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CEV Revolutionary Gimballed Thrusters

simonbp writes "A Tennessee Tech Professor has proposed an innovative gimbal mount for 'inclusion to the design of [NASA's] CEV (Crew Exploration Vehicle), revolutionizing the vehicle's RCS (Reaction Control System) and solar panel orientation capabilities.' This will allow for nimble maneuvering and for the solar cells to maximize power production."

71 comments

  1. What's the symbol? by Anonymous Coward · · Score: 0

    What's the symbol for a nimble gimbal??

    1. Re:What's the symbol? by ScrewMaster · · Score: 1, Insightful

      I dunno ... but it fits in a thimble. I think a guy named Kimball invented the nimble gymbal that fits in a thimble, and I believe he lives on the ice shelf Fimbul and plays the cymbal.

      --
      The higher the technology, the sharper that two-edged sword.
    2. Re:What's the symbol? by Anonymous Coward · · Score: 1, Informative

      How many thimbles full of Kimball's nimble-gymbal symbol would it take to assemble a cymbal-playing gymbal in Fimbul? Simple.

    3. Re:What's the symbol? by saifatlast · · Score: 1

      I like how this is modded insightful. Yay slashdot!!

      --
      note: i'm known as plugwash most places but i screwd up registering that here somehow in the past and now can't regist
    4. Re:What's the symbol? by ScrewMaster · · Score: 1

      Yeah ... kinda took me by surprise too.

      --
      The higher the technology, the sharper that two-edged sword.
  2. the russian wessels by User+956 · · Score: 1

    Didn't the Soyuz 11A511U have Gimballed Thrusters?

    --
    The theory of relativity doesn't work right in Arkansas.
    1. Re:the russian wessels by Anonymous Coward · · Score: 0

      I would think the thing about fixed thrusters is the training involved in understanding how to control the space craft. These principles are well understood. The problem with the gimble mounted is you are at the whim of the control software. If there is a malfunction then it becomes a fly by the seat of your pants approach. It is much harder to fly the spacecraft if you have to compensate for unknown angles of the thrusters. Even if you have a readout of the angle you must discover the properties of the craft and use trial and error to regain control. Not a very good method in an emergency. If you don't get it correct the first time, you could end up denting whatever you are near or worse. Remember the russian space station and that cargo vessel. Ooopsie.

    2. Re:the russian wessels by Muad · · Score: 1

      I share the concerns you mentiond - particularly because just the cost of re-learning the performance of the RCS, in terms of fuel wasted, would be prohibitive and way more dangerous than the risk of impacting something.

      Your analogy with the progress collision with Mir is, however, flawed - it had nothing to do with gimbals, as the capsule DOES NOT have gimballed RCS, the first stage of the rocket does.

      to the original poster, I must note that the soyuz roket variant you pointed to used gimballed vernier thrusters, which are not exactly a reaction control system of the same type mentioned here, they are used to orient the rocket in athmospheric flight.

      --
      --- "I didn't think anyone would understand it" -Prof. Bob Muller
    3. Re:the russian wessels by Dun+Malg · · Score: 1
      Didn't the Soyuz 11A511U have Gimballed Thrusters?

      Indeed, as was the Rocketdyne J-2 on the Apollo command module. Both the Soyuz and Apollo thrusters are main engines. These gimballed thrusters are for the Reaction Control System, used for fine positioning and attitude control. RCS thrusters have traditionally been fixed, rather than steerable.

      --
      If a job's not worth doing, it's not worth doing right.
    4. Re:the russian wessels by Anonymous Coward · · Score: 0

      I understand what you are saying. However.
      My analogy was not related to whether the progress spacecraft had gimballed reaction jets, but rather the dangers of errors when in close proximity to another object in space.
      Spacecraft are delicate beasts. Not like a car but more like a pop can made of tinfoil. A three mile an hour crash could easily destroy both craft. However again I'm refering to close in manouvering. My main point is how do you control with malfunctioning position of gimballed jets that you don't know where they are pointing. On top of that you now don't know their relation to the centre of mass of your craft in that event. At least with fixed reaction jets you always know that relationship even if something goes wrong with a thruster. Therefore you must conclude that recovery will be significantly longer and this maybe time you just don't have available. Hard to train for that.

