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Russian Manned Space Vehicle May Land With Rockets

The Narrative Fallacy writes "Russia's next-generation manned space vehicle may be equipped with thrusters to perform a precision landing on its return to Earth. Previous manned missions have landed on Earth using a parachute or, in the case of space shuttles, a pair of wings. Combined with retractable landing legs and a re-usable thermal protection system, the new system promises to enable not only a safe return to Earth, but also the possibility of performing multiple space missions with the same crew capsule. The spacecraft will fire its engines at an altitude of just 600-800m, as the capsule is streaking toward Earth after re-entering the atmosphere at the end of its mission. After a vertical descent, the precision landing would be initiated at the altitude of 30m above the surface. Last July, Korolev-based RKK Energia released the first drawings of a multi-purpose transport ship, known as the Advanced Crew Transportation System (ACTS), which, at the time, Russia had hoped to develop in co-operation with Europe. 'It was explained to us how it was supposed to work and, I think, from the technical point of view, there is no doubt that this concept would work,' says Christian Bank, the leading designer of manned space systems at EADS-Astrium in Bremen, Germany. However, the design of the spacecraft's crew capsule had raised eyebrows in some quarters, as it lacked a parachute — instead sporting a cluster of 12 soft-landing rockets, burning solid propellant. Inside Russia, the idea apparently has many detractors. During the formal defense of the project, one high-ranking official skeptical of the rocket-cushioned approach to landing reportedly used an unprintable expletive to describe what was going to happen to crew members unlucky enough to encounter a rocket engine failure a few seconds before touchdown."

197 comments

  1. Unprintable expletive? by religious+freak · · Score: 4, Funny

    Of all the crap I've seen on /. I didn't realize we had unprintable expletives around here? Now, I'm curious - what could be so bad that it can't be printed on a /. page?!

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    1. Re:Unprintable expletive? by Chasmyr · · Score: 2, Funny

      what could be so bad that it can't be printed on a /. page?!

      Well he could have been running around the stage pretending he was an airplane.

    2. Re:Unprintable expletive? by Red+Flayer · · Score: 4, Funny

      I didn't realize we had unprintable expletives around here? Now, I'm curious - what could be so bad that it can't be printed on a /. page?

      Remember, the expletive was in Russian.

      Obviously, the expletive would be written using the Cyrillic alphabet, which, due to lack of UTF-8 support, is unprintable on slashdot.

      Also, in Soviet Russia, unknown expletive cannot print you.

      --
      "Trolls they were, but filled with the evil will of their master: a fell race..." -- J.R.R. Tolkien on Olog-hai
    3. Re:Unprintable expletive? by clyde_cadiddlehopper · · Score: 4, Funny

      Must be related to the unpronounceable symbol

      --
      Obi-Wan: "I felt a great disturbance in the Force, as if millions of voices suddenly cried out in terror and were sudden
    4. Re:Unprintable expletive? by camperdave · · Score: 3, Funny

      Um... That's pronounced "Publicity Stunt".

      --
      When our name is on the back of your car, we're behind you all the way!
    5. Re:Unprintable expletive? by mea37 · · Score: 2, Insightful

      You must be new here.

      It's not a question of "what's unprintable on slashdot".

      It's a question of "from whence was the summary text plagiarized, and what is considered unprintable there".

    6. Re:Unprintable expletive? by drinkypoo · · Score: 1

      Everyone knows it's pronounced "cha-ching!" That, or it's what it looks like when Prince tries to sign his name while having an especially energetic fit.

      --
      "You're right," Fisheye says. "I should have set it on 'whip' or 'chop.'"
    7. Re:Unprintable expletive? by The+Redster! · · Score: 1

      The bit about the "unprintable expletive" is a direct grab from the first article. BBC News didn't print it in the first place.

      You didn't seriously think a slashdot editor actually checked a summary, did you? :)

    8. Re:Unprintable expletive? by Garth+Vader · · Score: 1

      So I wasn't the only one who's first thought when reading this was "Well I am sure there is no way the Russians can fuck this up"

    9. Re:Unprintable expletive? by Anonymous Coward · · Score: 0

      As long as we are talking about form--you left your period in the wrong place ".

    10. Re:Unprintable expletive? by Anonymous Coward · · Score: 0

      > Now, I'm curious - what could be so bad that it can't be printed on a /. page?!

      Belgium.

    11. Re:Unprintable expletive? by Anonymous Coward · · Score: 0

      "oni yobnutsya"

    12. Re:Unprintable expletive? by Anonymous Coward · · Score: 0

      It's likely pronounced "peace death". Here, printed that for ya.

  2. Comment removed by account_deleted · · Score: 2, Funny

    Comment removed based on user account deletion

  3. Unicode support by TheLink · · Score: 4, Funny

    It's Russian, and Slashdot doesn't support the russian alphabet well?

    --
    1. Re:Unicode support by srmalloy · · Score: 4, Informative

      It's the BBC; if he used a term in Mat', the colloquial translation would be outside the range of what could be considered 'good taste', and in many cases the literal translation would be equally vulgar.

    2. Re:Unicode support by SEWilco · · Score: 1

      I wonder what his hovercraft is filled with, then.

    3. Re:Unicode support by skudenfaugen · · Score: 1

      eels?

    4. Re:Unicode support by moxley · · Score: 2, Interesting

      Thanks Srmalloy - learning about Russian "Mat" was the most interesting thing I read today while avoiding work.

      With my newfound skill, I am sure you'll understand when I say 'Yob tvoyu mat' that it is in the spirit of friendship.

    5. Re:Unicode support by slashdotwannabe · · Score: 0, Troll

      Oh yea, 'cos the best way to make new friends is to ask to fuck their mothers! Preferably in the basement bedroom of their 40yo slashdotting sons.

      --
      This comment is my opinion and does not represent an official position of Donald Trump or others I do not work for
  4. Using rockets for breaking? by TheRaven64 · · Score: 5, Funny

    That's so retro.

    --
    I am TheRaven on Soylent News
    1. Re:Using rockets for breaking? by kreyszig · · Score: 1

      retro as they are, the rockets are used for braking to stop the cosmonauts breaking

    2. Re:Using rockets for breaking? by ArcherB · · Score: 5, Funny

      retro as they are, the rockets are used for braking to stop the cosmonauts breaking

      or...

      If the retro retro's break, there will be no brakes to break the fall and the cosmonauts will become cosmo-nots.

      --
      There is no "I disagree" mod for a reason. Flamebait, Troll, and Overrated are not substitutes.
    3. Re:Using rockets for breaking? by Anonymous Coward · · Score: 0

      yo dawg i herd...

    4. Re:Using rockets for breaking? by sharkey · · Score: 1

      Well, they probably do a good job if you are trying to break things by burning them. Not sure how that is 'retro' though.

      --

      --
      "Outlook not so good." That magic 8-ball knows everything! I'll ask about Exchange Server next.
    5. Re:Using rockets for breaking? by mdielmann · · Score: 1

      cosmonauts will become cosmo-nots

      I prefer cosmo-blots.

      --
      Sure I'm paranoid, but am I paranoid enough?
    6. Re:Using rockets for breaking? by Daravon · · Score: 3, Funny

      If the retro retro's break, there will be no brakes to break the fall and the cosmonauts will become cosmo-nots.

      Burma Shave.

      --
      I traded all my mod points for these magic beans.
    7. Re:Using rockets for breaking? by Q-Hack! · · Score: 0

      cosmonauts will become cosmo-nots

      I prefer cosmo-blots.

      Through a little dirt over the top and you then have cosmo-plots.

      --
      Some days I get the sinking feeling Orwell was an optimist.
    8. Re:Using rockets for breaking? by MichaelSmith · · Score: 1

      In the Apollo and Mercury programs the Launch Escape System had to be able to lift the capsule high enough to deploy parachutes to make a soft landing. Take out the parachutes and the LES doesn't need to be so beefy. In fact it can use the same thrusters which are used for landing. This is a pretty good idea.

    9. Re:Using rockets for breaking? by Anonymous Coward · · Score: 0

      not nale. not-nale. thog help nail not-nale, not nale. and thog knot not-nale while nale nail not-nale. nale, not not-nale, now nail not-nale by leaving not-nale, not nale, in jail

  5. Expletive vial even to non-Russians? by Maximum+Prophet · · Score: 0

    one high-ranking official skeptical of the rocket-cushioned approach to landing reportedly used an unprintable expletive to

    I only know enough Cyrillic to recongize it, I can't actually read Russian.

    Imagine, an expletive so vial it transcends language barriers.

