Slashdot Mirror


NASA Engineers Work On Alternative Moon Rocket

Gibson writes "A team of 57 engineers at NASA's Marshall Spaceflight center feel that the Ares rocket is not the best solution for launching the new CEV. They are currently working on their own time developing an alternative launch system known as Jupiter. The 131 page proposal, along with other information, is available on the project website. Proponents of the project say that it is 'simpler, safer, and sooner' than the Ares project, predicting the ability for a return to the moon in 2017, two years before the current goal. Ares management has so far dismissed the proposal as a 'napkin drawing.'"

340 comments

  1. Yes, because we all know.... by mlwmohawk · · Score: 5, Insightful

    That a "napkin drawing" by engineers never amount to anything.

    1. Re:Yes, because we all know.... by MadRocketScientist · · Score: 5, Funny

      Does the napkin drawing include a doodle of the engineer as a cowboy?

    2. Re:Yes, because we all know.... by Anonymous Coward · · Score: 0

      Is it because it is hard to write in Copperplate Gothic Bold on a napkin?

      (See http://ubersoft.net/ for explanation)

    3. Re:Yes, because we all know.... by ari_j · · Score: 4, Insightful

      The problem is keeping all 131 napkins in order and intact.

    4. Re:Yes, because we all know.... by QuantumRiff · · Score: 2, Funny

      Yeah, its not like its rocket science or anything.. Oh, wait!

      --

      What are we going to do tonight Brain?
    5. Re:Yes, because we all know.... by mlwmohawk · · Score: 1

      All I can think of is, in the TV show "Big Bang" was Sheldon's embarrassment when his sister says he's a "rocket scientist or something."

      LOL. literal "Rocket Science" isn't figurative "rocket science."

    6. Re:Yes, because we all know.... by locokamil · · Score: 2, Informative

      Didn't the guy who invented ethernet sketch out his idea on the back of a napkin back in the day?

    7. Re:Yes, because we all know.... by bonehead · · Score: 1

      For God's sake, Don't Spill Your Coffee!!!

    8. Re:Yes, because we all know.... by failedlogic · · Score: 1

      Duh ... That's what page numbers are for! ;)

    9. Re:Yes, because we all know.... by charleste · · Score: 1

      Hey, if Kurt Vonnegut could do it while writing a NOVEL, why can't engineers do it for a proposal?

    10. Re:Yes, because we all know.... by tgd · · Score: 3, Funny

      It sure almost worked for Richard Pryor -- he damn near killed Superman with a computer drawn on the back of napkins.

    11. Re:Yes, because we all know.... by pohl · · Score: 5, Funny

      There's at least one notable example where a napkin drawing caused a stonhenge monument to be in danger of being crushed by a dwarf.

      --

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

    12. Re:Yes, because we all know.... by Anonymous Coward · · Score: 0

      helpful hit for napkin drawings:
        it's ' not "

    13. Re:Yes, because we all know.... by budgenator · · Score: 1

      I remember a guy named Adam Osborne was alleged to have sketched the first luggable computer the Osborne 1 on the back of a napkin.

      --
      Apocalypse Cancelled, Sorry, No Ticket Refunds
    14. Re:Yes, because we all know.... by dkleinsc · · Score: 1

      It's ok this time though, because the people implementing the project will think 36" is actually 36 meters, which is close enough.

      --
      I am officially gone from /. Long live http://www.soylentnews.com/
    15. Re:Yes, because we all know.... by imipak · · Score: 1

      Not your fault (unless you're from Wiltshire) but I think you'll find that's spelled "Stone'enge".

    16. Re:Yes, because we all know.... by Joe+the+Lesser · · Score: 1

      And more importantly, does it include a midget?

      --
      "I only speak the truth"
      Karma: null(Mostly affected by an unassigned variable)
    17. Re:Yes, because we all know.... by Tablizer · · Score: 2, Funny

      The problem is keeping all 131 napkins in order and intact.

      Just buy an Apple iWipe. (But careful not to mix anal mode and facial mode.)

         

    18. Re:Yes, because we all know.... by ari_j · · Score: 1

      Have you read Vonnegut's stuff? I'm not always convinced that the napkins maintained their order - or that they should have.

    19. Re:Yes, because we all know.... by lgw · · Score: 1

      The first Compaq computer was a sketch on the back of a napkin (or was it a placemat?) from House of Pies. It was in the company museum while the company lasted.

      --
      Socialism: a lie told by totalitarians and believed by fools.
    20. Re:Yes, because we all know.... by Anonymous Coward · · Score: 0

      That's not a problem. NASA always has such trouble with their budget because they only buy huge napkins that can be unfolded into 131 sheets.

