASA doesn't even have the capability to launch crew to the International Space Station.

  6. MOAR BOOSTERS! by jordanjay29 · · Score: 2, Informative

    I love how the Russian "SLS" version had four boosters. Someone over there must play Kerbal Space Program.

    1. Re:MOAR BOOSTERS! by Anonymous Coward · · Score: 0

      Is it two or four? http://www.newyorkdick.org/storage/Aides_2.jpg

    2. Re:MOAR BOOSTERS! by K.+S.+Kyosuke · · Score: 3, Informative

      Energia flew two times with four side-mounted kerosene boosters and it worked. Angara A5 also has four of them. Atlas V regularly has up to five large SRBs. There's no problem with that.

      --
      Ezekiel 23:20
    3. Re:MOAR BOOSTERS! by Anonymous Coward · · Score: 0

      but the N1, on the other hand...

      "The first stage, Block A, was powered by 30 NK-15 engines arranged in two rings, the main ring of 24 at the outer edge of the booster and the core propulsion system consisting of the inner 6 engines at about half diameter."

      BOOOOOOOOOOOOOOOOOOOOOOOOOOM!

    4. Re:MOAR BOOSTERS! by K.+S.+Kyosuke · · Score: 1

      It was a monoblock rocket. How is that relevant to launchers involving parallel staging?

      --
      Ezekiel 23:20
  7. Cheaper to steal SLS design by Anonymous Coward · · Score: 0

    just watch.

  8. Re:And in the US by blue+trane · · Score: 4, Interesting

    The government should not be run for profit. The government should be an alternative to markets, provide a safe haven for those who want to do things because they're interested in advancing knowledge, not selling something. Space exploration is in the General Welfare, not only for the 1%.

  9. Translation by DerekLyons · · Score: 1

    Translation: "Russia can't even afford the power points for it's super heavy booster, so it's going to concentrate on the development of an unproven booster that budget crunches have already delayed for over two decades."

    1. Re:Translation by hairyfeet · · Score: 4, Insightful

      Well considering that we wasted a couple decades on a "space truck" that actually met NONE of its original goals, not weight carrying, not turn around, and not cost per load, and was designed more for passing pork than anything else (just like the new one, which is why so much shuttle shit is included despite the boosters being what killed Challenger) while the Soviets were able to build the most dependable rocket family in history with Soyuz?

      Frankly I give them better odds than I do the USA as it seems the only projects NASA has been able to get done has been the ones that are small enough Senator Porkus and Congressman Bribaton haven't gotten a whiff of. With the amount of money being shat into SLS? It will end up with each widget being built in a different state (and some states having a widget per district) so you end up with a bloated whale that when it comes together will probably leak like a sieve and be only good for blasting money into space.

      --
      ACs don't waste your time replying, your posts are never seen by me.
    2. Re:Translation by nojayuk · · Score: 4, Interesting

      The "space truck" was actually a complete space station. It had living space for seven people, airlocks for EVAs, a shower and a toilet as well as having 20 tonnes of cargo space in the back of the "truck" and a payload arm/manipulator.

      The Shuttle had considerable cross-range capability once in orbit with up to 18 tonnes of manoeuvering fuel (twice the total payload of a current Falcon 9) and could stay in orbit for up to a month if needed with a reduced crew. It did most of the heavy lifting of the construction of the ISS in orbit and carried out multiple Hubble repair and upgrade missions. At the end it came back down to Earth and landed on a runway.

      The Dragon capsule is purely for canned monkeys with no toilet, no shower, no airlocks and no EVA capability. It has no cargo capacity, no manipulator arm, limited cross-range capacity in orbit and limited endurance and it certainly can't be used to carry out maintenance flights to the Hubble or its successors.

    3. Re:Translation by K.+S.+Kyosuke · · Score: 2

      Soyuz is dependable because it's simple and because it's old. Today it's reasonably cheap (especially the Soyuz-U modification) because it paid itself off a very, VERY long time ago (although even with Russian labor prices, the old design is probably more expensive than would be strictly necessary with modern manufacturing). But even Soyuz also had something like fifty or sixty launch failures in the first two decades before the kinks got ironed out. The Shuttle cost more, but at least it didn't need that. In addition, the Russian attempt at cloning the Shuttle design (ultimately with some modifications) did basically the same thing as the Shuttle - wasted a lot of money, basically almost bankrupting the Soviet Union (some people postulate that it may have directly contributed to the dissolution of the Soviet Union), although without actually achieving anything meaningful (besides the RD-170 design that got used on the Zenit and eventually mutated into the RD-180 engines on the Atlas V). So with the Shuttle, for all its deficiencies, you got at least something for your money (ISS, Hubble, etc. etc.) instead of breaking up the country.

      --
      Ezekiel 23:20
    4. Re:Translation by K.+S.+Kyosuke · · Score: 1

      And you're saying that even this additional capability was worth extra $1B per flight? I beg to differ. The idea that you couldn't achieve the things you named without a one-size-fits-all vehicle is preposterous.

      --
      Ezekiel 23:20
    5. Re:Translation by K.+S.+Kyosuke · · Score: 1

      BTW, the Dragon could almost certainly do maintenance on the Hubble. And quite probably more easily in many respects. For starters, it wouldn't be forced to lift 80 tonnes of dead mass above the lowest LEO levels that Shuttle had to fly in to achieve reasonable payload. So it wouldn't need anywhere near 18 tonnes of fuel to do the same. And Falcon 9 has 13 tonnes of payload capacity to LEO, not 9. (Plus I'm also reasonably certain that Shuttle's OMS fuel load was limited by payload - that you couldn't have both full fuel load and considerable cargo, but that probably wouldn't hamper most servicing missions.)

      --
      Ezekiel 23:20
    6. Re:Translation by nojayuk · · Score: 1

      How much would it cost to build and launch an 50-tonne "workshop" spacecraft to do the Shuttle's job and then ditch it into the upper atmosphere after every flight? A lot more than a billion a flight, never mind the extra launch of a manned capsule to dock with the Space Workshop module.

      A recoverable and reusable spacecraft with the capabilities to do the same job as the Shuttle would need heat-tiling, some aerodynamic appendages to control re-entry and oh look! it's a Space Shuttle!

      Saying that the Shuttle concept was laid out in the days when scheduling launches and docking in space was not as refined as it is today so the workshop was integrated with a manned "capsule" and living space and everything went up in one stack. One use (about the only repeated use I can think of in fact) for Falcon Heavy would be to launch a unmanned son-of-Shuttle "workshop" which would be recoverable to autoland on a runway for refurbishment and repurposing after spending a few months in orbit being visited by Soyuz/Dragon/SLS crews.

      At the moment Dragon's only intended purpose is ferrying crews to the ISS but the space station is wearing out and its days are numbered. Once it is decommissioned then what? Dragon can only put meatbags in space, it can't do anything else unless there's somewhere for them to work and live. The Shuttle was an inelegant solution to that problem but it worked for 133 and a half flights. Sure it cost a lot but spaceflight generally costs a lot, thousands of bucks per kilo into LEO.

    7. Re:Translation by nojayuk · · Score: 3, Informative

      The Dragon has no airlocks, no space (heh) for spacesuits, no external cargo capacity in the service module (although they're working on it) to carry spare parts, no manipulator arm to tether and position EVA personnel around the Hubble or other large space infrastructure item like, say, an ISS Mark 2. It's a minimal spam-in-a-can meatbag-to-orbit delivery system, not a lineman's truck with a cabover as the Shuttle was.

      The Shuttle's OMS fuel load could be maxed out to 18 tonnes if lots of in-orbit manoeuvering was planned at the cost of a reduced payload bay manifest. Most flights it didn't carry that much fuel but it didn't need to be rebuilt to take max fuel/oxidiser if the next flight necessitated it. Any Dragon plus disposable workshop mission is going to cost more and take longer as each workshop will have to be built and individually tailored to the expected mission's requirements. The other option is to build a son-of-Shuttle recoverable workshop/living quarters spacecraft, a bit like the autolanding X-37, but I don't see any budget for that anywhere.

    8. Re:Translation by thrich81 · · Score: 4, Interesting

      The Shuttle never lived up to what it was sold as -- cheap, reliable access to space. The most damning evidence of that is that the only major sponsor/user besides NASA, the US Air Force, abandoned it as soon as its actual operational limitations became clear. The Air Force went to the expense of developing new large expendable launch vehicles rather than try to stick with the Shuttle. For the last few years the Shuttle had only one mission -- support the ISS, every other mission had been taken from it. And, the US had a perfectly viable space station program without the Shuttle -- Skylab, and for that matter, so did the Russians. Speaking of the Russians -- they figured out pretty quickly that the Space Shuttle concept was operationally a loser and abandoned their Buran version after one flight. So, the Shuttle looked good in the marketing slides from the 70's and early '80s, but has to be judged an operational failure by the standards set for its justifications to be built. The Shuttle could do things that no other vehicle can do, but those capabilities, such as its huge cross range landing capability, just turned out to be not very useful and not worth the cost.

    9. Re:Translation by K.+S.+Kyosuke · · Score: 1

      How much would it cost to build and launch an 50-tonne "workshop" spacecraft to do the Shuttle's job and then ditch it into the upper atmosphere after every flight?