    --
    All ideas^H^H^H^H^Hprocesses in this post are Patent Pending. (as well as the process of patenting all postings)
    1. Re:Expletive vial even to non-Russians? by Anonymous Coward · · Score: 2, Funny

      Belgium

    2. Re:Expletive vial even to non-Russians? by Capt.DrumkenBum · · Score: 5, Funny

      "Imagine, an expletive so vial it transcends language barriers."

      I don't have to imagine it. The word you refer to is "Belgium".

      --
      If I were God, wouldn't I protect my churches from acts of me?
    3. Re:Expletive vial even to non-Russians? by snl2587 · · Score: 2, Funny

      You can fit all of that in a vial?

    4. Re:Expletive vial even to non-Russians? by Opyros · · Score: 1

      Two girls, one vial?

  6. Expletive: by InsertWittyNameHere · · Score: 1

    Splat!

  7. Re:"unprintable expletive" by moofmonkey · · Score: 0, Troll

    Chechnya ... I think

  8. unprintable expletive by ianare · · Score: 1

    SPLAT !!!

  9. Re:"unprintable expletive" by Maximum+Prophet · · Score: 2, Interesting

    In most languages copulation isn't an expletive. A native German speaker told me that the worst he could think of was "Go to the Devil", in Deutch.

    --
    All ideas^H^H^H^H^Hprocesses in this post are Patent Pending. (as well as the process of patenting all postings)
  10. Weight problems? by eebra82 · · Score: 3, Interesting

    In other words, they must think that adding that extra fuel weight (for landing) is worth the extra fuel weight that is needed to launch the rockets into space. After all, the landing fuel will cost them a lot of extra weight. I don't know how much extra it would be, but it doesn't sound like a good idea.

    1. Re:Weight problems? by Red+Flayer · · Score: 2, Insightful

      Yes, but how heavy were the parachute, parachute deployment system, and parachute shielding system that they were able to remove?

      --
      "Trolls they were, but filled with the evil will of their master: a fell race..." -- J.R.R. Tolkien on Olog-hai
    2. Re:Weight problems? by snaz555 · · Score: 5, Informative

      Without use of Kazakhstan, Russia has only a narrow strip of land that stretches far enough south to be worth launching from - and landing at. And this is not a flat desert wasteland. The reason for the rockets is to allow for a controlled landing. Parachutes are more suited for an ocean or desert landing where a few miles of accuracy doesn't make much difference. Presumably they figured that the weight of the landing system is outweighed by the benefit of launching (and landing) at a more southern latitude. Ocean landings aren't exactly free, either.

    3. Re:Weight problems? by skynexus · · Score: 1

      After all, the landing fuel will cost them a lot of extra weight.

      But what is the difference in weight between the thruster versus parachute landing systems?

      [...] it doesn't sound like a good idea.

      Sure, the added complexity may not improve the odds, but ignoring the inherent risk new technology entails, how much of an impact on safety are we really talking about here? It would seem that this is the way forward considering how NASA has also been contemplating a similar approach with the Delta Clipper for quite some time.

    4. Re:Weight problems? by Thanshin · · Score: 1

      they must think that adding that extra fuel weight (for landing) is worth the extra fuel weight

      Or, they could get their fuel on space.

      Is there any cheap way of sending light materials to a space station and turn them into fuel there to make a refueling orbital station for returning spaceships?

    5. Re:Weight problems? by Bill,+Shooter+of+Bul · · Score: 1

      Well, nothing in space is cheap. But we are currently using the cheapest methods of moving materials, or in the process of moving to cheaper methods. I think the Shuttle isn't very cheap when used to move raw materials, but there are somethings that only it is able to put in space due to size/weight of a discrete object.

      I think you are trying to invent the space elevator/gun or what not. Which sounds like a good idea. Go for it. Let me know when its operational, and I'll send a bottle of Sparking wine.

      --
      Well.. maybe. Or Maybe not. But Definitely not sort of.
    6. Re:Weight problems? by cheesybagel · · Score: 1

      Soyuz already includes retro rockets besides the parachute landing system.

    7. Re:Weight problems? by Anonymous Coward · · Score: 0

      It would seem that this is the way forward considering how NASA has also been contemplating a similar approach with the Delta Clipper for quite some time.

      Actually the Delta Clipper was a 1/3 scale vehicle developed by the DoD for the SDI project to prove you could take-off, maneuver and land verticaly under rocket power. It was to be the first step to developing an SSTO vehicle.

      After successfully demonstrating multiple vertical take-off and landings, it was handed over to NASA for further testing. On it's 4th flight, a technician forgot to connect a hydraulic line and the vehicle tipped-over on landing which cracked the LOX tank. The resulting fire destroyed the vehicle.

    8. Re:Weight problems? by GodfatherofSoul · · Score: 1

      How much lighter would the Space Shuttle's orbiter be if it didn't have those massive wings, tail, aerodynamic chassis, and airliner-style landing gear? Would a simple landing rocket system weigh LESS than everything required to make the orbiter a glider?

      --
      I swear to God...I swear to God! That is NOT how you treat your human!
    9. Re:Weight problems? by tsotha · · Score: 1

      Yes. And after they've added all that extra weight it will still be less than the wings chosen for some other country's retarded white space elephant.

    10. Re:Weight problems? by Methuseus · · Score: 1

      Wouldn't you like a space elevator? I would think sparkling wine would be better than sparking...

      --
      Two things are infinite: the universe and human stupidity, though I'm not yet sure about the universe. - A Einstein
    11. Re:Weight problems? by lgw · · Score: 1

      Far lighter than the fuel needed for a thrust-based landing. Remember the rocketry problem is exponential: twice the delta-V doesn't mean double the amount of fuel, but squaring the amount of fuel (more or less).

      --
      Socialism: a lie told by totalitarians and believed by fools.
    12. Re:Weight problems? by lgw · · Score: 1

      It's not the weight of the rocket engines. You already have those for takeoff. It's the weight of the fuel. They amount of fuel a rocket has to carry grows exponentially with g-seconds (delta V) of thrust needed. Doubling the delta-V you'll provide for the payload means squaring the amount of fuel needed. Most rockets are already mostly fuel.

      --
      Socialism: a lie told by totalitarians and believed by fools.
    13. Re:Weight problems? by An+anonymous+Frank · · Score: 1

      What about refueling while in space?

    14. Re:Weight problems? by DerekLyons · · Score: 1

      Yes, but how heavy were the parachute, parachute deployment system, and parachute shielding system that they were able to remove?

      Much, much lighter than the rockets, legs, and fuel systems. A parachute system for a Soyuz size vehicle weighs a few hundred pounds. The fuel alone for a rocket landing system will probably weigh over a ton at minimum.

  11. Old news? by AZScotsman · · Score: 5, Informative

    McDonnell-Douglas did this almost 20 years ago - the DC-X (http://en.wikipedia.org/wiki/DC-X), later known as the Delta Clipper.

    1. Re:Old news? by Anonymous Coward · · Score: 0

      It never did it after re-entry, though.....

    2. Re:Old news? by ColdWetDog · · Score: 1

      Thanks for the reminder on the DC-X. I forgot that thing existed, much less actually worked (for takeoff and landing, getting out of the atmosphere wasn't attempted).

      --
      Faster! Faster! Faster would be better!
    3. Re:Old news? by netruner · · Score: 1

      Didn't the clipper use liquid fuel? IIRC that was its downfall when it blew up on the landing pad when one of its feet didn't deploy and it tipped over.

      Either way, I would urge anyone trying to crack this tech to review the clipper's failure before continuing.

      --



      DISCLAIMER: This post was not checked for speling and grammar- if you complain- you're a whiner
    4. Re:Old news? by AZScotsman · · Score: 4, Informative

      The original DC-X was a half-scale (IIRC) version just designed to demo the tech of "Landing on your own tailfire", and all the initial flights were tethered. Flew several times in '93 and '94, but the final flight in '96 experienced a hydraulic line failure in one of the struts, and tipped over. In a "full-up" system, a backup manual extender would have mitigated the problem.

      Good info on the flights are found on NASA's Website http://www.hq.nasa.gov/office/pao/History/x-33/dc-xa.htm

    5. Re:Old news? by Anonymous Coward · · Score: 0

      but the final flight in '96 experienced a hydraulic line failure in one of the struts, and tipped over.

      This was after it was handed over to NASA after the initial concept; i.e, taking-off, maneuvering and landing under rocket power was proven.

      NASA outfitted it with an experimental fuel tank (I forget, either the H2 or LOX tank) and it tipped over while landing when a tech "forgot" to connect a hydraulic line to one of the landing structs. Oddly enough, it wasn't the tipping over that destroyed it, but the fire caused by leaking LOX.

      NASA didn't want it and went on to "prove" that SSTO is impossible with the failure of the X-33 project.

      What? Me a cynic? Where did you get that idea?