      The main difficulty is finding a manufacturer who can create napkins that unfold into a number of sheets not divisible by 2.

    21. Re:Yes, because we all know.... by antdude · · Score: 1

      Check out these napkins.

      --
      Ant(Dude) @ Quality Foraged Links (AQFL.net) & The Ant Farm (antfarm.ma.cx / antfarm.home.dhs.org).
    22. Re:Yes, because we all know.... by pragma_x · · Score: 1

      Don't worry. Apple is planning to come out with the iSnot that features a facial-only-mode, to avoid any unpleasant confusion.

    23. Re:Yes, because we all know.... by tyrione · · Score: 1

      The problem is keeping all 131 napkins in order and intact.

      Just buy an Apple iWipe. (But careful not to mix anal mode and facial mode.)

      Warning: May cause streaking if not thoroughly fscked.

    24. Re:Yes, because we all know.... by evilviper · · Score: 1, Flamebait

      That a "napkin drawing" [...] never amount to anything.

      No, of course not: http://www.hitler.org/artifacts/volkswagen/

      --
      Slashdot gets worse every day... Pipedot: News for nerds, without the corporate slant
    25. Re:Yes, because we all know.... by shrikel · · Score: 1
      You mean Richard Pryor almost killed Christopher Reeve. It was Gus Gorman who almost killed Superman.

      And yes, the fact that I remember the character's name after so many years surprises even myself.

      --
      Any sufficiently simple magic can be passed off as mere advanced technology.
    26. Re:Yes, because we all know.... by el+americano · · Score: 1

      No, but it does look suspiciously like this.

      --
      Those are my principles. If you don't like them I have others. -Groucho Marx
    27. Re:Yes, because we all know.... by cthulhu11 · · Score: 0

      Not crushed, just trod upon.

    28. Re:Yes, because we all know.... by caldodge · · Score: 1

      The Voyager round-the-world aircraft was originally sketched on the back of a napkin at a Mojave restaurant.

  2. "A Napkin Drawing?" by Illbay · · Score: 5, Insightful

    How can anyone whose project is in the design stage, scoff at another that is in the conceptual stage? Neither of them EXIST yet!

    Where is Ares? Oh, it's in AUTOCAD! Well, that makes ALL the difference!

    Meanwhile, their brilliant project isn't expected to get anyone to the moon before, what, twenty years?

    Sheesh.

    --
    Any technology distinguishable from magic is insufficiently advanced.
    1. Re:"A Napkin Drawing?" by l2718 · · Score: 0, Troll

      Meanwhile, their brilliant project isn't expected to get anyone to the moon before, what, twenty years?

      Eleven years, actually (till 2019). It will take longer in practice, I'm sure, but you should check your figures before posting.

    2. Re:"A Napkin Drawing?" by SomeJoel · · Score: 3, Funny

      Eleven years, actually (till 2019). It will take longer in practice, I'm sure, but you should check your figures before posting.

      He wasn't quoting a figure, he was asking a question. But don't let that stop you from answering his question in a condescending and arrogant manner.

      --
      <Complete your profile by adding a signature!>
    3. Re:"A Napkin Drawing?" by MightyYar · · Score: 4, Interesting

      While I'm sure that it would cost less to have one vehicle instead of two, I disagree with their safety and "simpler" claim.

      I'm no rocket scientist (though I am an engineer), but a simple look at the NASA plan shows that the crew vehicle is much simpler than this Jupiter plan. The Jupiter are looking to use 2 shuttle boosters and the center fuel tank with shuttle engines mounted on it to put a crew into space, while NASA is using only one booster and one engine for the 2nd stage.

      Do I have this right? Seems to me that NASA's solution for the crew vehicle is simpler (and thus probably safer). Especially considering that there's never been a booster failure, has there? Though Challenger was arguably a booster failure, would it have been catastrophic without the center fuel tank explosion?

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    4. Re:"A Napkin Drawing?" by everphilski · · Score: 5, Informative

      Where is Ares? Oh, it's in AUTOCAD! Well, that makes ALL the difference!

      Guess I'd beg to differ, having seen metal cut for Ares I-X. Just do a google image search and see for yourself.

      And by the way, the Ares side of things is, to the best of my knowledge, on schedule to launch in 2009. If you have facts to differ, please let me know. The one thing that will probably delay them is the upcoming Hubble mission - until they vacate pad 39B, the appropriate pad modifications can't be made, so it's a day-for-day slip as the Hubble mission slips.