      Why would you need such a thing, especially "on every flight"? Even Salyuts were under 20 tonnes, and that was with hard (and rather rugged) structure and with all amenities. I suspect that with Bigelow's inflatable modules, you could cut that down almost by half, even when still keeping such things as robotic arms etc. Most of the mass of the Shuttle is the airframe, thermal protection, ten tonnes of engines, and the payload bay. There's absolutely no reason to haul it into orbit every time. It cost the US space program over 6000 tonnes of payload that could have been delivered to space instead. Are you saying that Dragon would have to haul (even if just for satellite servicing missions) a thirty-ton airlock and a twenty-ton robotic arm? I don't think these things are being made of lead...

      Saying that the Shuttle concept was laid out in the days when scheduling launches and docking in space was not as refined as it is today so the workshop was integrated with a manned "capsule" and living space and everything went up in one stack.

      No, the Shuttle concept was laid out as a rather plain crewed vehicle, until the DoD stepped in saying that they want to steal Russian satellites. That is the reason why the Shuttle had a lot of expensive capabilities that ended up vastly underutilized.

      At the moment Dragon's only intended purpose is ferrying crews to the ISS

      No, it really isn't. :D

      --
      Ezekiel 23:20
    10. Re:Translation by Anonymous Coward · · Score: 0

      The reason "space truck" was in scare quotes is that the Shuttle was intended to be like a truck - simple, reliable, transporting cargo efficiently and safely - but ended up as something completely different. As you point out, the Shuttle was effectively a completely space station - which had to be launched back into orbit every time it was used, making it horrendously expensive compared to the disposable rockets for which it was supposed to be a cheaper replacement.

      95% of what the Shuttle did could have been done better and cheaper by a combination of a permanent space station and canned-monkey capsules like the Dragon, both launched with old-fashioned stacked rockets. The exception, which you mentioned, is the Hubble repair and upgrade missions - but the Hubble successor, the James Webb Space Telescope, will be positioned at the Sun-Earth Lagrange-2 point, far out of reach of a Shuttle mission, so this justification is slipping away, too.

    11. Re:Translation by K.+S.+Kyosuke · · Score: 2, Interesting

      The Dragon doesn't need any of those things. Its purpose is to take a few people into orbit and back and not to weigh too much in the process of doing so. The idea to put the things you mention onto something that has to be launched every time at a significant cost, and equipped with increased reentry facilities (which also have to be launched) to return all those things afterwards is preposterous. Shuttle's half-tonne arm alone has subtracted almost 60 tonnes of total payload from all the Shuttle flights (an equivalent of $3B). And the reason why you don't see the budget for anything beyond the Shuttle was formerly the effing Shuttle and now is the efffing SLS. The Shuttle completely killed most of the research in that particular area for decades. Today, the SLS is killing research in anything beyond refurbishing the Shuttle infrastructure. Smart move indeed!

      --
      Ezekiel 23:20
    12. Re:Translation by Megane · · Score: 1

      To be completely fair, it wasn't the SRBs that killed Challenger, it was the side-mounted configuration that killed both Challenger and Columbia.

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

      Every Shuttle flight needed spacewalks, the cargo bay, the spacelab, the manipulator or other features sadly lacking in a people-only spacecraft like the Dragon until the ISS was ready for habitation. The ISS couldn't have been built without the Shuttle though, not without a (non-existent at the time) SLS that could throw a complete space station or large ready-to-go part of it with spacesuit airlock(s), manipulator arm, power systems etc. into orbit in one launch. Even then a "fork-lift truck" spacecraft like the Shuttle would probably have been needed to move shit around as more parts arrived in orbit -- the ISS is over 400 tonnes as is, nothing larger than about 16 tonnes in one piece.

      Either a workshop/fork-lift spacecraft would have been recoverable to Earth as the Shuttle was or it would have been disposed of into the upper atmosphere and a new one built, furbished and launched every time a new task needed to be accomplished. The Shuttle was there to do that job, repeatedly.

      Sure the Shuttle never succeeded in what it was originally designed for, nor was its launch tempo (50 launches a year was mooted at one time!), costs or other factors met. It did the job though when the ISS was built and when it was laid out in the early 70s nobody knew the ISS was going to exist at all. There's lots of Monday-morning quarterbacking about how things should have been but having the Shuttle to hand made things a lot easier when it was needed.

    14. Re:Translation by nojayuk · · Score: 2

      "The Dragon doesn't need any of those things. Its purpose is to take a few people into orbit and back"

      Where are they going to go when they get to orbit? The ISS won't be there after 2020 or so. Bigelow is a lot of hot air. The Russian ISS-remnant will be serviced by Soyuz. So what's left for Dragon/Falcon apart from space tourism?

      The Dragon alone can't build an ISS Mark 2 or even a Mars Expeditionary vehicle, it needs a workshop vehicle/microstation to dock to for the crew to do anything significant in orbit (and have a shower, use the toilet etc.). That's what the Shuttle was, as well as being the crew vehicle. A Falcon Heavy could launch such an unmanned microstation but they cost a lot of bucks so having it recoverable to be refurbished and reused would be a good idea. A heatshield re-entry system to splashdown on something that large would be cumbersome so tiles or another lightweight heat protection system on a lifting-body or winged vehicle would be preferable, like the X-37 or the new ESA re-entry testbed article flown recently on a Vega. Thus is the Shuttle reinvented, better and shinier than before with the lessons of the past learned.

    15. Re:Translation by K.+S.+Kyosuke · · Score: 2

      Every Shuttle flight needed spacewalks

      Wrong.

      , the cargo bay,

      The thing is that one shouldn't be forced to haul large payloads with such a useless reusable vehicle in the first place. So some cargo capacity is certainly desirable but not for 300 m^3 and 24 tonnes. Even the lousy large launchers we already have are much more economical for such things.

      the spacelab,

      A thing like that could have stayed in the orbit.

      the manipulator

      A thing like that could have stayed in the orbit, too.

      The ISS couldn't have been built without the Shuttle though, not without a (non-existent at the time) SLS that could throw a complete space station or large ready-to-go part of it with spacesuit airlock(s), manipulator arm, power systems etc. into orbit in one launch.

      Mir was assembled without the Shuttle. Granted, even with the additional modules, it was smaller, but it could have been assembled into a much larger station if something like Canadarm2 had been available at that time. The core of the Mir was exactly the kind of "a complete space station" you describe, and it even though Russian-built, it weighed so little that the Proton was able to launch it. (And I'm pretty sure that today, we would be able to do an even better job than what Russians did twenty years ago.)

      Even then a "fork-lift truck" spacecraft like the Shuttle would probably have been needed to move shit around as more parts arrived in orbit -- the ISS is over 400 tonnes as is, nothing larger than about 16 tonnes in one piece. Either a workshop/fork-lift spacecraft would have been recoverable to Earth as the Shuttle was or it would have been disposed of into the upper atmosphere and a new one built, furbished and launched every time a new task needed to be accomplished.

      Why would you dispose of it? Is there a rational need for that?

      Sure the Shuttle never succeeded in what it was originally designed for, nor was its launch tempo (50 launches a year was mooted at one time!), costs or other factors met.

      I think the "kills astronauts every fifty flights or so" part would have become quite problematic if such a high launch cadence had been ever achieved. The same goes for the cost which never allowed for the flight rate anyway. Nobody really needed extra people in space just to launch satellites, and the expenses associated with it. So satellites stopped being launched on the Shuttle. I can't say I'm surprised by all that...

      It did the job though when the ISS was built

      Because nothing else was avaiable. Nothing else was available because the Shuttle sucked out all the money.

      There's lots of Monday-morning quarterbacking about how things should have been but having the Shuttle to hand made things a lot easier when it was needed.

      The Air Force backed out of the Shuttle on Saturday, not on Monday.

      --
      Ezekiel 23:20
    16. Re:Translation by Anonymous Coward · · Score: 0

      Lugging a "complete space station" into orbit only to bring the whole thing back in two weeks is dumb. That could have been payload.

      Lugging giant wings and a tail and landing gear into orbit when you could have brought a parachute instead is dumb. That could have been payload.

    17. Re:Translation by nojayuk · · Score: 1

      Adding landing legs to the first stage and not using all the fuel in the tanks, that could have been payload. Wait, what?

    18. Re:Translation by ColdWetDog · · Score: 1

      No, it was the stupid PR people and managers that insisted on launching it when every fucking engineer associated with the launch told them otherwise. If they would have waited for everything to warm up, the Challenger would likely have had a normal launch.

      Likewise, had NASA management effectively killed engineering plans to deal with ice damage the Columbia disaster might well have been averted. Certainly, space flight is risky and the Shuttle overly complex and prone to breaking down, but the proximate cause of both disasters was management, not engineering.

      --
      Faster! Faster! Faster would be better!
    19. Re:Translation by khallow · · Score: 1

      How much would it cost to build and launch an 50-tonne "workshop" spacecraft to do the Shuttle's job and then ditch it into the upper atmosphere after every flight? A lot more than a billion a flight, never mind the extra launch of a manned capsule to dock with the Space Workshop module

      Why do that when you can launch 10-20 ton chunks into orbit and do all your "workshop" stuff on a permanent space station? For example, instead of developing the near useless Space Shuttle, NASA could have launched and assembled the ISS with the Saturn 1B back in the early 80s.

      And looking at your further post on the subject, it's not that hard to launch a teleoperated mechanic arm or two for moving and mating components of the station.

      Also, you claim the ISS wasn't even on the drawing board back in the 70s. That is incorrect. That stuff was planned from back in the 60s. NASA allowed its budget to get sucked into another big rocket rather than focus on building space infrastructure that could have actually been useful.

      A recoverable and reusable spacecraft with the capabilities to do the same job as the Shuttle would need heat-tiling, some aerodynamic appendages to control re-entry and oh look! it's a Space Shuttle!