    5. Re:the russian wessels by tgrockhead · · Score: 1

      Not to be completely anal, but the conical command module was essentially the capsule that returned to earth. The cylindrical service module (where the infamous LOX tank exploded on Apollo 13) had the gimballed J-2. Otherwise, right on.

  3. Gimbal? by iopha · · Score: 3, Informative

    If you're like me and are wondering what the heck a gimbal is, wikipedia has an article. Not being an engineer, I still only have but the fuzziest idea of what's going on here; blame a liberal arts background.

    1. Re:Gimbal? by interiot · · Score: 4, Informative
      Better is wikipedia's Gimbaled thrust and the NASA pages it points to.

      (funny, I was just reading that before coming to slashdot... even better is the semi-related water rocket page.... awesome stuff)

    2. Re:Gimbal? by AndroidCat · · Score: 1
      So, it's not what slithy toves do in wabes?
      'Twas brillig, and the slithy toves
      Did gyre and gimble in the wabe:
      All mimsy were the borogoves,
      And the mome raths outgrabe
      --
      One line blog. I hear that they're called Twitters now.
    3. Re:Gimbal? by murderlegendre · · Score: 1

      For the most part, you Liberal Arts types need only concern yourselves with one type of joint.

      To be blunt.

      --
      There's a Starman, waiting in the sky / He'd like to come and meet us, but he hasn't got the time.
    4. Re:Gimbal? by User+956 · · Score: 1

      If you're like me and are wondering what the heck a gimbal is, wikipedia has an article.

      Wikipedia says a Gimbal is "a type of coin-operated arcade game where a player attempts to score points by manipulating one or more metal balls on a playfield inside a glass case. " Well, looks like I've learned something today!
      Excellent!

      --
      The theory of relativity doesn't work right in Arkansas.
    5. Re:Gimbal? by Anonymous Coward · · Score: 0

      I thought they were the rival store that Macy's wouldn't tell.

    6. Re:Gimbal? by Pollardito · · Score: 1
      there's one spot in that article that is in-error, but i don't know enough about rockets to be able to correct it :
      In the case of super-roc or backgliding rockets, the centre of gravity and the centre of gravity are as close as possible, so it spins around, which slows down it's descent.
      not sure how to make note of this on Wikipedia itself, do you just edit the discussion page?
    7. Re:Gimbal? by corngrower · · Score: 1
      Gee none of the wikipedia articles does a very thorough job of explaining gimbal or gimballed thrust. The joint has two degrees of freedom, like your shoulder joint or hip joint. The thrust of the rocket is directed along a line through the center of the nozzle, or very nearly so. If the line along which the thrust is directed goes through the center of mass of the rocket, the rocket goes straight. If it doesn't go through the center of mass of the rocket, the rocket experiences a torque, which will cause the orientation or direction of the rocket to change.

      The article mentions that the gimballed thrusters will be used for the reaction control system on NASA's CEV. This implies that the thrusters will be able to gimball by more than just the few degrees that the main engines are able to gimbal.

    8. Re:Gimbal? by brian0918 · · Score: 1

      "Better is wikipedia's Gimbaled thrust and the NASA pages it points to."

      I just started this page a few hours ago! Must be a new record for wiki-to-slashdot linking.

    9. Re:Gimbal? by Anonymous Coward · · Score: 0

      I think it should be "centre of pressure".

    10. Re:Gimbal? by ultranova · · Score: 1

      If you're like me and are wondering what the heck a gimbal is, wikipedia has an article. Not being an engineer, I still only have but the fuzziest idea of what's going on here; blame a liberal arts background.

      Do you know the small motorboats, where the boats direction is controlled by turning the engine so it pushes the back of the boat to the side instead of straight forward ? According to the Wikipedia article, the gimbal is a device that lets a rocket do the same.