    6. Re:Old news? by Anonymous Coward · · Score: 0

      And the thing used a russian made fuel tank, so it wasn't just all American :P

    7. Re:Old news? by John+Bayko · · Score: 1

      As I recall, a technician forgot to plug in a hydraulic line on one strut. The real flaw was having only four landing legs - even one more would have made it stable if one failed.

    8. Re:Old news? by hitmark · · Score: 1

      i knew i had seen the "solution" before somewhere, thank you so much.

      --
      comment first, facts later. http://chem.tufts.edu/AnswersInScience/RelativityofWrong.htm
  12. Seems Pretty Inefficient by Kozar_The_Malignant · · Score: 4, Insightful

    It seems pretty inefficient to carry the fuel mass for the retro rocket braking all the way up out of the gravity well into orbit and then back down into the gravity well so you can use it in the last kilometer of the flight. There doesn't seem any way to stop at a gas station on the way down, but maybe they are planning on lifting the fuel to orbit on non-reusable tankers, which also seems inefficient. In something like this, inefficient equates to really fucking expensive.

    --
    Some mornings it's hardly worth chewing through the restraints to get out of bed.
    1. Re:Seems Pretty Inefficient by OolimPhon · · Score: 4, Informative

      From TFA, the fuel is solid. Not easy to refill from tankers.

    2. Re:Seems Pretty Inefficient by arielCo · · Score: 2, Interesting

      It seems pretty inefficient to carry the fuel mass for the retro rocket braking all the way up out of the gravity well into orbit and then back down into the gravity well so you can use it in the last kilometer of the flight.

      In other words, spend additional energy to take more energy up with you, which you will spend dissipating all of the energy you gained going up.

      That, or to keep taking advantage of the viscous gas you'll find on the way down to brake, where available. If you want precision, then you add a bit of chemically-generated thrust to steer. Where there's not enough gas (Mars and smaller), gravity may be weak enough to make the DC-X approach add up.

      --
      This post contains no rudeness or derision of any kind. All arguments are friendly. Terms and exclusions may apply.
    3. Re:Seems Pretty Inefficient by evanbd · · Score: 4, Insightful

      Your choices are rockets, parachutes, wings and landing gear, or a variety of weird and exotic options (like deploying helicopter blades; see the Roton concepts). There are a variety of reasons to prefer rockets to parachutes (and vice versa). The rockets are likely somewhat heavier than the parachutes and their deployment system, but I suspect the weight difference is small enough that the decision would likely be made on the basis of operational advantages (like being able to do a landing on solid ground instead of the ocean easily).

      The American space program seems to be of the opinion that everything should be as light weight and efficient as possible, without regard to other criteria. The Russians, on the other hand, have a long history of being willing to build larger, heavier, less efficient rockets in order to make operations easier. Personally, I think the Russian approach is better -- the correct figure of merit to optimize is not liftoff weight, but cost. If you can develop, build, and/or operate more cheaply by spending more weight on the problem, that's a win in my book.

    4. Re:Seems Pretty Inefficient by vlm · · Score: 1

      That, or to keep taking advantage of the viscous gas you'll find on the way down to brake, where available.

      Oh, they're doing that... Its not like you'll decelerate from orbital to rest in just 600 meters above the surface. Heck I don't know if you'd decelerate from orbital to reset going 600 meters below the surface.

      I did enjoy the funny slashdot headline, if you emphasize the word "may" as in possibly or maybe.

      --
      "Science flies us to the moon. Religion flies us into buildings." - Victor Stenger
    5. Re:Seems Pretty Inefficient by Anonymous Coward · · Score: 0

      If you had read the article, you'd find out that in this case the reason to go with rockets is not cost, but politics. The russians want to stop using Kasachstan for their space port, and since they want to have efficent location as far south as possible for the launch, they are limited to a rather small speck of Russia to land on. To aim more precisely at that small speck, they need rockets for their improved control.

    6. Re:Seems Pretty Inefficient by jollyreaper · · Score: 1

      Your choices are rockets, parachutes, wings and landing gear, or a variety of weird and exotic options (like deploying helicopter blades; see the Roton concepts). There are a variety of reasons to prefer rockets to parachutes (and vice versa). The rockets are likely somewhat heavier than the parachutes and their deployment system, but I suspect the weight difference is small enough that the decision would likely be made on the basis of operational advantages (like being able to do a landing on solid ground instead of the ocean easily).

      This is where you have to weigh the cost of the additional weight of rockets vs. parachute with the cost of having a carrier battle group standing by to pluck the astronauts out of the water. The Russian technique of just pointing the capsule at a wide expanse of steppe and sending out helicopters to retrieve the crew makes a lot of sense, far cheaper.

      --
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    7. Re:Seems Pretty Inefficient by hey! · · Score: 1

      Speaking as a totally ignorant (and thus opinion-entitled) person, I'd like to know why you couldn't combine parachutes and rockets. I'm imagining something like a powered paraglider.

      My ignorant mind can think a of a number of apparent advantages to that over rockets alone.

      --
      Post may contain irony: discontinue use if experiencing mood swings, nausea or elevated blood pressure.
    8. Re:Seems Pretty Inefficient by Anonymous Coward · · Score: 0

      If I remember correctly, the Russians have been landing their spacecraft on land with parachutes for as long as they've been going to space.

    9. Re:Seems Pretty Inefficient by shutdown+-p+now · · Score: 1

      Building launch facilities with slave labor (prisoners) is another way to cut operational costs which Russians have perfected. Same go about designing rockets - Korolev started to work on space program in a work camp for engineers (sharashka.)

      I see you've missed the news for, like, the last 20 years, if you think that your comment is in any way relevant to this discussion of modern Russian space tech...

    10. Re:Seems Pretty Inefficient by dwye · · Score: 1

      > The Russian technique of just pointing the capsule at
      > a wide expanse of steppe and sending out helicopters
      > to retrieve the crew makes a lot of sense, far cheaper.

      First, you do not need a carrier battle group, just the carrier and a bunch of heavy lift helos.

      Second, we have a dozen (or more - some WWII carriers were used in Project Mercury) just laying around, and they had none.

      Third, they have a million square miles of steppe just laying around (some of it with nice cooling ice), and we have a lot less. Further, theirs is east to west in the long dimension, and ours is north to south.

      Fourth, we have to hit the 3/4 of the Earth's surface that is water, when planning splash-down, but they have to hit their steppe, which is a fairly small fraction of the land, which is just 1/4 of the Earth's surface.

      Different cost structures, you see. How much would it have cost for the USA to rent or buy all of Siberia and the less mountainous parts of the -stans from the Soviets? How much for the Soviets to rent or buy a carrier or two from, well probably from France rather than the USA, but still, how much?

      For the USA, sea landings and carrier pick ups were cheaper.

      We also had a better accident rate, until we started landing on land, too.

    11. Re:Seems Pretty Inefficient by Anonymous Coward · · Score: 0

      but I thought landing with rockets on Earth was just to practice for landing on Mars with rockets

    12. Re:Seems Pretty Inefficient by justin12345 · · Score: 1

      I'm imagining something like a burning parachute. ;-)

      --
      Cool art gallery, if you're into that sort of thing.
    13. Re:Seems Pretty Inefficient by ArcadiaAlex · · Score: 0

      I have to say that launching a shuttle while very cool in concept and very handy for returning large objects from orbit, but given how little that was used is about the heaviest solution I think you could imagine to lift a few astronauts to the space station.

      I think the weight of the russian capsule with the added weight of the solid rockets, plus a few spares in case of failure would still come in as a lighter option than lifting a shuttle.

      This of course will change with the new Orion as it is back to the light weight capsule idea (as is required to leave low earth orbit)

  13. High-G landing? by cdrguru · · Score: 3, Interesting

    Let's see, how fast might the ship being going when the landing system kicks in? Falling from orbit to the ground is going to produce a lot of velocity to bleed off in apparently a very short time. The shuttle uses both atmospheric braking and S-turns to bleed off velocity and still lands pretty darn fast.

    It sounds like this just falls without a chute. I'm not going to do the math, but even if it is subsonic at 800m, you are going to have to brake like mad at the end. 10G braking? 20G doesn't sound like it would be outlandish. OK, so it is a short period of time and with solid-fuel rockets it is just one pulse. But it sounds like it would be ohe heck of a pulse.

    1. Re:High-G landing? by starglider29a · · Score: 2, Interesting

      Something is amiss here. The energy to stop a falling box of people is APPROXIMATELY* the same energy is takes to get it up to where it fell FROM.

      If this could REALLY work as described, we wouldn't need a whole stinking stage to get the box o'humans UP into space. Email me when this works. If it doesn't, I'll hear about it.