      Not at all. A fluffier vehicle (with less density per cross-sectional area) would have less heat load at reentry and could make do with a titanium or other more mundane heat shields.

      At the moment Dragon's only intended purpose is ferrying crews to the ISS but the space station is wearing out and its days are numbered. Once it is decommissioned then what? Dragon can only put meatbags in space, it can't do anything else unless there's somewhere for them to work and live. The Shuttle was an inelegant solution to that problem but it worked for 133 and a half flights. Sure it cost a lot but spaceflight generally costs a lot, thousands of bucks per kilo into LEO.

      Falcon 9 can put up another ISS. And that's not even counting the Falcon Heavy, which can throw massive payloads to space (though it doesn't quite have the fairing size of the Space Shuttle payload bay). I would go with inflatable modules and the Falcon Heavy.

    20. Re:Translation by WGFCrafty · · Score: 1

      I think you and me have VERY different definitions of what a shower is.

      "But on the International Space Station and NASA shuttles, astronauts have a squirt gun that shoots water and a wash cloth. They also have a special rinse-less shampoo to keep their hair clean."
      http://www.space.com/7060-slee...

    21. Re:Translation by WGFCrafty · · Score: 1

      Note: I wasn't saying that your definition is wrong, just I wouldn't quite refer to such a device as a shower.

    22. Re:Translation by K.+S.+Kyosuke · · Score: 1

      Where are they going to go when they get to orbit? The ISS won't be there after 2020 or so

      I think you meant 2024?

      Bigelow is a lot of hot air.

      Here's your first lot of hot air :-), already having been packaged for delivery to the ISS, probably in September.

      The Russian ISS-remnant will be serviced by Soyuz.

      What "ISS remnant"? There most likely won't be any such "remnant". Russians don't have money to even finish their planned modules and to launch them, much less to refurbish an already expired set of modules in orbit. Zarya will be 30 years old by 2024, but it is American property now. Zvezda's structural frame dates back to 1985! It will be almost 40 years old by 2024... Nauka - which hasn't even launched yet! - is as old as Zarya, and they already have had to repair it at least once. Alas, they don't have money, even for those repairs... It was supposed to have launched in 2007(!). It now seems that it could launch in 2017...provided that before that date, they manage to replace its major propulsion system that's already out of warranty. If it doesn't happen, I won't be surprised.

      BTW, I found it supremely amusing that despite your incessant Shuttle eulogies, you don't even for a second doubt the Russians' ability to build and maintain a new space station even if they don't have any of your precious Shuttles with a robotic arm, airlock, and your beloved camping toilet to do it. :-p

      The Dragon alone can't build an ISS Mark 2 or even a Mars Expeditionary vehicle

      Why would a Dragon need to "build" anything? What's wrong with you? You seem to have this fixed idea that every manned vehicle needs to contain everything conceivable that you could possibly bolt onto it. That has never been the case.

      A Falcon Heavy could launch such an unmanned microstation but they cost a lot of bucks so having it recoverable to be refurbished and reused would be a good idea.

      First, if something weighs fifty tons, it's not a "microstation" in anyone's book, especially if it will use modern technology. Tiangong-1 is a "microstation". BA-330 or anything similar...not so much. Second, it could easily be reused without being hauled down to Earth's surface and back every time. Salyuts had no problem with this mode of operation. Plus, your "recovering" and relaunching would cost a lot of bucks, too. So you propose to replace wasting a lot of bucks with wasting a different lot of bucks. How is that reasonable?

      A heatshield re-entry system to splashdown on something that large would be cumbersome so tiles or another lightweight heat protection system on a lifting-body or winged vehicle would be preferable, like the X-37 or the new ESA re-entry testbed article flown recently on a Vega. Thus is the Shuttle reinvented, better and shinier than before with the lessons of the past learned.

      Your obsession with reentry vehicles of all kinds and sizes continues. Go see a psychologist or a psychiatrist to help you with that problem. I'm apparently an inadequate counselor on these matters.

      --
      Ezekiel 23:20
    23. Re:Translation by K.+S.+Kyosuke · · Score: 1

      Except that accelerating, decelerating and landing extra 1 kg of mass to/from 1.5-2.5 km/s (F9-R/FH-R first stage) is much easier and less costly that doing the same at 9.5 km/s of characteristic velocity (the STS orbiter). In fact, by something like a factor of five to ten or so. But by this point in time, I suspect that lessons in numeracy are lost on you anyway.

      --
      Ezekiel 23:20
    24. Re:Translation by Anonymous Coward · · Score: 0

      This is full of inaccuracies. 18,000 pounds is not 18 tonnes. The Dragon capsule most certainly has cargo capacity.

      The shuttle was all one unit. It couldn't be significantly reconfigured for different missions. The Dragon is the crew capsule of a modular system.

      One thing they can do with the Dragon is extend the trunk and put it on top of a Falcon Heavy. Then they can send it up with at least half-again the cargo of the shuttle. Or they can put it on the Heavy with no cargo and send it to orbit the moon. Or they can send it up on top of a "complete space station" with EVA capability, and have the capsule separate, turn around, and dock with it, like the Apollo capsule did.

      The Falcon/Dragon modular system can do anything the shuttle did, at far lower cost.

      Or when you don't need crew, you can just use the Falcon or Falcon Heavy, to economically send huge payloads to LEO, or substantial payloads to geostationary orbit or beyond Earth orbit. Try that with the space shuttle.

      The modular approach is much better, especially the SpaceX execution of it.

    25. Re:Translation by Anonymous Coward · · Score: 0

      Oh, no: the Space Transportation System (STS, aka Space Shuttle) did exactly what it was designed to do: launch the Keyhole class of intelligence satellites from a space platform that could change orbits after launch to hide the satellite's orbit as long as possible.

      NASA was out of money. NASA faced extinction. NASA went to the DOD and begged for a task. DOD gave them the dimensions and weight for something they wanted lofted into orbit. NASA built the shuttle around a cargo bay that met those specifications.

      The specifications were for the KH class of electro-optical reconnaissance satellites.

      That's why the shuttle got built. Anything else was gravy.

    26. Re:Translation by cheesybagel · · Score: 1

      At the moment Dragon's only intended purpose is ferrying crews to the ISS

      Google "DragonLab".

    27. Re:Translation by cheesybagel · · Score: 1

      You can easily put an airlock in a capsule. Soyuz has one as does Shenzhou (orbital module). The manipulator could have been attached into the first space station core launched into orbit using a regular launch vehicle like a Delta IV Heavy. Delta IV Heavy has more payload than the Proton rocket which was used to launch the Mir modules and the Russian ISS segment. If, for whatever reason, you actually needed a mobile construction yard you could just launch a space tug into space and use that instead of wasting time and fuel getting it up and down all the time.

      The Shuttle was a jack of all trades master of none vehicle. It is a pathological case of design by committee. NASA wanted an RLV, the DoD wanted the capability to launch and recover huge earth reconnaissance satellites, DoD wanted wide cross-range capability. These requirements don't mix well so the resulting vehicle was an abortion. Kind of like the JSF.

    28. Re: Translation by Anonymous Coward · · Score: 0

      you forget the capability to snatch your own sats after a couple of years. that is important for many sar r and d reasons. especially when your sats fly low enough for the atmosphere to have effects.

    29. Re:Translation by cheesybagel · · Score: 2

      They also decided that they didn't have the money to make the first stage design reusable so they tacked together a fuel tank with a couple of solid rocket boosters to do the same job. Then they gave the task of building the solid rocket boosters to ATK. The worst of both design choices. Why? So the pork could be spread to Utah as well. Then Challenger happened.

    30. Re:Translation by cheesybagel · · Score: 1

      For all we know the Russians could build their next space station together with the Chinese.

    31. Re:Translation by cheesybagel · · Score: 1

      The same engine design is also be basis for the RD-191 rocket engine used in Angara.

    32. Re:Translation by K.+S.+Kyosuke · · Score: 1

      It looks like Chinese economy is growing in such a way that around 2025-2030, Russians could be "second-class contributors" to a Russian-Chinese station in exactly the same way as they are now on the ISS. But I'm not sure how they would stomach something like that...

      --
      Ezekiel 23:20
    33. Re:Translation by K.+S.+Kyosuke · · Score: 1

      It is ironic that the losing design proposal for Angara - one that proposed using RD-180 in the core stages - lost, among other things, for the reason of RD-180 not existing at that time. The objection was that developing a new engine would cost a lot of money - despite the fact that the RD-180 is something like a 70%-identical version of RD-170! (Identical combustion chambers, scaled-down pump.) I think it speaks volumes that all these "new" Russian engines are modifications and derivatives of the original major design work on the RD-170, which took something like a decade or so around 1980 when the Soviets still had something remotely resembling lots of money. And of course, the winning design that counted on simply reusing RD-170 was scrapped anyway and the current design uses a different derivative that also had to be developed and paid for...but by that time, Americans have already fully funded the RD-180 that could have powered the originally proposed launcher! History is funny sometimes...

      --
      Ezekiel 23:20
    34. Re:Translation by currently_awake · · Score: 1

      Turning the Dragon launcher into a satellite launcher is easy. It's mostly just taking stuff out from the manned launcher and covering what's left with a launch shroud. As for the space shuttle, we'd have been better off just keeping the Saturn 5 launcher. It had a heavier payload, more reliable, and the design was paid for. Even if we had to launch 2 to get the men in orbit it would still have been cheaper and safer.