      In other words, a gimballed rocket can be steered.

      --

      Forget magic. Any technology distinguishable from divine power is insufficiently advanced.

    11. Re:Gimbal? by dhakbar · · Score: 1

      TRINITY FTW!

      It's been years since I've thought of that game.

  4. Video Model. by Anonymous Coward · · Score: 0

    Here is a video model of the joint in action. Frankly, I can't help thinking of a Rube Goldberg machine when I look at it.

  5. I will think you will find... by Skiron · · Score: 1

    ... MS owns the copyright to the word 'innovative'. They will be releasing this new design in 6 months after copying it.

  6. Wow...Old News Is So Exciting! by tpconcannon · · Score: 1

    The original CSM had gimballed engines. So they announced they are going to do the same damn thing that they did in the 60's? Snore.

    --
    I found the "Any" key.
    1. Re:Wow...Old News Is So Exciting! by lax-goalie · · Score: 1

      The main SM engine was gimballed. The RCS system wasn't.

    2. Re:Wow...Old News Is So Exciting! by shmlco · · Score: 2, Informative
      From TFA: "four single RCS thrusters, placed 90 degree apart around the circumference of the service module, with the ability to direct thrust to any direction in a hemispherical motion, replacing - and capable of even more manoeuvres than - the current four groups of four (16 in total) body-fixed thrusters."

      And I'm pretty sure the orginal CSM did not have a gimbled engine. The Saturn did, but with no where near the same range of motion as being discussed here.

      --
      Any sect, cult, or religion will legislate its creed into law if it acquires the political power to do so.
    3. Re:Wow...Old News Is So Exciting! by georgewilliamherbert · · Score: 2, Interesting

      It's standard practice to gimbal the main engines in a launch vehicle, or an upper stage. That gives you pitch and yaw (and sometimes, if you have 2 or more engines, roll) orientation control while you're under thrust from those main engines, without having to use the smaller RCS engines as well.

      Other ways of doing it include using a RCS anyways, with fixed main engines; putting vanes or paddles in the main engine exhaust stream but keeping it fixed; using aerodynamic control fins (only works in an atmosphere during certain speed ranges, useless at liftoff or in space); injecting a liquid or gas into the main rocket engine nozzles on one side but not the other, to give side thrust (LITVC or Liquid Injection Thrust Vector Control, though it can technically use gas as well).

      It is not standard practice to gimbal the reaction control system used in space. The assumption to date has been that the four fixed quads approach gives the best reliability under circumstances where part of the system suffers a failure. If you lose one of these oriented thrusters (stuck actuator or thruster fails) then it's like losing a whole standard quad, in terms of the vehicle's remaining dynamics. Lose two, and your maneuverability is severely impaired.

    4. Re:Wow...Old News Is So Exciting! by TubeSteak · · Score: 1

      While TFA may say "with the ability to direct thrust to any direction in a hemispherical motion" the video only shows the thrusters being fired in 4 directions... the same directions a normal pod would be thrusting.

      --
      [Fuck Beta]
      o0t!
    5. Re:Wow...Old News Is So Exciting! by HermanAB · · Score: 1

      AFAIK the Saturn 5 rocket had gimballed thrusters. Gawd knows why this is revolutionary now. When and why did JPL stop using gimballs?

      --
      Oh well, what the hell...
    6. Re:Wow...Old News Is So Exciting! by tgrockhead · · Score: 1

      All of the main engines on the three stages of the Saturn V, along with the main engine on the Service Module were mounted on gimbals, as are the three main engines on the Shuttles. I suppose the LEM used similar technology, but I don't feel like checking. Each of the RCS thrusters on the Service Module consisted of four nozzles at 90 angles. For Apollo geeks/modellers, here's a site absolutely loaded with detail shots of the Saturn V, including gimbals; http://www.apollosaturn.com/

    7. Re:Wow...Old News Is So Exciting! by tgrockhead · · Score: 1

      Stupid ME! As noted elsewhere in this thread, the CSM (command service module) J-2 main engine was not gimbaled.