      *Yes, the atmosphere drags both ways, but the speed it gains from falling 100,000m to 800m is less than what it would lose punching through the atmosphere.

    2. Re:High-G landing? by RobertB-DC · · Score: 4, Funny

      It sounds like this just falls without a chute. I'm not going to do the math, but even if it is subsonic at 800m, you are going to have to brake like mad at the end. 10G braking? 20G doesn't sound like it would be outlandish. OK, so it is a short period of time and with solid-fuel rockets it is just one pulse. But it sounds like it would be ohe heck of a pulse.

      You're missing the point, though. Gravity is an *acceleration*. These guys will be *decelerating*. You know, like zero gee is zero acceleration? Since they'll be slowing down, they won't feel a thing. It's genius!

      (I can feel the karma draining now...)

      --
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    3. Re:High-G landing? by Stratocastr · · Score: 0

      Just name it COLBERT.. It will land perfectly.

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      Slashdot - I went there to fix their grammar that they're so bad at.
    4. Re:High-G landing? by Aranykai · · Score: 2, Informative

      Lol, you accidentally the whole equation.

      --
      If sharing a song makes you a pirate, what do I have to share to be a ninja?
    5. Re:High-G landing? by Rolgar · · Score: 1

      I think the space shuttle orbits earth 16 times a day (90 minutes/orbit), or about 27,000 kph. Terminal velocity of the capsule is much lower (less than 300kph) than the speed of the capsule in orbit, which is why the reentry from space is so hot, because the spacecraft is losing speed as it reenters, not picking up speed. This is the same speed that was gained when the craft originally launched into orbital. Link

      If you compare this to a fighter taking of from an aircraft carrier, a catapult changes the speed of the craft by 265m in two seconds which works out to 9Gs. I think fighter pilots and astronauts are trained for at least 10G acceleration, and this craft would be making a similar change in speed.

      Tough, sure, but it's nothing that these guys aren't trained for.

    6. Re:High-G landing? by Rolgar · · Score: 1

      Forgot to proof read my link: http://www.lpi.usra.edu/education/explore/capsules/

      What I said isn't an approval of the use of this method, just a recognition that the acceleration experienced to land at the end could be successful in not killing the astronauts.

    7. Re:High-G landing? by Waffle+Iron · · Score: 4, Insightful

      Capsules don't just plummet vertically through the atmosphere. They spend most of the reentry going almost horizontally bleeding off speed. Most of them also angle the heat shield so that they get a good deal of lift, and they "fly" for a more gentle reentry.

      In any case, a capsule must slow down to less than hypersonic speeds before deploying a parachute. Otherwise the parachute would burn up and/or be ripped to shreds.

      Once a capsule is going slowly enough to put out a chute, it doesn't have all that much kinetic energy. Small retrorockets would be sufficient to stop it instead.

    8. Re:High-G landing? by Plekto · · Score: 1

      You're missing the point, though. Gravity is an *acceleration*. These guys will be *decelerating*. You know, like zero gee is zero acceleration? Since they'll be slowing down, they won't feel a thing. It's genius!

      ****
      I wonder if the impact will be over with quicker than their neurons can fire? I suspect that if it fails, yes, they won't feel a thing.

    9. Re:High-G landing? by sjames · · Score: 1

      Even a simple capsule doesn't just fall. It's quite common for them to gain some lift from their attitude as they reenter. That is, even without wings, the reentry path is not ballistic.

      Keep in mind, the energy to get people into orbit isn't just the gravitational potential energy to raise them to their final altitude, they also need to be accelerated at a tangent to the Earth's surface to achieve orbit. Much of that energy is what is converted to heat during reentry.

      The other factor is that on ascent, the rocket has to lift it's own weight and the weight of it's fuel. Most of that is gone by the time the humans reenter.

      The potential and kinetic energy of the fuel dissipates into the atmosphere. That of the stages is dissipated by burning in the atmosphere and in the splat when their remains "land".

      The crew vehicle dissipates much of it's energy into the atmosphere during reentry leaving only a small fraction of the total to be managed by rockets of parachutes.

    10. Re:High-G landing? by smoker2 · · Score: 1

      Please define 800m. Is that metres or miles ? Because 800 metres is not enough, for any known human or braking system.

    11. Re:High-G landing? by cdrguru · · Score: 1

      I was assuming some aerobraking, of some sort. Think back to Apollo capsules. They would leave orbit at 25000MPH and start re-entry. Lots of aerobraking. I don't know the deployment speed, but the first chute out of the bag was a ribbon chute which would slow it down enough to deploy the three big chutes. Touchdown was in water, but the impact velocity wasn't enough to submerge the capsule.

      Now, take away the ribbon chute and the main chutes. With just the heat shield you are going to get lots of aerobraking just as before. So we have slowed from 25000MPH to maybe 500. Let's be extremely generous and say they are going to jog around in the atmosphere shuttle-style until the speed drops to 200MPH.

      The summary said the rockets we going to fire around 800m - meters, I presume. 2500 feet.

      Yes, this would be similar to a figher plane catapult launch, maybe a little worse. One thing that I see right off the seating for launch is all wrong for this type of landing. You are laying on your back with a nice, broad supportive seat to hold you and distribte the liftoff acceleration. Same idea with a catapult launch where you are being pushed back into the seat. So what, are you experiencing 9 or 10 G hanging in the straps? Hope those are nice, wide straps.

      As a note aside, acceleration is a vector. You can have acceleration in a positive direction or a negative direction. Braking is a negative acceleration. The forces are identical, just the sign is flipped.

    12. Re:High-G landing? by shutdown+-p+now · · Score: 2, Insightful

      Something is amiss here. The energy to stop a falling box of people is APPROXIMATELY* the same energy is takes to get it up to where it fell FROM.

      If this could REALLY work as described, we wouldn't need a whole stinking stage to get the box o'humans UP into space. Email me when this works. If it doesn't, I'll hear about it.

      You missed one crucial factor here: terminal velocity. An object falling down to Earth does not accelerate indefinitely, but only until the force of air resistance (which, naturally, grows as speed increases) becomes large enough to offset the gravity completely - at that point, the speed is constant. So you only need to be able to brake from that to whatever is safe for touchdown.

      I've no idea what the terminal velocity of this thing would be (it depends on both its mass and profile), but to give some idea of how it works: for a human, that velocity is ~200 km/h. Note that this is no matter how high you jump down from - it will still be the same figure as you approach the surface. It will certainly be higher for the module, but I wonder how much higher...

    13. Re:High-G landing? by rts008 · · Score: 1

      No, it's meters and not miles.
      The ISS it would be coming back to Earth from only orbits the Earth at around 160 miles altitude.

      The abbreviation for mile is mi.

      Because 800 metres is not enough, for any known human or braking system.

      Why is it not enough?
      Thousands of skydivers and paratroopers will dispel that statement of yours.

      --
      Down With Slashdot BETA!!! I've been around the corner and seen the oliphant; you can only abuse me from your perspecti
    14. Re:High-G landing? by Tacvek · · Score: 1

      Oh come on. Swivel seats. Duh!

      --
      Stylish sheet to fix many problems in Slashdot's D3: https://gist.github.com/801524
    15. Re:High-G landing? by Tacvek · · Score: 1

      Terminal velocity applies when starting from zero velocity. You are correct that the vertical velocity should never exceed terminal velocity since that is initially zero, but the horizontal velocity begins at a rate that greatly exceeds terminal velocity. (Even that is slightly inaccurate thanks to Earth being a damned rotating reference frame.) Thus the speed of the craft will exceed terminal velocity until nearly the very end. That is the whole concept of aerobraking. Once you are in the atmosphere, the atmosphere will tend to slow you down to terminal velocity. However, not only would terminal velocity for the craft still be fatal, but it is very unlikely the craft would even slow down to it before impact if not for parachutes (these greatly reduce terminal velocity) or retrorockets (these don't change the terminal velocity, but do change the actual velocity).

      --
      Stylish sheet to fix many problems in Slashdot's D3: https://gist.github.com/801524
  14. Comment removed by account_deleted · · Score: 2, Interesting

    Comment removed based on user account deletion

  15. Sounds more like NASA by wjousts · · Score: 0, Troll

    Take a simple, cheap, reliable solution (parachute) and replace it with an expensive, complicated and less robust solution (retro rockets).

    I can't help but think of the space pen (beacause regular pens don't write in zero-g) that NASA invented at great expense. The Russians (allegedly) just used a pencil instead.

    1. Re:Sounds more like NASA by blind+biker · · Score: 1

      I can't help but think of the space pen (beacause regular pens don't write in zero-g) that NASA invented at great expense. The Russians (allegedly) just used a pencil instead.