    35. Re:Translation by shutdown+-p+now · · Score: 1

      There is no evidence that abandonment of Buran had anything to do with its practicality. A far more likely explanation, given the dates, is that it was all about the country being in a financial shithole where it simply couldn't afford the program.

    36. Re:Translation by cheesybagel · · Score: 1

      Yeah but as it turns out Orbital will be using some modified version of the RD-191 on the Antares because the NK-33 went kaput. Also be Russians claim they are selling the RD-180s below cost.

    37. Re:Translation by K.+S.+Kyosuke · · Score: 1

      They were selling below the cost for some time. Right now, the price tag is $23.4M per one RD-180 unit for ULA, out of which $20.2M goes to Russia. This is also an interesting number, since we were discussing the Angara above: If $20M+ were the cost (equal to or higher than the price, if the Russians are actually right about the price dumping thing) of two chambers and a turbopump, how much should the engines for Angara, with five chambers and five (somewhat smaller) turbopumps cost? $50M+ would appear to be the case if price per turbopump kW were fixed, but I find it likely that a greater number of smaller turbopumps is somewhat more expensive - after all, it's more components to manufacture, assemble, and test. And the turbopumps are definitely a significant portion of the cost. Let's say $55M-$60M? But that's just the five engines. Now you also have to manufacture the five cores, the second stage, its own engine, the cryogenic stage, its own engine, and control systems for all that. (Not to mention that two fuel systems on the pad - one of them deeply cryogenic - are quite certainly going to be more expensive to run.) All that while keeping in mind that Proton people basically say they can launch a Proton for you for less than $70M.. So if the RD-170-lineage engines are so expensive, despite having been in large-scale serial production for at least the last 15 years, how is Angara supposed to end up cheaper than the Proton?

      --
      Ezekiel 23:20
    38. Re:Translation by stoatwblr · · Score: 1

      "The most damning evidence of that is that the only major sponsor/user besides NASA, the US Air Force, abandoned it as soon as its actual operational limitations became clear."

      Which took a shitload of chuntzpah, given that it was USAF demands for crossrange abilities which put the huge wings on the thing and made it so big it had to be bolted to the side of a tank instead of sitting safely at the top of the stack.

      Shuttle was a camel (in the sense of "a horse designed by committee") and ended up spending most of its life in search of a reason for existence - other than the obvious "national prestige" flagwaving one.

      As a "space truck" it didn't need those enormous wings and as a USAF single orbit spysat launcher it lost a _lot_ of payload capacity for space truck operations.

    39. Re:Translation by stoatwblr · · Score: 1

      > Here's your first lot of hot air :-) [nasa.gov], already having been packaged for delivery to the ISS, probably in September.

      That's the third one. The first 2 were free-flying testbeds which are still in orbit.

      https://en.wikipedia.org/wiki/...
      https://en.wikipedia.org/wiki/...

    40. Re:Translation by stoatwblr · · Score: 1

      Or it could be Russia, the EU and China, with India and Brazil joining later.

      The only country dead-set against working with China in space is the USA.

    41. Re:Translation by cheesybagel · · Score: 1

      You can easily reduce production costs by using mass-production. With larger production runs it becomes more cost effective to automate certain production processes. Lower unit production often also implies manufacturing in small batches, with more production you can change to an assembly line kind of production facility. You can also bulk buy materials with large production runs.

      RD-170 family engines have had a much smaller production run than the RD-275. Also that article you linked to claims they currently charge more than $100 million a Proton flight.

      The hypergolic propellant cost is probably a lot more expensive and it is not easier to handle than cryogenics.

      I don't expect the cost of Angara to be low in the beginning.

    42. Re:Translation by K.+S.+Kyosuke · · Score: 1

      Except they've already produced over 400 combustion chambers of the RD-17x/18x type and countless turbines. You'd think they're pretty far along the learning curve of the existing design already. Obviously, better manufacturing techniques are always desirable, but I doubt that they'll be able to achieve that without a redesign. SpaceX, for example, had made some serious changes between the 1C and 1D versions of their engines, specifically targeted at manufacturing speed and costs. It ended up being a completely different engine. Whether Russians actually have enough money to redesign a much more complicated engine of their own to save money in the future remains to be seen. They haven't bothered to do that in 15 years of RD-180 deliveries.

      The fact that Proton operators charge $100M+ only means that they're in it for the money. It doesn't say that they're barely scraping by. They explicitly mentioned in that article that they can go much lower, but with the current demand, it doesn't make sense to go for artificially low prices - you're killing your profits. And Russian rocket companies managed to accumulate some serious debts in the past, so they desperately need the current high prices to stay high even if their costs are much lower.

      --
      Ezekiel 23:20
    43. Re:Translation by cheesybagel · · Score: 1

      The main difference between Merlin 1C and 1D was that they switched from a tube wall nozzle to a channel wall nozzle. The Russians have been using channel wall nozzle since the 1960s unlike the US. So the Russian engines already optimized like that.

      We should be able to compare the prices better once Orbital Antares gets the RD-181 and SpaceX has the Raptor working.

    44. Re:Translation by Megane · · Score: 1

      If there had been no side-mounted configuration, there would have been no disaster, whether or not the O-rings failed, or ice fell off of the ET. The basic design of the Shuttle stack prevented any form of crew escape, period, and it also subjected the crew vehicle to damage from the launch vehicle. Fortunately we're going back to capsules on top that can perform an emergency escape from the launch vehicle. It's not as sexy as an OMG SPACE PLANE but that was more trouble than it was worth.

      --
      #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
  10. Re:Vodka fueled Niggers by Anonymous Coward · · Score: 0

    Just finished Ukraine, blasting into Russia now.

  11. Propaganda much? by cyn1c77 · · Score: 3, Insightful

    Wow... Was the summary written by Putin? (Hello Mods: The author is even Russian!)

    There may be no current commercial need for the SLS, but you can bet that it will appear once the system launches successfully a few times.

    Also, I'm sure the US military and NASA will be excited to be able to launch heavier and heaver things into space and stop being reliant on Russian launch technology, especially with the Russians dusting off their 1950's era bombers to test NATO defenses.

    1. Re:Propaganda much? by K.+S.+Kyosuke · · Score: 5, Insightful

      There may be no current commercial need for the SLS, but you can bet that it will appear once the system launches successfully a few times.

      At a total cost of way over $1B per flight (unless it flies more than once or twice per year, which is highly unlikely), you can be sure that even the 130 mt version of SLS will be in much smaller demand than a $100M semi-reusable Falcon Heavy with a ~40 mt capacity, or even the expendable ~$150M, ~55 mt version.

      --
      Ezekiel 23:20
    2. Re:Propaganda much? by SuricouRaven · · Score: 1

      I'm not sure exactly what commercial uses there are for really heavy launches. Comms and science do not need to be so large. Only thing I can think of is a space hotel, and that's not going to be commercially viable unless you can bring the human launch cost down far enough for the moderately rich to afford a holiday there, rather than just the obscenely rich. There aren't enough billionaires around to constitute a sufficient market.

    3. Re:Propaganda much? by Anonymous Coward · · Score: 0

      Yeah, because your propaganda is better when padded with speculations and wishful thinking.

    4. Re:Propaganda much? by K.+S.+Kyosuke · · Score: 5, Insightful

      I'm not sure exactly what commercial uses there are for really heavy launches.

      Economy of scale? But that's only worthwhile as long as the heavier launcher won't hit low launch frequencies and unsustainable infrastructure costs. Which is definitely the problem that the SLS will hit.

      Comms and science do not need to be so large

      Circular logic. Right, they don't need to be so large because we've learned to make them smaller...and we've learned to make them smaller because we had no choice, large rockets were prohibitively expensive. But that doesn't mean that, e.g., science couldn't use more capable vehicles. Science can always use more capable vehicles. Missions could be much easier with them (or even possible in the first place), and a cheaper larger launcher could make even the mission itself cheaper (besides launch costs).

      Galileo would have gotten to Jupiter almost four years faster with Centaur-G instead of the less-capable solid stage it was forced to use. That meant extra four years of running (and paying) the mission team without results, and also four years less of hardware lifetime once the probe got to its destination. The Mars Science Laboratory wouldn't have had to use a working but convoluted and custom-designed landing system. In a few years, a payload of this size (or even somewhat larger) would simply use a "marsified" Dragon-derived lander with no parachute and just a longer segment of propulsive landing. It might weigh almost twice as much, but who cares?

      You could use serially manufactured components instead of custom designs if you weren't forced to shave every kilogram.

      --
      Ezekiel 23:20
    5. Re:Propaganda much? by SuricouRaven · · Score: 1

      I should have clarified that I was limiting the discussion to commercial uses. Commercial science means things like weather monitoring and resource surveys - things you do in LEO. There's absolutely nothing beyond geostationary that pays for itsself - that's why those missions you mention all had to be paid for with someone's tax money.

    6. Re:Propaganda much? by Kjella · · Score: 1

      There may be no current commercial need for the SLS, but you can bet that it will appear once the system launches successfully a few times.

      The difference compared to the Apollo days is that now we have a lot of experience building modules and docking them in orbit to form the ISS. The biggest single piece we've sent up there so far is the S3/S4 truss at 16,183 kg. Falcon Heavy will do 53,000 kg. SLS will do up to 130,000 kg. The total launch mass of the ISS is 417,289 kg, so even with the SLS it's not enough to launch as big structures as we might like. Most plans for a human mission to Mars seem to involve many SLS launches to assemble a ship in LEO, NASA's latest "design reference mission" called for seven launches at 130 tons = 910 tons total.