  7. Woops! Video Model. - Working Link. by Anonymous Coward · · Score: 1, Informative

    Sorry! Slashcode diddled the spaces in the URL.

    Here's the working link.

  8. Where's Pravna? by Anonymous Coward · · Score: 0

    Starbuck: "Where's Pravana? He's gotta fix that fraakin gimbal or I'm gonna have his ass"

    Tyrol: "He's dead"

    Starbuck: "How many did we lose in the attack?"

    Tyrol: "85"

  9. Connecting Hoses by qualico · · Score: 1

    There are a couple of weak links to this solution, but nice design none the less.

    The connecting joints and hoses will be subject to flex failure.
    No doubt they will use appropriate materials to counter repetative wear.

    Also, as with most space equipment, they will most likely make a redundant system.

  10. Hm.... by inphizzible_friend · · Score: 0

    Any chance of harnessing this space-age technology to use here on earth?

    --
    Women- the final frontier...
    1. Re:Hm.... by AndroidCat · · Score: 1

      What are you going to use gimballed thruster on, your flying car?

      --
      One line blog. I hear that they're called Twitters now.
    2. Re:Hm.... by inphizzible_friend · · Score: 0

      I was actually hoping for an alternative to, "Choco-Lax"

      --
      Women- the final frontier...
    3. Re:Hm.... by corngrower · · Score: 1

      Not a snowball's chance under a powered F1 engine.

  11. Gimballed thrusters? by Saiyine · · Score: 2, Funny


    Gimball looks to me like a perfectly cromulent word!

    --
    Hosting 20G hd, 1Tb bw! ssh $7.95
  12. This is front page news? by drsquare · · Score: 0, Troll

    The original shuttle had gimballed engines, now they're using it for the RCS as well? Big fucking deal. May as well post an article about how the toilet's going to have a different colour of soap.

    The original design with millions of RCS thrusters all over the place was stupid anyway.

  13. Link to actual animation by Animats · · Score: 5, Informative
    If you don't want to plow through all the blogodreck and registration, here's the animation of the Canfield joint (quicktime).

    As a rocket engine gimbal, this doesn't look promising. It's a rather bulky mechanism; the linkage is much larger than the engine bell. It requires fifteen bearings, not including the three motors. The standard solution, a gimbal ring arrangement, only requires four. The bearings also have to handle off-center loads, never a good thing. Bearings in space are headaches; lubrication is tough and temperature changes can jam them.

    The motors are in a weak position from a leverage standpoint; the engine thrust is applied directly to the motor shafts, so they (and their gear trains) must be strong enough to overpower the thruster. In a gimbal ring arrangement, the bearings are usually placed so that the center of thrust is at the center of the gimbal, so that the bearings, not the actuators, take almost all the thrust. Very large engines, like the Space Shuttle and Saturn V main engines, have been successfully gimballed that way.

    The three motors don't seem to add redundancy; it looks like they all have to be working.

    For comparison, here's a simple gimbal from Amadillo Aerospace, Carmack's rocket program.

    In reality, having many fixed reaction thrusters is probably more reliable than have a few steerable ones. Fewer moving parts.

    1. Re:Link to actual animation by TubeSteak · · Score: 1

      Ummm.... the quicktime video you linked to looks nothing like the video they have on the nasaspaceflight.com website.

      The 3 movable arms look more like two sevens (7) that got mashed together along the flat part.

      Here's a screenshot (modified with my crazy mspaint skillz)

      I assume the rest of what you said still stands though.

      --
      [Fuck Beta]
      o0t!
    2. Re:Link to actual animation by Animats · · Score: 2, Informative
      Different animation, and a different version of roughly the same klunky mechanism. Better bearing mounts, though. That one you could actually build.

      The motors seem to be right out of the Maxon catalog, with the planetary gearhead option on one end and the encoder on the other. Those are good motors (we used one to steer our DARPA Grand Challenge vehicle), but they are not rated for spacecraft operation.