      That myth/urban legend has been busted long time ago, tovarish :o)

      --
      "The agriculture ministry is not in charge of Gundam" - Japanese ministry official.
    2. Re:Sounds more like NASA by fracai · · Score: 5, Informative

      This again? Let it die.

      NASA didn't fund the pen at all.
      When it was developed, BOTH the Russians and the US adopted it's use.
      Before that, they BOTH used grease pencils, because broken graphite and flammable wood are loads of fun in space.

      http://en.wikipedia.org/wiki/Space_pen#Uses_in_the_U.S._and_Russian_space_programs

      --
      -- i am jack's amusing sig file
    3. Re:Sounds more like NASA by vlm · · Score: 1

      Take a simple, cheap, reliable solution (parachute) and replace it with an expensive, complicated and less robust solution (retro rockets).

      Parachutes are by no means as simple and cheap (or reliable) as you'd think.

      On the other hand, for a bunch of "rocket scientists" whats just one more rocket? If there's one thing rocket scientists know, its rockets.

      Bonus points if you could use the "other half" of the final ascent stage. Of course no vacuum nozzles allowed, would need a ground pressure (or higher) rated nozzle to eliminate flow separation.

      --
      "Science flies us to the moon. Religion flies us into buildings." - Victor Stenger
    4. Re:Sounds more like NASA by santax · · Score: 1

      BOTH

      I understand the Bastard Operators but the T and H are beyond me. Anyone?

    5. Re:Sounds more like NASA by idontgno · · Score: 1

      Well, "BOFH" is "Bastard Operator From Hell".

      By simple symmetry, I'd guess that "BOTH" stands for "Bastard Operator To Hell" and represents the sysadmin's commute home.

      H2H.

      --
      Welcome to the Panopticon. Used to be a prison, now it's your home.
    6. Re:Sounds more like NASA by daeley · · Score: 1

      Bastard Operator To Hell

      Oh no! The Unprintable Expletive! You madman! What have you done??!!

      --
      I watched C-beams glitter in the dark near the Tannhauser gate.
    7. Re:Sounds more like NASA by jheiss · · Score: 1

      "Flammable wood" is no good, but grease is OK? I don't know what kind of pencil they used, but if it was grease instead of graphite I suspect it wasn't due to flammability concerns. Broken graphite seems a more plausible concern.

  16. Re:"unprintable expletive" by Daimanta · · Score: 2, Funny

    "Chechnya"

    You have insulted my mother you American pig-dog, prepare for a duel!

    --
    Knowledge is power. Knowledge shared is power lost.
  17. Safety by wiredlogic · · Score: 1

    I can't imagine that a parachute wouldn't still be used for the initial descent. This plan also requires comparatively large amounts of rocket fuel to be launched and brought back down and is a potential safety risk in the event of a malfunction on landing. In the case of the survived malfunctions with the Soyuz system, many have been sheer luck but some of the survivability has to be attributed to the simplicity of the design.

    --
    I am becoming gerund, destroyer of verbs.
  18. What?! by G0N70 · · Score: 0

    Are they still searching for that dog?!

    --
    (Score:0, Offtopic)
  19. This comes up all the time. by Eevee · · Score: 5, Informative

    It's an urban legend.

  20. Unprintable? by Anonymous Coward · · Score: 0

    Come on Comrade, I'd love to learn some Russian swear words. Openness and all, remember? :)

  21. Cost? by EvilBudMan · · Score: 1

    Just making new capsules without the rockets may be just as cost effective. That is all that you are saving from the trip.

    1. Re:Cost? by drinkypoo · · Score: 1

      Just making new capsules without the rockets may be just as cost effective. That is all that you are saving from the trip.

      I think you're forgetting something. Is it just as cost effective to make new cosmonauts? Or maybe you planned to have them make some UHALO jumps. Master Chiefs away!

      --
      "You're right," Fisheye says. "I should have set it on 'whip' or 'chop.'"
    2. Re:Cost? by sjames · · Score: 1

      Nah, the cosmonauts are just instructed to jump up the instant the capsule hits the ground. What could go wrong?

    3. Re:Cost? by EvilBudMan · · Score: 1

      I'm pretty sure that their old system with parachutes and retro rockets that sometimes didn't work and gave a pretty rough landing would be far lighter than a bunch of huge retro rockets.

      I don't think this idea will fly even in Russia.

      Capsules have parachutes on them. Plain and simple and proven. I guess you could put ceramic tiles on the whole damn thing and reuse it.

      Throw away, at least for rocket science, seems to be the cheapest way to go. The only reason Nixon approved the shuttle wasn't because of cost (they just told us that). It was because someone from NASA told him that we could bring stuff back with it like Russian spy satellites.

      I don't make sense and if the glove don't fit ya gotta acquit.

    4. Re:Cost? by drinkypoo · · Score: 1

      I agree that using retros to land on Earth doesn't make sense at this point, for that you need a nuclear rocket and someplace to land it. But the issue is still more complicated than "delete retros"

      --
      "You're right," Fisheye says. "I should have set it on 'whip' or 'chop.'"
  22. Firing off at 30 meters!? by alta · · Score: 1

    That's got to be some serious thrust and precision. Actually, if this works, without intertial dampeners, the people inside are going to be goo on the floor ;)

    --
    Do not meddle in the affairs of sysadmins, for they are subtle, and quick to anger.
  23. Do we know the plan doesn't use air resistance? by JSBiff · · Score: 2, Interesting

    Ok, so the design is based upon rockets, but does it mean that it uses *no* aerodynamic braking at all? I don't know a whole lot about aerodynamics, but I remember from physics class the discussion of drag and terminal velocity. Is it possible that the shape of their vehicle has a relatively slow terminal velocity, so that the rockets don't have to do *that much* braking at the end? Not that I'm saying that I think even requiring a small amount of retro-rocket braking is a good design, but it seems like maybe you are assuming an awful lot about what speed it will be at when they fire the rockets?

    1. Re:Do we know the plan doesn't use air resistance? by evanbd · · Score: 2, Interesting

      I suspect you're absolutely correct. Killing your orbital velocity on rockets alone is almost as hard as getting there in the first place. In fact, if you take the weight of the Apollo heat shields and the amount of delta-v they provide during reentry, you find they get an Isp of around 7000s -- compared to numbers in the range of 260-450 for bipropellant rockets. Heat shields are so vastly superior for the problem that you'd be insane not to use them.

    2. Re:Do we know the plan doesn't use air resistance? by jbb1003 · · Score: 3, Informative

      The energy to stop a falling box of people is nowhere near the same energy it takes to get it up to where it fell from when you're dealing with high speeds. Aerodynamic resistance is signficant even on a bicycle at 30mph, never mind a space reentry behicle.

      The atmospheric drag does work both ways. But on the way up, a rocket presents an aerodynamically efficient profile - i.e pointy bit first. On the way down reentry vehicles go what you might call butt first, presenting the most aerodynamically *inefficient* profile possible.

    3. Re:Do we know the plan doesn't use air resistance? by JSBiff · · Score: 2, Informative

      I think I know what you're talking about. I remember when I was young, going to some sort of space museum (I think it was part of the NASA facility near Cleveland, OH), and they had a space capsule (well, it might have just been a replica - don't remember if it was real or now). But, the capsule was presented 'detached' from the rocket, and it had a very wide, slightly rounded 'bottom', which they said during re-entry orients itself towards the ground, so all the air is colliding with the large surface-area bottom, creating a lot of drag.

      I suppose this proposed Russian design is at least somewhat similar.

    4. Re:Do we know the plan doesn't use air resistance? by vlm · · Score: 1

      Is it possible that the shape of their vehicle has a relatively slow terminal velocity, so that the rockets don't have to do *that much* braking at the end?

      Yes, and not only that, you can take an off the shelf survivable roll cage and crunch zone design from a race car, and build the capsule around it. So, if the rocket doesn't work, the vehicle is an utter total loss, but the crew walks away basically unscratched, more or less.

      --
      "Science flies us to the moon. Religion flies us into buildings." - Victor Stenger
    5. Re:Do we know the plan doesn't use air resistance? by treeves · · Score: 2, Interesting

      [Pointy end first = most aerodynamic] is not necessarily true.
      Why do submarines have the big round end in front and the pointy end at the rear?

      --
      ...the future crusty old bastards are already drinking the Kool-Aid.
    6. Re:Do we know the plan doesn't use air resistance? by jbb1003 · · Score: 1

      I don't know anything about submarine design, but I suspect a large part of the design is driven by the requirement to be as quiet as possible. A submarine also needs to withstand significant pressures.