      Alternatively that could be 18 launches of the Falcon Heavy, assuming no module needs to be bigger than 53 tons. For comparison the four RS-25s powering the SLS first stage only weighs about 3.5 tons each for a total of 14 tons, the bulk is fuel. Fuel you can bring up in as small quantities as makes economic sense. My guess is that 53 tons dry weight is plenty. They only publish a standard cost these days not a full weight launch but it used to be $135m, let's say $150m and that we need 20 launches. For $3 billion you have your launch capability.

      What's missing is really all the rest, a Mars transfer vehicle, lander, habitat with supplies and power, launch vehicle, return craft and splashdown capsule. It's possible the Dragon can be expanded and adapted but it's made for short hops to the ISS, not living quarters for months. But we're also getting a little bit ahead of ourselves because the Falcon Heavy hasn't flown yet. I think that around 2020 with five years of launches behind us we'll wonder WTF did we build the SLS and maybe ask SpaceX to add another few boosters for a superheavy but we're not ready to do that just yet. I'm guessing the SLS will be the last rocket NASA will build though.

      --
      Live today, because you never know what tomorrow brings
    7. Re:Propaganda much? by K.+S.+Kyosuke · · Score: 1

      Even commercial satellites in LEO, MEO or GEO could significantly benefit from a cheap heavy launcher: a, say, ten-fold decrease in launch costs would not only decrease launch costs themselves but it would also shift optimum spacecraft design mass to higher levels, which would mean either more capability per unit of mass (for example, larger communication satellites are more economical due to more transponders sharing the same bus), less constrained (conservative and heavier but cheaper) engineering, or both.

      --
      Ezekiel 23:20
    8. Re:Propaganda much? by khallow · · Score: 1

      There may be no current commercial need for the SLS, but you can bet that it will appear once the system launches successfully a few times.

      Even if that were really true (it weren't for the Space Shuttle, which got payloads by forcing everyone to launch on the Space Shuttle through to 1985 or so), you still have the problem that a few successful launches puts you somewhere past 2030. That's at least 15 years of fucking around.

      Also, I'm sure the US military and NASA will be excited to be able to launch heavier and heaver things into space and stop being reliant on Russian launch technology, especially with the Russians dusting off their 1950's era bombers to test NATO defenses.

      The SLS has to successful fly first. NASA's last success construction of a launch vehicle was the Space Shuttle Endeavor which was delivered to NASA on 1991 and first launched a year later. Since the Space Shuttle has been under development, there has been a long string of failed launch vehicles: DC-X, X-33, X-37, and Ares I.

      There's a history of failure here. When you also consider that SpaceX is likely to fly its Falcon Heavy in the next year, which can put 50 metric tons into orbit, and probably could develop a straight up SLS competitor for two years of the spending that NASA has chucked so far at SLS (and a timeline of say, five years), I think the SLS will be obsolete before it ever launches, assuming it ever does.

    9. Re:Propaganda much? by Anonymous Coward · · Score: 1

      Actually, science missions, especially to the outer solar system and beyond, could benefit from a really big rocket. The SLS can either push a big thing into LEO, or push a little thing out of Earth really fast. New Horizons was launched on a pretty hefty rocket (Atlas V 551, 18 tons to LEO -- with five solid-rocket boosters, how's that for MOAR BOOSTERS?) and flew past the Moon in 9 hours (vs. 3 days for Apollo to get there -- though to be fair, Apollo was going to orbit around the Moon, so getting there any faster would require more fuel for the capture burn), and will still take 11 years to get to Pluto.

      So, with the SLS, science missions can be bigger and/or get to their destinations faster, which is good for reduced radiation exposure (thus more reliability), more time to use RTGs in their "prime" years, reduced life support system needs (for crewed missions)...shame NASA probably won't get the budget to launch enough of them to get the costs down by economies of scale, but what can you do?

    10. Re:Propaganda much? by Megane · · Score: 1

      And that's why it's a good thing that FH will be using the same parts as F9, only with a few struts added. Don't need heavy launches? Simply don't strut it together, and make three regular launches!

      But don't limit your thinking to what we do now with what we have now. Just like with oil reserves increasing as the price of oil goes up (due to cost of recovery), the things people will want to launch rockets for will increase as the cost of launches goes down. And likewise, as the cost of heavy launches comes down, people will start building bigger stuff (or stacking multiple payloads) to make use of it.

      --
      #naabhaprzrag, #sverubfr-000, #agi-fcbafberq, negvpyr[pynff*=' negvpyr-ary-'] { qvfcynl: abar !vzcbegnag; }
    11. Re:Propaganda much? by Neowolf2 · · Score: 1

      Most of the benefit of heavy launchers can be obtained by in-orbit mating of parts launched on smaller launchers, and most importantly in-orbit propellant transfer. "Tank farms" in orbit containing oxygen and hydrogen (or methane) would be a real game changer for getting to the Moon and beyond, particularly if they can be refilled with propellants processed from ET sources (lunar polar ice, for example). The one thing SLS could sell itself for would be large unitary payloads, for example heat shields for landing on Mars. But I strongly suspect the problem of assembling a large heat shield in space from smaller segments could be solved.

    12. Re:Propaganda much? by K.+S.+Kyosuke · · Score: 1

      I don't question the value of orbital assembly, or the use of tugs etc. It's just that "too small" launchers are going to have uneconomical operations, just like "too small" modules where size is valued (pressurized compartments, for example). We need to find the right size, whatever it turns out to be, but I'm pretty sure it's not below 20 tonnes to LEO.

      --
      Ezekiel 23:20
    13. Re:Propaganda much? by Neowolf2 · · Score: 2

      It depends on flight rate. If your vehicle is going to fly just once a year (or less), it's too big.

    14. Re:Propaganda much? by K.+S.+Kyosuke · · Score: 1

      My guess is that 53 tons dry weight is plenty. They only publish a standard cost these days not a full weight launch but it used to be $135m, let's say $150m and that we need 20 launches. For $3 billion you have your launch capability.

      Even the semi-reusable version ought to be even better for fuel in terms of $/kg for bulk transport. I think one could reasonably expect a 45+ tonne capability (15% payload decrease) for about $90M (say, -40% cost) - that's perhaps even conservative. Fuel flights also have the benefit of being largely risk-insensitive and fungible, thus being prime candidates for flying reused stages. If something goes wrong, you'll be sending another fuel flight from the payload queue soon anyway.

      --
      Ezekiel 23:20
    15. Re:Propaganda much? by Anonymous Coward · · Score: 0

      There's never going to be a commercialneed for SLS itself. It's a project designed to meet NASA's perceived manned spaceflight needs, strictly as a government R&D project. The design elements are dictated as much by political requirements as it is NASA's requirements. Estimates are running $1B per launch; it will be too expensive for commercial applications. If Boeing or SpaceX can find customers demanding >120mT payload to orbit (maybe even NASA or DOD), then they could conceivably build an economical vehicle, if allowed to do it their way without all the political interference.

    16. Re:Propaganda much? by cheesybagel · · Score: 1

      Yeah no kidding. The SLS is supposed to fly once every two years.

    17. Re:Propaganda much? by K.+S.+Kyosuke · · Score: 1

      Well, I was speaking more of FH-class launchers than the SLS. An SLS-like launcher would be unaffordable anyway even if smaller simply because it uses seriously expensive components such as the RS-25 (expendable!) and the RL-10.

      --
      Ezekiel 23:20
  12. Chunkatize to Commoditize. by Tablizer · · Score: 1

    waste billions on an inefficient rocket for which there is no commercial demand -- as NASA is doing with SLS (under orders from a wasteful Congress)

    Putin is indeed cocky, but our Congress takes the cake.

    Why do we have to launch big loads all at once? Launch a booster first, and then have the payload rendezvous with it in orbit. It may take some R&D and practice to get right, but it seems the more logical way to handle big projects instead of supporting bigass rockets and launch platforms that are not used enough to pay their rent.

    Plus, having a spare in place is easier with commodity rockets.

    1. Re:Chunkatize to Commoditize. by Anonymous Coward · · Score: 0

      Why do we have to launch big loads all at once?

      Because we're (rah rah!) the USA and we have to have the biggest phallic symbol that can shoot the biggest loads all at once, or we're going to feel inferior. We don't care how much it costs as long as we can show off that ours is the biggest and best.

    2. Re:Chunkatize to Commoditize. by MightyYar · · Score: 1

      That does not really describe the USA anymore. Most of us don't pin too much nationalist pride on things like the tallest this or the longest that anymore. Hell, we didn't even bother maintaining a manned space program.

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
  13. Re:And in the US by K.+S.+Kyosuke · · Score: 4, Informative

    while Russia is stuck with shitty Space-X sized rockets that only has commercial appeal.

    Russia regularly launches Proton-M, which has a Shuttle-like LEO payload capability. With the exception of Apollo, it should have been able to launch any of those things, and at a much lower cost. The problem for the Russians is that they hoped that Angara would be cheaper than the Proton-M. In retrospect, achieving that turns out to be quite problematic. Angara's saving grace is that it is - yet again - a military rocket, and unlike Energia, it's a military rocket for which they have no replacement (at least not after the Proton gets retired). It could have commercial appeal, but if Falcon Heavy works out well, which is very, very likely, few people are going to bother with Angara. Between ITAR, costs, transportation issues, general shunning of doing business with Russia these day, etc., I'm not sure there's a lot of potential. It may very well end up just launching scores of spy sats.

    --
    Ezekiel 23:20
  14. Re:And in the US by K.+S.+Kyosuke · · Score: 1

    The government should not be run for profit.