      Here's an Aeroflex gimbal that actually is used in space to steer a thruster. Note how the rotational axes go through the line of thrust, and how big and solid the bearing blocks are, compared to the proposed design.

    3. Re:Link to actual animation by Dale+Dunn · · Score: 2, Informative

      The basic mechanism shown is basically the same.

      What I don't like about this idea is that the thrust seems to be carried by the actuators holding their position. Come to think of it, they're using 3 actuators to accomplish 2 degree of freedom motion. Great. Armadillo's gimbal doesn't have these problems, but it does have a very limited range of motion in comparison.

      It's not difficult (I just did it) to imagine a gimbal with the same or better range of motion, loads not significanlty carried by motors, no hoses (rotary seals), and only two actuators. The weakness in my idea is the need for a set of somewhat large diameter bearings. It's just a trunnion on a swivel base.

      What problem is this gimbal supposed to solve in addition to the large range of motion in a space-rated package?

    4. Re:Link to actual animation by kurzweilfreak · · Score: 1

      Is it just me, or does the top left of the gadget bear a passing similiarity to the Napster cat-head logo?

      --

      kurzweil_freak

      5th Kyu Genbukan Ninpo/KJJR student

      Be the darkness that allows the light to shine.

    5. Re:Link to actual animation by Animats · · Score: 1
      trunnion on a swivel base.

      The trouble with a trunnion on a swivel base for this application is that it has a singularity around the straight position. Small changes of direction when pointed nearly straight require big changes in the swivel base position. For a thruster, you need to make small corrections quickly, with minimal actuator motion. (Think WWII antiaircraft guns, forced to slew around frantically when the attackers were overhead, usually missing the target at its point of closest approach.)

  14. Wikipedia definition way over specialised. by Flying+pig · · Score: 2, Informative

    Gimbals have been around since...well, if you believe Needham, at least the 10th Century AD in China. A gimbal is just a way of mounting something so it can rotate relative to something else while still being attached to it and moving linearly with it, and the main application has been on boats where equipment like lamps and compasses is suspended in mounts so it can swing. http://www.sailgb.com/p/captains_cabin_lamp/ is a picture of a small gimballed lamp. So long as the centre of gravity of the equipment is below the plane of the mount, the boat can rock underneath and the lamp, compass, cooker or whatever will stay more or less upright.
    By using an outer pair of pivots to hold a ring which then has another pair of pivots at 90 degress to which the equipment is attached, you get two axis gimbals which allow for rocking and for pitch, which is important on small boats. It isn't practical to suspend (say) a marine stove from a chain because it would swing all over the place, whereas suspending it from pivots near the top means that the base can swing a bit while the pans stay more or less in the same place.
    So all the stuff in Wikipedia about Euler angles is all very well, but a gimbal is just a way of allowing one thing to be attached to another while being able to rotate in one, two or three dimensions relative to it. There are various designs and obviously the Canfield one is a clever one, but there is nothing mysterious about gimbals themselves.

    --
    Pining for the fjords
    1. Re:Wikipedia definition way over specialised. by Anonymous Coward · · Score: 0

      Then why don't you stop bitching about it, and contribute to the article?

  15. A video of the actual joint by qbwiz · · Score: 1

    If you're just curious about what this new gimbal looks like, tntech.edu has a video showing how it works. Or, for those who don't like Coral cache, here's a link to the original site.

    --
    Ewige Blumenkraft.
  16. COOL concept by dolphin558 · · Score: 1

    I hope this idea is adopted. We're talking major cost and energy savings.

  17. There's a video by TubeSteak · · Score: 1

    The video illustrates exactly how the gimbal works.

    It's quite neat actually.

    Too bad the video is a few MB over 50, otherwise they could have coralized the link.

    I won't post a link here, because they say that they don't want their server to go down in flames.

    --
    [Fuck Beta]
    o0t!
  18. I'm pi$$ed. by Almost-Retired · · Score: 1

    I went to the site, where it says a video of the device in action can be seen at the link on the bottom of the page.