      All modern aircraft I have ever seen have the pointy bit at the front

    7. Re:Do we know the plan doesn't use air resistance? by treeves · · Score: 1

      The making it quiet part is achieved by minimizing turbulent flow, which is equivalent to minimizing drag, which means "more aerodynamic". The withstanding pressure part is accomplished by the double hull, of which the inner one, the pressure hull, is a simple tube with hemispherical ends. The outer hull is the part that can be shaped to achieve the desired flow characteristics.

      --
      ...the future crusty old bastards are already drinking the Kool-Aid.
  24. Re:"unprintable expletive" by atari2600 · · Score: 0

    Level 80 epicced DK here bitch, prepare to lose.

  25. what was going to happen to the crew by blind+biker · · Score: 1

    During the formal defense of the project, one high-ranking official skeptical of the rocket-cushioned approach to landing reportedly used an unprintable expletive to describe what was going to happen to crew members unlucky enough to encounter a rocket engine failure a few seconds before touchdown."

    It would accidentally the whole crew!

    --
    "The agriculture ministry is not in charge of Gundam" - Japanese ministry official.
  26. Re:"unprintable expletive" by Aranykai · · Score: 1

    That is soooo my new insult of choice.

    --
    If sharing a song makes you a pirate, what do I have to share to be a ninja?
  27. Re:"unprintable expletive" by Chris+Burke · · Score: 5, Funny

    In French Québec, we're lucky enough to combine all four.

    And not just in your profanity!

    --

    The enemies of Democracy are
  28. Don't judge by oldhack · · Score: 4, Funny

    I think this will work. It's used extensively on giant robots in Japanese cartoons.

    --
    Fuck systemd. Fuck Redhat. Fuck Soylent, too. Wait, scratch the last one.
  29. Not completely new by Urban+Garlic · · Score: 4, Informative

    The existing Soyuz TMA capsules also have "soft-landing rockets", they're used just at the point of touchdown to cushion the landing. Of course, the TMAs also have a parachute, so it's less of a problem if the landing rockets fail.
    Interestingly, the very first Soyuz TMA had all kinds of other problems, but the landing-rocket part actually worked.

    --
    2*3*3*3*3*11*251
  30. the quotation is wrong by Anonymous Coward · · Score: 1, Informative

    The high ranking official and flying expletive both refer not to the spacecraft design of today, but to the Zarya spacecraft of 80's. Read the article carefully - it mentions that; only the /. quote is wrong.

  31. Re:"unprintable expletive" by zlenko · · Score: 1

    Ex-ple-tive. Nice new word for me. No, "fuck" is not THAT word.

  32. Re:Using rockets for breaking? Homage to NASA? by davidsyes · · Score: 1

    It was a "windy day in Arizona" when the US flag fluttered.

    Now, Federal'noe kosmicheskoe agentstvo Rossii, (RKA) will blow DUST in the yankee eyes by landing with RETRO RETROs... But, i don't know if it will be a dusty/chokey day in Chernobyl or Sunny Siberia...

    (Since, apparently, Russia has no deserts...

    http://www.worldreviewer.com/travel-guides/desert/in-russia/

    )...

    --
    Previously: "Linux... Toward the Sunrise..." Now: "Linux... Toward the-- No, now, part of Every Sunrise"
  33. I'm still waiting for... by HikingStick · · Score: 1

    Astronauts that have heat-shielded spacesuits and pop-out hang-glider wings gliding back to terra firma.

    --
    I use irony whenever I can, but my shirts are still wrinkled...
  34. Re:"unprintable expletive" by dnormant · · Score: 1

    And Chernobyl would be the past tense, fucked?

  35. Re:"unprintable expletive" by nacturation · · Score: 1

    +6, Funny

    --
    Want to improve your Karma? Instead of "Post Anonymously", try the "Post Humously" option.
  36. Air is not enough. by fm6 · · Score: 1

    Ok, so the design is based upon rockets, but does it mean that it uses *no* aerodynamic braking at all?

    I'm sure it does. Hard to imagine that they could carry enough fuel to rely solely on the rockets for braking.

    But they still need to land. Since you're moving relatively slow at this point (but still fast enough to kill your crew) you can't airbrake with your vehicle body. At this point you have to deploy a system that works at relatively slow speeds. Most spacecraft rely on parachutes, sometimes supplemented by the extra cushioning of an ocean landing. But this doesn't give you a lot of control over how you touch down, and you really need it if you're going to design a reusable vehicle.

    And we really need to reuse more of our space hardware. We'll never have a self-sustainable business model for space travel as long as all our expensive hardware is one-use-only.

    The Shuttle implements precision landing by turning into a glider after the aerodynamic braking is done. (I still think this is the best model; the Shuttle's problems stem from skimping on other features of the design.) The Russians would seem to have decided that landing rockets are a better approach (pun unavoidable).

    1. Re:Air is not enough. by lgw · · Score: 1

      And we really need to reuse more of our space hardware. We'll never have a self-sustainable business model for space travel as long as all our expensive hardware is one-use-only.

      Sure, if the goal is to make rockets that look like the covers of 60's SF novels. Not so much if the goal is to get into space cheaply. Many of the "re-usable" elements of the space shuttle turned out to be more expensive per flight than discardable elements would have been. The goal needs to be "do what's cheap" not "do what looks cool in SF".

      Make the discardable boosters cheap, don't try for even-more-expensive reusable boosters.

      --
      Socialism: a lie told by totalitarians and believed by fools.
    2. Re:Air is not enough. by fm6 · · Score: 1

      Many of the "re-usable" elements of the space shuttle turned out to be more expensive per flight than discardable elements would have been.

      The space shuttle was poorly planned from beginning to end. First they tried to do it on the cheap, then they spent gobs of money kludging on fixes for their initial mistakes — kludges that have killed way too many astronauts. The only lesson I take away from the shuttle program is that if Congress refuses to give you a proper budget for building a spacecraft, don't try to build it anyway.

      Nor do I buy the "cheap throwaway booster" concept. Saturn V launches cost three billion 2009 dollars. Each. Perhaps economies of scale and clever design could bring that cost down by 2/3. (I'm skeptical, but let's suppose.) Do you think you can get somebody to give you a whole gigabuck just to land a few thousand pounds on the moon? Never mind the hundreds of launches it would take to do anything serious, like build and supply a permanent moon base or mount an interplanetary expedition.

      It goes against all reason to assume that littering the Atlantic ocean with billions of dollars worth of debris is the most cost-effective way to get into space. The idea never would have gained traction, except in an administration that loved to make grand plans, but always dodged cost issues and had no capacity for thinking through the consequences.

    3. Re:Air is not enough. by lgw · · Score: 1

      My point is: government isn't going to change it's nature. Reusable components have proven more expensive than one-shot components in the real world, for reasons that may have nothing to do with engineering (perhaps the components need to be reworked in a ridiculous location to get money for that to go to the state os a key senator - something must explain that the size of the boosters was limited to the size of a particular train tunnel).

      There's actually nothing in an early-stage booster that is inherently expensive. The materials technology is old hat now, and while there's extreme benefit to lightening the structural elements of the part that goes into orbit, there's small benefit to lightening the structural elements of the first stage. If we had 1000s of launches, economy of scale would take care of making these low-tech parts cheap.

      --
      Socialism: a lie told by totalitarians and believed by fools.
    4. Re:Air is not enough. by fm6 · · Score: 1

      Your post makes no sense. Governments waste money, therefore disposable boosters will always be cheaper? I simply don't see the connection.

    5. Re:Air is not enough. by lgw · · Score: 1

      No, governments waste money in *particular ways*. The actual, real world costs of reusable vs disposable boosters can be compared, and the disposables win. I attribute the difference between the naieve engineering expectation of cost and the reality to political tomfoolery.

      "Always" is a long time, and of course this may change, but it wouldn't be an *engineering* change.

      --
      Socialism: a lie told by totalitarians and believed by fools.
    6. Re:Air is not enough. by fm6 · · Score: 1

      The actual, real world costs of reusable vs disposable boosters can be compared

      From one attempt to design a reusable vehicle? In a project that everybody agrees was poorly planned?

      Sorry to get personal, but that's one of the stupidest argument I've even heard.

  37. Buck Rogers by SnarfQuest · · Score: 1

    Yea! We get the Buck Rogers rocket ships that land on their fins. Do we also get the evil galactic empires too? And the super-weapons of EE Doc Smith?

    --
    Who would win this election: Andrew Weiner vs Andrew Weiner's weiner.
  38. Is it just me... by camperdave · · Score: 1

    Is it just me, or does this thing look a lot like the Orion module? Hmm... first the Buran which looks like the shuttle, now this thing that duplicates Orion. The Russians should try their hand at making a small, passenger only ship, like the HL-20 or the X-38, or the Mig Spiral.