    But that's not an argument in favor of wasteful projects (when cheaper alternatives are available), I hope.

    --
    Ezekiel 23:20
  15. Re:Vodka fueled Niggers by Anonymous Coward · · Score: 0

    please blast harder.

  16. Re:And in the US by Anonymous Coward · · Score: 0

    Angara is not a military rocket.

  17. Didn't think it through did you? by dbIII · · Score: 0

    The government should keep it's dirty claws out of profit and let private enterprise work without having an 800lb gorilla breathing down it's neck. We want people who understand a market selling products, not a horse judge who happened to sleep in the same room as someone who later became a powerful government figure.
    A government's role is to act for citizens when they are taken advantage of, not to fleece them for profit with no alternative.
    See state owned power utilities regulated by the state that owns them for an example - eg. price rises of around 500% over 8 years and no alternative other than putting a solar panel on your roof.

    1. Re:Didn't think it through did you? by Daemonik · · Score: 4, Informative

      See state owned power utilities regulated by the state that owns them for an example - eg. price rises of around 500% over 8 years and no alternative other than putting a solar panel on your roof.

      As opposed to what? Private power companies that stage brownouts to drive up their own prices?

      At least state owned power utilities have to face a public board of inquiry before they can raise their rates, and the state regulates how much of their income has to go to keeping their own services repaired. Unlike telecoms letting wired phone service wither because they can make more money on cellular.

      Yeah, the private market has always been such an example of fairness and customer service. *eye roll*

    2. Re: Didn't think it through did you? by Anonymous Coward · · Score: 0

      that is egregious, which utility are you referring too?

    3. Re:Didn't think it through did you? by Anonymous Coward · · Score: 0

      Could you keep your dirty apostrophes out of possessive pronouns? Do you have any idea how dumb you look when you write "it is dirty claws", or "breathing down it is neck"?

    4. Re:Didn't think it through did you? by ShanghaiBill · · Score: 3, Interesting

      As opposed to what? Private power companies that stage brownouts to drive up their own prices?

      False dichotomy. Government monopolies and private monopolies are not the only alternatives. What seems to work best is to separate ownership of the grid (which is a natural monopoly) from power generation (which is not). Whether the grid is owned by the government or by a regulated private utility doesn't much matter. The grid owner charges a fee, which can vary with load, for transporting power from producer to consumer. But the production of power can be done by anyone that can meet the technical requirements of feeding power into the grid, including individual homeowners with extra solar power or residential micro-cogeneration.

    5. Re: Didn't think it through did you? by Anonymous Coward · · Score: 0

      Exactly! It's called network neutrality elsewhere.

    6. Re:Didn't think it through did you? by Anonymous Coward · · Score: 1

      Yes, it worked so well up Massachusetts, that 2015 winter electric rates went up by 35+%. Of course, the politicians that split the transmission and generation apart and promised lower energy rates are long retired with their generous government pensions leaving the electric utility customers holding the bag. All of those "non-monopoly" generators built gas plants and took the grid from a balanced energy source mix designed by utility engineers over the decades to one with over 50% natural gas. A number of those "non-monopoly" plants even went so far as refuse to run because their contracted gas could be sold at a higher price on the spot market. Of course, the grid operator then had to dispatch even more expense power. Unfortunately, this is a humpty-dumpty situation and what was split apart can't be put back together.

    7. Re:Didn't think it through did you? by HornWumpus · · Score: 1

      Mass and the entire NE massively under built and failed to update their grid under ratebase.

      Ratebase guarantees the utility a fixed % of return on costs. Why would they ever retire a plant under that rule set? In fact they didn't, so theory is moot.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
  18. Not for SpaceX it isn't. Others - already there. by dbIII · · Score: 1

    That's because they are a little startup without the resources to deal with such complexity and not a very large org that already has experience using that fuel.
    Yes hydrogen has many issues, like the embrittlement problem that's been known about and dealt with since the 1940s, but it's a tradeoff that some can do already but is uneconomic for others to go near.

  19. I still do not understand SLS by Anonymous Coward · · Score: 0

    What SLS can do that other rockets can't?

    I am not one who would stand in the way of progress, but no matter how I look at SLS, that thing just does not make any sense (and also cents) to me

    If anyone can convince me that SLS is indeed needed, please do ... I am all ears, ... and eyes

    1. Re:I still do not understand SLS by K.+S.+Kyosuke · · Score: 2

      What SLS can do that other rockets can't?

      It can launch more suitcases of money into the right congressional districts. ;-)

      --
      Ezekiel 23:20
    2. Re:I still do not understand SLS by Anonymous Coward · · Score: 0

      Bingo. This.

      The B1-B has at least one part made in every congressional districts of the US. That was not a mistake.

  20. Re:And in the US by taiwanjohn · · Score: 3, Interesting

    The gov't could at least lose less money if it issued its own currency (beyond just coins) instead of borrowing its money supply from privately owned banks.

    --
    XML is like violence. If it doesn't solve your problem, you're not using enough of it. --AC
  21. Re:Not for SpaceX it isn't. Others - already there by K.+S.+Kyosuke · · Score: 2

    I'd think that hydrogen is somewhat uneconomical for launch vehicles also because it generally gets used in upper stages, so you need more different pieces of launch pad infrastructure, and all-importantly, at least two types of engines. The fact that some other companies are not "little startups" still doesn't protect them from the effect of economies of scale. (And if you want to suggest unifying on hydrogen, check out the boondoggle named "Delta IV".) Look at how hideously expensive the RL-10 has ended up due to restricted production, and rejoice in the wisdom of Falcon 9 designers (which, besides unifying propulsion, gave them a landing level of thrust achievable in the first stage almost for free).

    It also doesn't help much that when hydrogen does get used in launch vehicles, those upper stages are optimized for high energy missions and therefore end up on average more expensive (because they're built to be super-lightweight) even if all you want is to get some standardized payload to LEO. I'd really reserve hydrogen for the future, purely in-space vehicles, especially the large ones (with presumably improved volume/mass ratio for the hydrogen tanks that wouldn't involve exorbitant costs to achieve in smaller tanks, giving hydrolox better economies of scale). And even that only after some important technological progress - besides vastly improved Isp of up to almost 500 s, the lower pumping pressures and potentially much greater engine lifetime could come in really handy.

    To sum it up, perhaps we're not doing those missions yet where hydrogen would actually be decisively beneficial from the economy point of view. Anywhere up to LEO, hydrocarbons win, especially with good engines, and even direct launch to GTO probably isn't a sufficient excuse.

    --
    Ezekiel 23:20
  22. Re:And in the US by CrimsonAvenger · · Score: 2

    The gov't could at least lose less money if it issued its own currency (beyond just coins) instead of borrowing its money supply from privately owned banks.

    Hmm, just printing more money as needed...

    Seems to me that's been tried a few times in history. Worked pretty well for Germany in the 1920's and -30's, as I recall....

    --

    "I do not agree with what you say, but I will defend to the death your right to say it"
  23. Re:And in the US by taiwanjohn · · Score: 1

    And the Fed's so-called "quantitative easing" is different from that... how?

    It appears that the debt-backed money system we've been using since 1971 (when Nixon closed the gold window) has run itself out to its logical conclusion: an exponential explosion of debt as we approach the vertical asymptote.

    I'm not arguing for a gold standard; a fiat system can work just fine as long as the quantity is controlled sensibly, as you imply. But I don't think that ceding the "issuing power" to private banks is a good solution either. For example, the Bank of North Dakota strikes a good balance. It doesn't issue currency per se, but it does handle all the state's revenues, and makes loans (which is essentially the same thing as issuing currency) to local banks and some other institutional borrowers. And the interest on those loans goes into ND's coffers instead of being paid to, say, Goldman Sachs.

    So, contrary to what the GP said, ND is in fact "making a profit" from all this, which is a distinct benefit to all its citizens.

    --
    XML is like violence. If it doesn't solve your problem, you're not using enough of it. --AC
  24. high module dev cost by Anonymous Coward · · Score: 0

    Skylab cost ~$2.6 billion, ~$11 billion 2015. The space station Freedom was expected to cost $8 billion in 1984, maybe $24 billion in 2015 dollars. The current cost has been over $75 billion.The ISS weighs 400 tons. The extra design, and assembly costs of modules outweigh the cost of bigger, heavier, cheaper modules, and just using a big rocket.

    1. Re:high module dev cost by K.+S.+Kyosuke · · Score: 1

      That's because the ISS modules are too small (plus, the expensive Shuttle). They're really, really tiny. However, that doesn't mean that two 50-tonne modules will be more expensive to build and launch than one 100-tonne module, if the 100-tonne module has to be launched on a launcher with absolutely no other use case than launching single 100-tonne modules (consequently ending up with insignificant launch frequency).

      --
      Ezekiel 23:20
  25. I used to be happy about... by Karmashock · · Score: 1, Insightful

    ... Russia being in space. But given their conduct, I think they should have as limited capabilities as possible.

    Russia is out of control and entirely unrepentant. If they have fewer capabilities their frequently bat shit crazy leaders will have more limited aspirations.

    --
    I've decided to stop wasting my time responding to AC trolls/sockpuppets... so if you want a response from me... login.
    1. Re:I used to be happy about... by ColdWetDog · · Score: 1

      Replace "Russia" with "humans" and I would agree with you.

      We're all assholes.

      --
      Faster! Faster! Faster would be better!
    2. Re:I used to be happy about... by Karmashock · · Score: 1

      I do not hate my own species and I encourage any member of my species that does hate its own species to dig a hole in the ground, stand in it, and then blow their own brains out. That way whomever has the ignoble duty of dealing with your corpse can do so with a minimum of effort.