    But guess what friends, when you click on the link, you are rejected because you are not a friggin member.

    It might for all I know, be a great idea, but screw em and the camel that rode in on them.

    Whyinhell does Taco post these stories without checking them out for veracity?

    --
    No Cheers, Gene

  19. Your urine must be very precious. by Anonymous Coward · · Score: 0

    bugmenot.com

  20. thrusters and reaction wheels by Jeff1946 · · Score: 1

    Most vehicles in space use a combination of thrusters and reaction wheels. Essentually a flywheel on each axis is spun up or down to rotate the vehicle. Eventually the wheel is moving too fast and a thruster is used to spin the vehicle so that the wheel can be slowed down. For moving the vehicle it is important to have the thrust vector point at the CG of the vehicle, else a torque is produced causing spinning which requires an additional thruster to compensate. By the way the solid rocket boosters on the Space Shuttle are gimbled. As others have said simplicity and redundancy are important considerations in space design. Look up for example the Apollo Luner Orbiter engine design.

    1. Re:thrusters and reaction wheels by corngrower · · Score: 1

      I don't believe the nozzles on the solid rocket boosters of the Space Shuttle are gimbled. I believe they use a different mechanism for vectoring their thrust.

  21. Revolutionary? by hackwrench · · Score: 1

    Well you see, it revolves, so naturally "Revolutionary" was quick to come from that, and they kind of just went with the flow to get "innovative".

  22. Tried BugMeNot, and the login they provided by Ellis+D.+Tripp · · Score: 1

    was not working....

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  23. Because I'm not arrogant enough by Flying+pig · · Score: 1

    To think that I have any useful contribution to make to Wikipedia. That doesn't stop me trying to explain to someone who is not an engineer why he did not understand the wikipedia article. My rantings on slashdot are just trivial observations of day to day things with no lasting value. I certainly do not have the technical expertise or authority to contribute to an encyclopaedia.

    --
    Pining for the fjords
    1. Re:Because I'm not arrogant enough by Fulcrum+of+Evil · · Score: 1

      I certainly do not have the technical expertise or authority to contribute to an encyclopaedia.

      Yeah you do. Your example would be a useful addition to the Gimball entry - applications help flesh out the meaning of the thing.

      --
      "We returned the General to El Salvador, or maybe Guatemala, it's difficult to tell from 10,000 feet"
  24. I work in this lab. by docfreezzzz · · Score: 3, Interesting

    I am a Mechanical Engineering Undergraduate who attends TTU and does research for the department in which this design originated. I work in the lab where the device was first prototyped. Just as an FYI, the device is revolutionary because of the elimination of repetitive structures. Granted the bearing are an issue but the gimble can achieve a full 360 degree spherical change in attitude with only the use of 3 stepper motors. Nothing else does exactly that at this time. That's why the device is interesting to NASA. Think of replacing the current arrangement of 5 motors with just one. Can you say cost savings? Just thought I would post my 2 cents since I have had to demo the device on several occassions and have first hand experience with the mechanism. OUT

    1. Re:I work in this lab. by AJWM · · Score: 1

      The nice thing about repetitive structures is that they lead to cost reductions through volume manufacturing and assembly. They're also easier to train technicians to service.

      The nice thing about fixed quads for an RCS system is that their only moving parts are the valves -- pretty simple parts. Moving parts are failure points.

      The nice thing about multiple quads vs just a few gimballed thrusters is that they provide redundancy and backup for each other.

      But then NASA has always been in love with the complex solution that might save a few grams of weight, and require a few more engineers and technicians to manage it -- which return requires a few more managers to manage them, and so on...