    --
    When our name is on the back of your car, we're behind you all the way!
  39. For Mars? by Anonymous Coward · · Score: 0

    Since you can't use parachutes on Mars (atmosphere too thin, craft with crew too heavy), this could potentially be reserved for landings on Mars, right?

  40. "Belgien" by Charles+Dodgeson · · Score: 1

    In most languages copulation isn't an expletive.

    Where did you come up with that factoid?

    A native German speaker told me that the worst he could think of was "Go to the Devil", in Deutch.

    Surely you must know that the strongest taboo word in German is Belgien.

    --
    Prime numbers are exactly what Alan Greenspan says they are -S. Minsky
  41. Re:"unprintable expletive" by Anonymous Coward · · Score: 0

    As opposed to simply being your new insult of choice?

  42. Synchronize by djdbass · · Score: 2, Interesting

    I don't know the first thing about rocket science, so let me ask the crowd here.

    How do you synchronize the firing of 12 solid fueled rockets?

  43. Re:"unprintable expletive" by Anonymous Coward · · Score: 0

    Your poofy lvl80 point and click is no match for my AWP.

  44. Usable by Idiomatick · · Score: 1

    I think while this is fairly useless for landing on earth. It could be more useful for landing on other planets. If we are landing on a planet without much atmosphere or some harsh environment parachutes could be rendered useless. Ignoring that repacking parachutes outside of a cleanroom using robots is not really done. So parachute re usability is down. As well parachutes do not allow you to chose a very specific landing point even here on earth where we know pretty much everything about the wind. As well most of the parts involved in retrorockets are already in the spacecraft or would be in a good future design. The only lost space/additional mass is in the fuel itself (which IS a lot).

    I don't think it is a very useful idea NOW. But in future spacecraft or more likely with future propulsion systems it could be. As odd as this sounds firing your rockets at insanely precise amounts and angles with thousands of recalculations a second could be simpler than using a parachute.

    As well, the downside many people mention of noplanb is silly. If parachutes don't deploy sure you have more time to think about it but you are still going to impact the earth fast enough to liquefy your body. I don't see why it matters if your death is decided at 10km in the air or 1km. The pieces of ship remaining would be slightly larger that is about it.

    Also this is old tech. I played lunar lander yearrrrs ago.

  45. Re:"unprintable expletive" by Anonymous Coward · · Score: 0

    And illness. In Dutch, Kankerman (Cancer Man) is a pretty bad insult.

  46. A precision landing with solid rockets? by roystgnr · · Score: 3, Insightful

    Don't get me wrong, I'm all in favor of spaceships landing on a tail of fire, "the way God and Robert Heinlein intended!" But rocket-powered landings on Earth are a questionable engineering decision even when you get to reuse some of the liquid-fueled rocket engines that you already needed for liftoff and already wanted to recover intact. If you instead have to add extra weight to your upper stage for single-purpose solid rockets of lower ISP, it seems even more dubious.

    And that's before you get into the issue of "solid rockets" and "precision". Even designing a liquid-fueled rocket with adequate throttle control for a gentle landing isn't easy. (It's like brain surgery! Or possibly like some other appropriate metaphor!) But at least throttling liquid fuel consumption rates is possible. Solid rockets basically have just three settings: "off", "on", and "kaboom".

    1. Re:A precision landing with solid rockets? by roystgnr · · Score: 1

      liquid-fueled rocket engines

      Let's say "liquid-propellant rocket engines" instead. In a paragraph contrasting spaceflight "the way God and Robert Heinlein intended" to "rockets of lower ISP", it was almost sacrilegious of me to assume that even the former would be wholly chemically fueled.

    2. Re:A precision landing with solid rockets? by Walking+The+Walk · · Score: 1

      But at least throttling liquid fuel consumption rates is possible. Solid rockets basically have just three settings: "off", "on", and "kaboom".

      That's what I thought as well - you can't turn off a solid fuel rocket once it's light, right? So what happens if they produce too much thrust while braking, and send you up again?

      --
      A recursive sig
      Can impart wisdom and truth
      Call proc signature()
    3. Re:A precision landing with solid rockets? by dave562 · · Score: 1

      Oh come on, this one is easy. You give the cosmonauts a trigger that they can use once they land. When they use the trigger, it pops the TOPs off of the retro-rockets and the rest of the propellant burns upward. Then the capsule looks like a big, Fourth of July fountain. But since they are Russians, I guess it would have to be a May Day fountain? Maybe they can just partner with the Chinese, since those guys make all of the fireworks anyway.

    4. Re:A precision landing with solid rockets? by Sinical · · Score: 1

      This is only "kinda true". I worked on a program that started with a variable thrust solid rocket motor. It was eventually discarded: I don't know all the details, but I think the overall thrust was too low to give us the range we required. However, ditching it did require substantial navigation changes for shorter range flights so as to keep terminal velocity within the required limits, i.e. without being able to throttle down we had to pull wacky manuevers to bleed velocity. I don't know how much is public, so I'll just stop there and state: yes, variable thrust solid rocket motors at least tentatively exist.

      But you're right, I find it unlikely that they'd be suitable for the given application.

    5. Re:A precision landing with solid rockets? by roystgnr · · Score: 1

      Thanks for the info; I figured the word "basically" was probably concealing some exceptions. If nothing else, you could always use a variable nozzle or a set of vectorable nozzles to (somewhat) control the thrust you get from an invariant rocket burn... but that would add complexity and (in this case) further reduce specific impulse.

  47. I can read Russian by Anonymous Coward · · Score: 0

    My mother was a saint you bastard!

  48. Just like God and Robert Heinlein Intended by The+Shootist · · Score: 1

    Takes off and lands straight up and down?

    Just like God and Robert Heinlein intended. Huzzah!

  49. 2174.749 f/s by starglider29a · · Score: 2, Interesting
    Based on this NASA app: http://www.grc.nasa.gov/WWW/K-12/airplane/termv.html
    • The Apollo Command Module weighed 12773lbf/5806 kg, but the app only takes 10000 lbf.
    • Diameter of 3.9m, 12' 10" yields frontal area of 128.5 square feet.
    • WILD A55 guessing the Drag Coefficient at 1.0 (based on the page: http://www.grc.nasa.gov/WWW/K-12/airplane/shaped.html)
    • Dropping from an altitude of 100000ft (ha!)

    2174.749 f/s SOMEONE has the wrong terminal velocity. Are we sure this isn't a way to eliminate political dissidents?

  50. Re:"unprintable expletive" by pohl · · Score: 1

    In American english we have things like "God damned pig buttfucker"

    --

    The "cue the foo posts in 3, 2, 1..." posts will commence with no subsequent foo posts in 3, 2, 1...

  51. Buran ( The Soviet Shuttle) by Anonymous Coward · · Score: 0

    could take-off from the ground with its own power. It was
    also fly-by-wire.

  52. Thunderbird 3 by Smivs · · Score: 1

    So what? Thunderbird 3 (and 1 come to that) did this way back in the '60s.

  53. Re:"unprintable expletive" by dwiget001 · · Score: 3, Funny

    Had a friend of mine that was Lithuanian. She told me that they had no curse words.

    About the worst thing you could say to someone in Lithuanian was, translated to English: "I hope your rabbit gets mange!"

    Scary words, those.

  54. Re:"unprintable expletive" by JustOK · · Score: 1

    Poutine! Nothing worse.

    --
    rewriting history since 2109
  55. Hmm by egork · · Score: 1

    how does launching site location limit landing landing location?

  56. Re:"unprintable expletive" by Abreu · · Score: 1

    I once heard a Spaniard curse:

    "Me cago en las tetas de la Virgen MarÃa para que el niño JesÃs coma mierda!"

    It doesnÂt have sex or animals, but the double dose of religion makes up for it

    --
    No sig for the moment.
  57. Re:"unprintable expletive" by Abreu · · Score: 1

    Damn you Slashdot and your lack of UTF-8 support! ...dang, that was an unprintable expletive, allright

    --
    No sig for the moment.
  58. I thougt by codepunk · · Score: 2, Interesting

    I thought the Ruskie's where smarter than that, sounds like something nasa would propose. Russia has always had a successful space program
    because they use well tested and simple engineering. Just a capsule it goes up and parachutes back to the ground, no wings no crazy rocket
    assisted landing. The higher the component count and complexity the more room for failure.

    --


    Got Code?
  59. Re:"unprintable expletive" by Anonymous Coward · · Score: 0

    I'm a Night Elf Mohawk. Bring it bitch!