      --
      I've decided to stop wasting my time responding to AC trolls/sockpuppets... so if you want a response from me... login.
    3. Re: I used to be happy about... by Anonymous Coward · · Score: 0

      You misspelled "USA". The US must be contained by all means necessary.

    4. Re: I used to be happy about... by Karmashock · · Score: 1

      In what way?

      Russia's recent actions would be like the US invading Mexico and then annexing Baja California.

      Can you cite something the US did that is in anyway like that or would you like to roll over right now and play dead?

      --
      I've decided to stop wasting my time responding to AC trolls/sockpuppets... so if you want a response from me... login.
    5. Re: I used to be happy about... by dunkelfalke · · Score: 1

      More like invading Mexico and then annexing Texas. Sounds familiar?

      --
      "It's such a fine line between stupid and clever" -- David St. Hubbins, Spinal Tap
    6. Re: I used to be happy about... by Karmashock · · Score: 1

      Did that happen recently or would you like to bring up every thing that every civilization has done in the history of ever?

      --
      I've decided to stop wasting my time responding to AC trolls/sockpuppets... so if you want a response from me... login.
    7. Re: I used to be happy about... by dunkelfalke · · Score: 1

      Well, some people aren't goldfish.

      --
      "It's such a fine line between stupid and clever" -- David St. Hubbins, Spinal Tap
    8. Re: I used to be happy about... by Karmashock · · Score: 1

      Well okay then you're going to have to judge everything that any nation has ever done ever against everything any other nation has ever done ever.

      You want to play that game? Because you're still not going to win that way.

      What you're trying to do is cherry pick your context by comparing all the sins of one country against a country that is so weak that it couldn't do something evil even if it wanted to... and then you're probably going to only allow very recent comparisions in their case while at the same time comparing that same little country against a big powerful country's entire record.

      That's not having a memory... that's just false equivilency. Its a logical fallacy.

      Aka your argument isn't benefiting from memory or a knowledge of history but from a lack of rational thought. And absent that, your position lacks credibility.

      So... the goldfish comment is nonsense.

      If you want to have a rational discussion on it then you're going to have to compare apples to apples.

      Define your context. The rules by which various things are examined. Once those rules are stated, you can then populate the argument with facts and examples that meet those pre stated criteria.

      I am asking you to do this because I think you need some help when it comes to forming a logical argument. If you just knew these rules inherently and obeyed them that would be one thing. But your goldfish comment makes it very clear that you don't.

      I don't say this with any intention of offending you. But it is literally impossible to have a rational discussion with you unless you form rational arguments. And rational means logical and logical means not contradicting yourself, changing the rules for data arbitrarily, engaging in circular logic, or relying on any argument that assumes if X must = Y when there is no substantiating evidence to support that position.

      --
      I've decided to stop wasting my time responding to AC trolls/sockpuppets... so if you want a response from me... login.
    9. Re:I used to be happy about... by Anonymous Coward · · Score: 0

      I'm not an asshole

      you asshole!

  26. Legacy of Sergei Kololev by DrTJ · · Score: 3, Interesting

    This "four booter rocket" configuration is not new to the russians. It was introduced by Sergei Korlev http://en.wikipedia.org/wiki/S... already in the 50:s, with the R7 line of rockets http://en.wikipedia.org/wiki/R... . In fact, it was one such R7 carrier rocket (8K71PS) that launched Sputnik-1 (and -2) into orbit. The detachment of the booster rockts were such a common sight, that it got its own name: Korolev cross https://www.google.se/search?q....

  27. Re:And in the US by khallow · · Score: 2

    The government should not be run for profit.

    Profit is a strong indication that you are generating more value than you cost. If you aren't generating a profit, there should be a good reason why. You don't provide such a reason. Let's look in more detail.

    The government should be an alternative to markets, provide a safe haven for those who want to do things because they're interested in advancing knowledge, not selling something.

    First of all, no. There's no "should" here. Second, who gets this safe haven and who doesn't? We can't have everyone sucking up money just because they're more interested in advancing knowledge than in the alternatives. Someone has to generate that tax revenue in order for the scheme to work.

    Then there's the matter of unintended consequences. If you put up this scheme, then someone will game it for profit. In practice, there's no real yardstick for what "advancing knowledge" means, so it's been long exploited by universities and businesses.

    Space exploration is in the General Welfare, not only for the 1%.

    One near universal problem that NASA has long contended with is that space exploration is just not that valuable to the US public. I don't mean just perceived to be not that valuable - public perception has always been lukewarm towards space activities. But truly not that valuable. It doesn't materially change the human condition to know a little more about our universe. And the vague intangibles which NASA supposedly brings, like inspiration to go into the STEM fields, could be achieved for a fraction of the cost by Earth-bound activities.

    Finally, NASA is just terrible at its assigned role. It might not need to be profitable, but it certainly needs to be getting an order of magnitude more activity and exploration out of the money it currently spends.

  28. Re:And in the US by rasmusbr · · Score: 2

    The government needs a frame in which it can legally operate. For instance you don't want the government to get into iron mining, steel making and knife making just so it can run hospitals. It's fine for a government-run hospital to buy surgical knives from private companies.

    The horror example where this separation from government subsidies never happened is the airline industry, where you have two giant corporations, Boeing and Airbus, that leech billions off of various governments.

  29. Re:Not for SpaceX it isn't. Others - already there by rasmusbr · · Score: 2

    Yes, but in addition to that the trade-offs are inherently different for re-usable rockets. Embrittlement is probably a pretty big problem if you intend to re-use your fuel tank many times, like SpaceX intends to.

    If SpaceX fails to make their second stage re-usable I would not be surprised to see them switch to hydrogen for that stage at some point down the line.

  30. Now if we could only kill SLS by Dereck1701 · · Score: 2

    I have to agree with the summary, this could be a blessing in disguise for the Russians given the right future economic conditions. We're burning enough money here in the US just on DEVELOPMENT of SLS that we could launch the mass of a WWII aircraft carrier into orbit on commercial launchers in todays launch market let alone the economies of scale you would get if we tried to do so. And the "$500 Million" per launch claim that NASA is putting out is hysterical, It will probably cost at least $1.5 Billion per launch not including development. If our intention is to make space access more reasonable there simply is no good reason for a SHLV at this time, we can do everything and more with standard LV's and if we get enough yearly flights economies of scale and competition will kick in and help space access costs even more. SHLVs are currently only good for shoveling massive amounts of money into the bank accounts of a few well connected defense contractors.

  31. Re:And in the US by ShanghaiBill · · Score: 3, Insightful

    And the Fed's so-called "quantitative easing" is different from that... how?

    It is different because the Fed is independent, and not subjected to short term political pressure.

  32. Might I suggest... by Anonymous Coward · · Score: 0

    a large trampoline instead?

  33. Article surreptitiously pushes an agenda by caballew · · Score: 1

    For Russia's space industry, it appears that these budgetary pressures have been a blessing in disguise. Rather than waste billions on an inefficient rocket for which there is no commercial demand — as NASA is doing with SLS (under orders from a wasteful Congress)

    samzenpus is using this article to present his opinions as facts while completely ignoring the valid reasons for building the SLS. The SLS is not going to be used for launching communication satellites or taking tourists to space. SLS is not a commercial project but a scientific and exploratory project to enable mankind to escape low earth orbit while preserving the U.S. space launch capabilities.

    1. Re:Article surreptitiously pushes an agenda by K.+S.+Kyosuke · · Score: 0

      I think you mistyped "while preserving the jobs of the former STS workforce"... It's not like the US wouldn't have space launch capabilities without the SLS, now is it? (Also, there's nothing scientific about the SLS project itself. It's a transport vehicle. All the science for its components was done in the 1970s. The best thing you could say now is that it's an engineering project.)

      --
      Ezekiel 23:20
  34. Re:And in the US by taiwanjohn · · Score: 3, Interesting

    LOL!! The Fed may be independent of gov't but it's not independent of corporate plutocracy. Indeed, this is the crucial struggle of our times, wresting control of our politics and our economy from these fat-cat SOBs.

    Get thee hence to Wolf-PAC.com and pitch in to help save our democracy from these blood-suckers.

    --
    XML is like violence. If it doesn't solve your problem, you're not using enough of it. --AC
  35. Re:Budgetary Pressures by WGFCrafty · · Score: 1

    It may be flamebait, but that doesn't make it any less true.

    I say we clone Soyuz 11 and give Putin a ride!

  36. Re:And in the US by WGFCrafty · · Score: 4, Insightful

    I forget which scientist was asked by a general if it had "military use, if it could protect America?" and he replied "no, but it will make America worth protecting."

    This is the reason we should do things. Not for profit, for material gain, for defense, or any other flimsy reason. It should be done because it is beneficial to us all, because it advances us all as humans.

  37. Re:Budgetary Pressures by theshowmecanuck · · Score: 0

    My mistake was to post that at night just before the Russians were waking up. They don't like to hear the truth about their dictator.

    --
    -- I ignore anonymous replies to my comments and postings.
  38. Wrong Again by DerekLyons · · Score: 1

    while the Soviets were able to build the most dependable rocket family in history with Soyuz?

    More dependable than anyone else - by about .2%, much celebrated by the clueless, irrelevant in the real world.

    1. Re:Wrong Again by cheesybagel · · Score: 1

      At least Soyuz is still around. And will be for the foreseeable future.