      --
      -- Alastair
    2. Re:I work in this lab. by docfreezzzz · · Score: 2, Interesting

      It was meant more for small craft travel vector correction. Hence the attachment to CEV. Not main craft repetitive flights like the space shuttle. Sorry I gave that as an example but its something everyone can relate to. I do have to disagree with you in terms of your analysis of engineering economics however. How many space shuttles do you think they mass produce? Most parts are one offs from precision manufacturing facilities. The only parts which are repeat manufactured are SRBs and those are extremely simple. The dies and CNC code is what is costed most in manufacturing. The mass production just makes the profit/cost ratio more favorable to the consumer... aka NASA. If you only make 30 pieces. There really isn't a mass production method in place. And technicians are much faster at servicing one part instead of 4. That's part of the reasoning behind the system. We are talking about replacing multiple pieces with one piece therefore they still have the same learning curve for servicing the system. As for redundancy I do agree with you there. It is far safer to have a backup system. However, even with the multiple booster positioning systems in place today. If one fails entirely, there is still a serious impairment to the craft. They just don't send up unused pieces with a space vehicle. Weight costs money. Several grams can cost on the order of thousands of dollars to reach high earth orbit. Once again the system that weighs less wins especially with funding reductions in the program as of late. Just my 2 cents... ;) OUT

    3. Re:I work in this lab. by Anonymous Coward · · Score: 0

      I don't know why you bothered replying to that troll - it's not likely that he'll even bother reading your reply, and if he does, he'll find a reason why NASA are evil.

    4. Re:I work in this lab. by AJWM · · Score: 1

      The only parts which are repeat manufactured are SRBs and those are extremely simple.

      No, the SRB's are re-used (although "crashed and salvaged" might be more accurate). The ET's are disposed of and manufactured new for each flight.

      The dies and CNC code is what is costed [sic] most in manufacturing.

      Right, so it doesn't cost much more to build 30 than it does to build 5. Even if you're largely hand-building the things (vs using CNC), you still need dies and templates. Besides, with any halfway modern CADD system, the CNC codes are just another output.

      And technicians are much faster at servicing one part instead of 4.

      They're not talking about one part. One combustion chamber and nozzle, perhaps, but three electric motors and some hairy mechanical linkages and flexible plumbing, plus valves. That's a lot more to maintain than four simple chambers and nozzles and no moving parts except the valves.

      We are talking about replacing multiple pieces with one piece

      No, you're talking about replacing simple, rigid plumbing fixtures with something combining flexible plumbing and electric motors, adding at least five points of failure (3 motors plus flex fuel and oxidizer lines). More than that when you consider the linkages and failure points within each motor.

      (I'm not counting valves -- yes the gimballed only has one set vs a quad's four sets, but (a) valves are pretty simple and (b) design of 4-way series/parallel valves to allow fail-operational in case of a valve stuck open or a valve stuck closed has about 50 years of aerospace engineering experience behind it.)

      Several grams can cost on the order of thousands of dollars to reach high earth orbit.

      Well, we're talking manned ops, so low Earth orbit, not high Earth orbit. But yes, if you design to weight rather than designing to cost, stuff costs a lot more. There hasn't been a real operational need (vs engineering desire or habit) to design to weight since the Apollo program. (NB, obviously weight is a factor that can't be totally ignored, the mistake is making it the primary criterion rather than cost and safety. The Soviets/Russians had better heavy-lift capability from the start, so they never fell into that trap. That may have cost them the Moon, -- doing Moon direct or even Lunar Orbit Rendezvous is weight critical -- but they dominate LEO.) (Weight is less of an issue for the Moon if you're doing an Earth Orbit Rendezvous rather than trying to lift everything in one shot.)

      --
      -- Alastair
    5. Re:I work in this lab. by docfreezzzz · · Score: 1

      Remanufactured is a more approptiate term. I do apologize once again for my choice of language.

      Right, so it doesn't cost much more to build 30 than it does to build 5. Even if you're largely hand-building the things (vs using CNC), you still need dies and templates. Besides, with any halfway modern CADD system, the CNC codes are just another output.

      The original reply gave benefit to the current setup due to cost reduction through volume. My point was it isn't cost reduction through volume. I was not implying mass manufacturing is more expensive. Instead I was illustrating that due to current techniques in manufacturing, the benefits would only arrive after several hundred units were built. Not a plus for either side here. I just disagree with the cheaper by shear volume example.