  60. Re:"unprintable expletive" by Jah-Wren+Ryel · · Score: 1
    --
    When information is power, privacy is freedom.
  61. Re:"unprintable expletive" by Anonymous Coward · · Score: 0

    In Dutch it is also common to swear with diseases. Common ones are typhus ('tyfus'), tuberculosis ('tering') and cancer ('kanker'). They can be used as expletives or as adjectives. In the latter case this can either mean that the speaker is unhappy with something ('teringweer', tuberculosis weather) or it can be a superlative ('kankergroot', cancer big, i.e. very large). The superlative use is only common around Rotterdam and The Hague, however.

    This is probably an aspect of the Dutch language that comes across as very awkward and uncivilised to non-natives.

  62. I've got a better name for it... by hyades1 · · Score: 1

    Might I suggest that the Russians call the new system the "Spacecraft Precision Lander And Transporter". The name might not be the greatest, but the acronym says it all.

    --
    I've calculated my velocity with such exquisite precision that I have no idea where I am.
  63. Re:"unprintable expletive" by troll8901 · · Score: 1

    5- Mother (for Chinese insults) (sometimes plus other elders too)

  64. Splat by caller9 · · Score: 1

    I feel bad for the guy that cleans the people soup this makes in the crater.

    Ron White might say. This will take them all the way to the crash site.

  65. Re:"unprintable expletive" by dunkelfalke · · Score: 1

    Huh?
    "Go to the devil" is probably the mildest expletive either in German and in Russian.

    By the way, the word for "to fuck" in russian is "yebat'" and is indeed considered unprintable.

    --
    "It's such a fine line between stupid and clever" -- David St. Hubbins, Spinal Tap
  66. Re:"unprintable expletive" by mpiktas · · Score: 2, Informative

    Not exactly. Half of the list are just ordinary words with negative meaning. Lithuanian really lacks strong swearwords of lithuanian origin. So we import the majority from russian, some from polish. But this does not mean that lithuanians swear in foreign language. Usually some description is combined with foreign swearwords to make a satisfactory expletive. The curious side effects of this is that lithuanians can understand perfectly russian swearing, but not vice versa, and that some really bad russian swearwords sometimes can pass just as a salty language. Sometimes I really envy other languages for having original swearwords, lithuanian ones for some reason vanished. I really doubt that they never existed.

  67. Re:"unprintable expletive" by mpiktas · · Score: 1

    I strongly suspect that russian name for men genitalia was used. Russians can say a whole sentence, which of course is unprintable, using only this word :)

  68. Re:"unprintable expletive" by dunkelfalke · · Score: 1

    there is an old russian joke going along the lines of:

    - What's the name of your cute doggie, little girl?
    - Boar.
    - Why's that?
    - He fucks pigs.

    --
    "It's such a fine line between stupid and clever" -- David St. Hubbins, Spinal Tap
  69. Runway by Anonymous Coward · · Score: 0

    Being able to hit the runway every single time seems like good precision to me.

    please type the word in this image: excrete

  70. Fuel by tsotha · · Score: 1

    There are all sorts of programs, both government and commercial (or, more accurately, hobby-companies of wealthy people), that have proven the tail-first rocket landing approach can work reliably. The question is do you want to carry all that fuel into orbit so you can burn it on the way home. From what I understand, since fuel is the major weight component for a rocket as you start your landing burn the ship weighs almost nothing compared to launch, so it's not as big a drawback as you'd think.

  71. Re:"unprintable expletive" by eleuthero · · Score: 1

    Sometimes I really envy other languages for having original swearwords, lithuanian ones for some reason vanished. I really doubt that they never existed.

    Couldn't it just be that the Lithuanian "think of the children" movement is just slightly stronger and older than any of us previously thought?

  72. Re:"unprintable expletive" by theolein · · Score: 1

    In German you can say "Fuck you" (Fick Dich) and even Motherfucker (Mutterficker), and it is a pretty bad insult, but the usual nasty German ones revolve around crap and piss: "Bekacktes Arschloch" - "shit covered arsehole" will makeyou friends all over the place, and "Pisser" (no proper translation) will save you teeth extraction fees at the dentist.

  73. Two birds one stone by le_sean_moon · · Score: 1

    Why don't they just attach a big drill to the front of it, and it can drill a new oil well as it lands?

  74. Deployment Height Seems Wrong by Gallomimia · · Score: 1

    Lots of math regarding the impulse required to slow said spacecraft to a speed worthy of using retros to attain a near stationary speed and land slowly with all cosmonauts alive and... well just alive.

    Let's consider one more thing that simply may not add up: the speed of the capsule when its rockets are fired. How fast is a vehicle under re-entry speeds moving when it reaches the altitude of 800-600 meters? If the margin of error is in fact 200 meters like the difference between 800 and 600 suggests, will this not leave only seconds between knowing there is an emergency situation and calling for the recovery crew to get out their egg flippers to pick up what's left of the cosmonauts?

    --
    Sadly, a Libertarian cannot force his views on another, and freedom cannot spread as does the cancer known as religion.
  75. Re:"unprintable expletive" by shutdown+-p+now · · Score: 1

    What is the russian translation for fuck?

    It strongly depends on whether it's used as a noun, adjective or verb, as well as on the specific context; i.e. "fuck off", "fuck up", "fuck over" etc translate to different Russian words, though normally with one of the two basic roots: "houy", a vulgar word for "penis", and "yeb", ditto for "copulate".

    On a side note, the latter one is actually recognizable Proto-Indo-European root for the very same thing - "eib" - so you could say that Russian vulgarities are among the most ancient (though the same goes for other Slavic languages, most (all?) of which also retain the same or similar root for such purposes).

  76. Re:"unprintable expletive" by John+Bayko · · Score: 1

    My profanity of choice is "flocon de mais!", which sounds very bad to anyone who doesn't understand French, but translates to "corn flakes!".

  77. Poor Delta Clipper... by tlambert · · Score: 1

    Poor Delta Clipper...

    Passed over in favor of a plane-like vehicle that would need runways to take off and land, and which had fuel tank requirements which were technically impossible. Looks like the government made the right choice of contractor on that one... the only thing the space-plane design had going for it was the linear aerospike engine, which the DC-X could have had as well, if not for the patent issues.

    Here's hoping China or some other country that ignores US patents puts together a VTOL SSTO craft like the DC-X with all the pieces that can't be put together for the next 20 years because of patents that aren't being used for anything, and then builds enough of them that we can start buying them used.

    -- Terry

    1. Re:Poor Delta Clipper... by hitmark · · Score: 1

      or that someone up top gets the bright idea of either canceling or buying out the patent(s) in question for the good of everyone...

      --
      comment first, facts later. http://chem.tufts.edu/AnswersInScience/RelativityofWrong.htm
  78. Science finally catches up... by roc97007 · · Score: 1

    ...with 1950's science fiction. Isn't it grand!

    --
    Oliver's law of assumed responsibility: If you're seen fixing it, you will be blamed for breaking it.
  79. So what if the rockets fail by blackpaw · · Score: 1

    "... what was going to happen to crew members unlucky enough to encounter a rocket engine failure a few seconds before touchdown."

    Every considered what happens if the Parachutes fail?

  80. It sounds okay by Kingrames · · Score: 1

    It sounds like it will work until you put yourself into this situation:
    You're floating in space, and this really really big, multi-trillion ton rock is being thrown at you.

    Now, just turn yourself around and fire your rockets until you can land on the rock being thrown at you without breaking yourself.

    --
    If you can read this, I forgot to post anonymously.
    1. Re:It sounds okay by Tacvek · · Score: 1

      The earth is not a multi-trillion ton rock (i.e. a multi gigaton rock) it is a multi zetaton rock (i.e. a multi yottapound rock).

      --
      Stylish sheet to fix many problems in Slashdot's D3: https://gist.github.com/801524
    2. Re:It sounds okay by Anonymous Coward · · Score: 0

      It sounds like it will work until you put yourself into this situation:

      You're floating in space, and this really really big, multi-trillion ton rock is being thrown at you.

      Now, just turn yourself around and fire your rockets until you can land on the rock being thrown at you without breaking yourself.

      -Now, just turn yourself around and fire your rockets until you can land on the rock being thrown at you without breaking yourself.

      -Now, just turn yourself around and shoot out a piece of cloth until the atmosphere of the rock slows you down enough to land on the rock without breaking yourself.

      -Now, just turn your belly toward it and allow friction/air resistance and your wings to glide you to a slow enough speed to land without breaking yourself.

  81. Re:"unprintable expletive" by Anonymous Coward · · Score: 0

    > What is the russian translation for fuck? Babelfish doesn't translate it...

    [yebAts]

  82. Re:"unprintable expletive" by Trent+Hawkins · · Score: 1

    What is the russian translation for fuck? Babelfish doesn't translate it...

    yob, but it's not used quite in the same way as fuck. hui (or in Russian) is probably what you're looking for.