  39. Re:And in the US by cheesybagel · · Score: 1

    Proton uses toxic hypergolic fuel. Energia was too expensive. That's why they made Angara. It's a cost-effective replacement for Proton.

  40. Re:And in the US by cheesybagel · · Score: 1

    It's not an ICBM like Proton. Angara was designed to launch satellites. Nothing more.

  41. It Won't Matter Anyway by Anonymous Coward · · Score: 0

    LEO is about to become useless when a few more large pieces of space junk break up and collide with other pieces to cause the junk cascade that pollutes LEO such that we can't either orbit in it or launch through.

    Don't take my word for it: go find the research. We're SO close to screwed that it's truly funny/scary/weird.

    Only I'm not laughing...

    1. Re:It Won't Matter Anyway by Anonymous Coward · · Score: 0

      Yup.

      Almost lost STS Endeavour to multi-thousand mph space junk paint flakes already. It blasted almost all the way through the "glass". Got lucky there...

      http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19950019959.pdf

      "For three of these windows, not enough of the projectile remained in the crater for a determination of the projectile material, but the majority of these impacts were man-made debris."

    2. Re:It Won't Matter Anyway by Mysticalfruit · · Score: 1

      The paint flake incident is what lead the shuttle to be basically flow upside down and backwards at an angle to put as much ship as possible between the crew and and any debris.

      I have heard talk of people pitching the idea of "space trash trucks" that would use a variety of techniques to capture and/or deorbit as much trash as possible. LEO is entirely too big to clean everything but there are some bands that are higher priority than others.

      --
      Yes Francis, the world has gone crazy.
  42. Re:And in the US by K.+S.+Kyosuke · · Score: 1

    It's a military rocket in the same sense that Atlas V and Delta IV are military rockets - they were commissioned by the military, for military needs, paid for with military funding (and therefore less likely to get cancelled in countries like US or Russia). I never claimed it was a missile.

    --
    Ezekiel 23:20
  43. Re:And in the US by K.+S.+Kyosuke · · Score: 1

    It was conceived as presumably cost-effective. It remains to be seen if this will actually be the case.

    --
    Ezekiel 23:20
  44. Re:And in the US by cheesybagel · · Score: 2

    That article is old news.

    Aborted launches happen all the time in the industry. Let alone in a new launch vehicle.

    The Angara A5 vehicle they are talking about in that article was successfully launched last December.

    They could use a better second stage for the rocket (i.e. the A7 version) but what they have is working fairly well. It would have been ready earlier if they didn't keep stalling the funding all the time. But it is ready now.

    All that's needed is for them to finish the construction of their new launch site at Vostochny and Proton can be killed.

  45. Re:And in the US by K.+S.+Kyosuke · · Score: 1

    What do you mean by "old news"? So the opinion voiced at the end of the article saying that (despite initial expectations) sustained cost of Angara will most likely be higher than sustained cost of Proton can change within half a year? And A7 is not A5 with two extra boosters, it requires a redesigned (different) core (meaning one more production line) and cannot launch from A5 pads.

    --
    Ezekiel 23:20
  46. Re:And in the US by Anonymous Coward · · Score: 1

    Why are you pushing this bullshit:

    The Wolf-PAC Resolution does not contain specific amendment language because we truly want to hear all sides and solutions at the amendments convention. We think the amendment should contain these core values:

    "Corporations are not people. They have none of the Constitutional rights of human beings. Corporations are not allowed to give money to any politician, directly or indirectly. No politician can raise over $100 from any person or entity. All elections must be publicly financed."

    *Note: The finished legislation will be worded differently and have to account for inflation, etc. This is simply to point legislators in the right direction and make sure the final amendment accomplishes the goals we have outlined here.

    http://www.wolf-pac.com/28th

    What part of CAMPAIGNING (not "elections" - lying-ass motherfuckers) do you want to publicly fund? Keep in mind that ELECTIONS are already funded publicly. Wolf-PAC is about coercive financing of:

    1) robocalls and telemarketing
    2) junk mail
    3) MOAR commercials (radio, TV, internet, etc)
    4) flyers littering the roads

    Funny thing about "3" is that I already block it but if they want me to be the sucker paying* for it, will it be claimed that I'm "stealing" from myself?

    Keep in mind, I have no dog in the 'corporate charter' fight. I'd be happy if we stopped issuing these limited liability monstrosities for non-public purposes (e.g., developing nukes to fight a war would be a public purpose that might require limited liability - selling me a burrito ... not so much).

    Keep in mind, I don't care if you require elected officials to be chaste and impoverished (although that would require a constitutional amendment).

    I draw the line at the government directing all the money - or even some of it - that is spent to determine how we run the government. Wolf-PAC is pro-statist and anti-democratic. It amazes me that so many people have fallen for it. "Why?", you might ask. It is because "Corporations are not people." True but that doesn't imply the true goals of the WOLF-PAC which is government control of how the government is selected.

    Why do people promote this without a text of the amendment? Do you really believe they will take in millions just to "hear all sides and solutions at the amendments convention"? They want a convention and your money without publicly disclosing amendment text. Dumb-ass mofo...

    * I pay 6-figures in tax (likely over $300,000 as a business owner)

  47. price of oil by Anonymous Coward · · Score: 0

    If the price of oil stays low, look for an announcement next year they are abandoning Angara and contracting it all out to SpaceX.

  48. So? by DerekLyons · · Score: 1

    So? I mean seriously, what is that elementary school level reply meant to accomplish?

    1. Re:So? by cheesybagel · · Score: 1

      Soyuz is more cost effective, and more reliable. What else do you need?

  49. Re:And in the US by cheesybagel · · Score: 2

    There are also plans to retrofit the KVTK LOX/LH2 second stage into A5. The whole A7 may or may not happen. It doesn't matter as A5 with KVTK would have more performance than Proton.

    The cost of handling hypergolics can be quite high. That is one reason why everyone is moving away from them. The costs for manufacturing the actual rocket may be higher but I kind of doubt it. Angara A5 is manufactured with more modern tools and it has less engines and parallel stages than Proton. Once it goes into full production the cost per unit is bound to be lower.

  50. Re:Not for SpaceX it isn't. Others - already there by dbIII · · Score: 1

    I'll restate my point in a different way - a small startup is going to be spread thin if they have multiple engines while an established org may already have had them for years.

  51. Re:And in the US by Damarkus13 · · Score: 1

    Is an ambitious project wasteful simply because there is a cheaper alternative? It seems like developing a super-heavy rocket might have benefits other than simply getting things to space cheaper than we could yesterday.

  52. We do these things... by Anonymous Coward · · Score: 0

    Why choose this as our goal? And they may well ask why climb the highest mountain?

  53. Re:And in the US by K.+S.+Kyosuke · · Score: 1

    Is an ambitious project wasteful simply because there is a cheaper alternative?

    What leads you to believe that there is something - anything - "ambitious" about recycling 1960s and 1970s technology? Wouldn't "ambitious" mean, I don't know...stuff like funding R&D for high-Isp pulse detonation engines?

    It seems like developing a super-heavy rocket might have benefits other than simply getting things to space cheaper than we could yesterday.

    You may not have noticed, but getting things into space cheaper is the greatest problem of all spaceflight at the moment.

    --
    Ezekiel 23:20
  54. Re:And in the US by K.+S.+Kyosuke · · Score: 1

    I believe the KVTK is not "a retrofit". It was planned for Angara A5 all along. There are simply different versions of it (or rather, there were plans for different versions), just like there are different versions of the DCSS and the Centaur. Regarding the costs, yes, it makes sense to think that the A5 offers a lot of potential for cost reductions in terms of modern manufacturing. At the same time, the engines are likely to be more expensive than the RD-275s (which, to my understanding, are basically dirt cheap) even if Angara needs fewer of them. All in all, I agree that switching to Angara is definitely a step in the right direction, but to assume implicitly that it will be cheaper than a launcher with very well established manufacturing and operation any time soon seems wildly optimistic at the moment. It will fall down from its current cost, but to what asymptotic level - that is the question to ask.

    --
    Ezekiel 23:20
  55. Private vs public expenditures by Anonymous Coward · · Score: 0

    Deep space research and rhus launch equipment is not a profit project yet and might become so in a few decades. In the mean time it is the role of governments to join together I such huge and costly projects. Had the US amd Russia and China been buddies along with EU and Canada,all of the players could have had a piece of this deep space project but human primates being what they are, cannot agree jot to compete, fight threaten and otherwise waste time and resources. Okay but on to the other topic that slipped into the comments which is about power companies private and state run.
          I live in Canada and we used to have a public electrical utilities. It was sold off to some US company. Our monthly charges are now broken into delivery line and a separate company,for energy costs. We pay at least five times what we did before. Do not be deceived by those fools who declare that public costs are always higher. Here we were being screwed by corporations who get away with lower taxes and a LAISSEZ faire provincial government in Alberta who gave away our birthright to foreigners. Some things work better as a private entrepreneurial system such as commercial entities such as SpaceX, a terrific innovative company but other things like running a power grid needs a wider net, a public one. One size does not fit all. It is childish frankly to think that private for profit is always better..yeah? Like the US medical establishment? Better? Don't make me laugh..ditto,for private insurance and power companies and the like. Ideologically driven economies are run by the 1 percent. Is this familiar?

  56. Re:And in the US by cheesybagel · · Score: 1

    The RD-275 may be dirt cheap as you say but those engines also use a bipropellant staged combustion cycle so I don't expect the parts count to be that different..

  57. Re:And in the US by cheesybagel · · Score: 1

    At most it has a simpler ignition because it runs on hypergolics.