      No, you're talking about replacing simple, rigid plumbing fixtures with something combining flexible plumbing and electric motors, adding at least five points of failure

      I do agree that complexity is not favorable in harsh environment applications. ie space. I was referring only the training necessary for service technicians. I never said that replacing the entire system with one unit was wise. In fact, I believe I point out the need for a failsafe. As for redundancy I do agree with you there. It is far safer to have a backup system.

      Several grams can cost on the order of thousands of dollars to reach high earth orbit.

      NASA has always been weight aware which is why so many satellites have been built twice. One is for operational checks and the light*expensive* version goes into space. Low launch weights are a necessity for monetary and equipment reasons. Personally, I think this system is far better suited to non-manned vehicles. Granted the proposal was for manned craft; however, the system doesn't seem well suited for that use. The system would need to be massive. Lighting the motor under launch conditions would be catastrophic due to the off axis loading on the single motor. I believe that high orbit or deep space flight is the only real use for the joint system. IMHO.

      Apologies if my post came across as vague. I was in a rush between meetings. The joint is a unique kinematic innovation of which I feel is greatly important. Our current method of sending things into low-earth orbit has worked well for many years and for good reason. 50 years of engineering practice as you say. I think the use of this technology lies farther out in our space ventures.

      OUT

  25. Design is a disaster by O2H2 · · Score: 4, Insightful
    The design is interesting in a sophomoric way. It is clearly designed by someone who has never had to qualify a device for spaceflight. Highly cantilevered, indeterminate stuctures with eccentric centroids and active mechanisms in the loads paths are terrible. I would give that thing about 60 seconds on a vibe table before it came to pieces. The use of flex hoses with such large motions is also a really bad idea- expecially when they have to flex in multiple axes at once- there is no practical solution to make such a fluid connection last more than a few thousand cycles under cryogenic conditions under the 300 psig pressure conditions that are planned for CEV propulsion. As someone who DOES design such things on a daily basis I give it a D- for practicality, cost and reliability/redundancy.

    Also the control valving is highly decoupled from the combustion chamber which means high dribble volume and terrible min Ibit. Those simple stepper motors also have to operate at 165R for prolonged periods- this denies you most lubricants and requires special resolvers and the like. There is also no way that such a mechanism can deliver the frequency response of multiple small thrusters pointed in multiple directions. There is also the need to interface either a fiber optic or high voltage spark igniter lead to the thruster across large motions- could be a problem for the non-optical approach.

    The issue is : just what problem are we trying to solve? is it cost of the combustion chamber? Number of valves? Weight? Overall complexity? Or is this just an interesting exercise for a kinematics class? The vehicle attitude control function can be performed two active and two standby modules- not four fully active as was used on Apollo. This is highly optimal for cryogenic thrusters since it minimizes the number of lines which must be chilled and pure 6 DOF operations are rare as opposed to simple maneuvers with coupled rotations and translations. This solution was proposed to NASA and rejected as being "just too different from what Apollo did". I cannot imagine them actually flying this contraption.

    1. Re:Design is a disaster by qualico · · Score: 1

      Nice assortment of information.

      When I build my space port, now I know who to call on for preliminary engineering consultation.

      It seems the main concept is to increase exposure of solar cells by allowing the craft to maneuver independantly using gimbles on thrusters.

      Why not use the already battle hardened multi directional thrusters found on a Harrier?

  26. I'll have a Gimbal and Water please by newpath4comVersion2 · · Score: 0
    No, no, no; Water would NEVER work.

    http_//www.newpath4.com/enginewow.htm . Everyone knows
    water is INERT. What everyone is just coming to find out is that non-nuclear fusion engines do not make any combustion pollution because NOTHING IS COMBUSTING. Why, they're everywhere. I have one myself!
    http://www.newpath4.com/millenialdawnpowerandlight secure21.htm

  27. obligatory simpsons... by Magius_AR · · Score: 1

    Mmmmm, gumball thrusters *drool*