    5. Re:"A Napkin Drawing?" by scuba_steve_1 · · Score: 4, Interesting

      Design phase means they have requirements. Most likely detailed requirements...with detailed interface specifications between thousands of systems. Design of a system like Ares is not just industrial engineering. There are most likely a myriad of electrical, computer, and software systems being designed in parallel. Most likely thousands of items in fact.

      Of course, the real issue is most likely that people have a vested personal interest in the current direction...and perhaps congressional support for tasks being performed (or that will be performed) in their districts.

      Of course, I am just guessing. I don't build rockets...but I do work on software systems that have 5-10 million LOC...and there is a heck of a lot of work that is performed before coding starts...so I wouldn't assume that they don't have much invested in Ares yet just because they are not yet building...unless they are performing extreme agile spiral rocket building. ;)

      Of course, good ideas should not be dismissed...and given the size of this contingent, their proposal almost certainly warrants further investigation. Napkin drawing? Some of the most creative ideas in the world started in this fashion...and 57 engineers with a 100+ page white paper and a website is one hell of a napkin. Of course, it's almost certainly orders of magnitude less mature than the Ares design, but I think that the idea at least warrants a DAR.

      What happened the last time that NASA ignored a bunch of their engineers? I think they had plenty of time to reconsider while they were picking up Shuttle parts all over the western US.

    6. Re:"A Napkin Drawing?" by RockClimbingFool · · Score: 3, Insightful

      Well, considering the original post was written in a condescending and arrogant manner, I think the response fits just fine.

    7. Re:"A Napkin Drawing?" by SomeJoel · · Score: 1, Offtopic

      You're right, of course. There certainly appears to be an abundance of condescension and arrogance on slashdot.

      --
      <Complete your profile by adding a signature!>
    8. Re:"A Napkin Drawing?" by jandrese · · Score: 2, Insightful

      2009? If that's true color me shocked. I though it would take much longer.

      --

      I read the internet for the articles.
    9. Re:"A Napkin Drawing?" by camperdave · · Score: 4, Insightful

      Though Challenger was arguably a booster failure, would it have been catastrophic without the center fuel tank explosion?

      A better question would be: would a center fuel tank explosion cause a catastrophic loss of the crew module if the module were at the top of the stack, rather than at the side (especially if the crew module has abort rocket that can pull it away from the stack)?

      --
      When our name is on the back of your car, we're behind you all the way!
    10. Re:"A Napkin Drawing?" by Anonymous Coward · · Score: 0

      From what I read, the existing CEV design is to be re-used between the two projects, so the crew vehicle is as complex (or simple) between Jupiter and Ares.

      As far as simplicity, I believe the argument is it's simpler to re-use our existing equipment and infrastructure, with minor modifications, than it is to completely re-tool. Re-use of the ground-based infrastructure, re-use of the existing booster technology, re-use, re-use, re-use. What's complex about that?

      "Simplicity" shouldn't be seen with "pureness of design" glasses but overall project implementation complexity.

    11. Re:"A Napkin Drawing?" by Intron · · Score: 3, Funny

      My design is much safer since no fuel is carried on board. It requires a long-barelled cannon packed with guncotton.

      --
      Intron: the portion of DNA which expresses nothing useful.
    12. Re:"A Napkin Drawing?" by notadoctor · · Score: 5, Informative

      The Ares I-X has no commonality with the actual Ares I. It will still use a four segment solid rocket motor from the space shuttle, instead of the five segment one (a $2 billion dollar development project) that the real Ares I will use, and will have a dummy fifth segment and dummy upperstage. The actual Ares I-Y (a closer test vehicle that uses the proper solid rocket motor) won't fly until 2013, and the real Ares I won't fly until 2015 at the earliest and can't fly earlier because the upper stage engine won't be ready until around that time. The flight next year is more of a political stunt by NASA to give the appearance of progress. It's like driving out a Ferrari, but the body is plastic, and there's a Ford engine and a one gear forward only transmission under the hood.

    13. Re:"A Napkin Drawing?" by Anonymous Coward · · Score: 0

      You must be new here...

    14. Re:"A Napkin Drawing?" by Thelasko · · Score: 1

      If it's in AUTOCAD, then NASA needs to really get out of the 80's and into the 21st century. It's all NX5 and CATIA now a days.

      --
      One of our competitors trademarked the term "hypothesis". From now on, we will call them "boneheaded ideas".
    15. Re:"A Napkin Drawing?" by notadoctor · · Score: 1

      The Ares isn't simpler because that booster (5 segment SRB)on the bottom doesn't exist yet. Nor do the propellant tanks (18 ft diameter) or the engine for the upper stage (J-2X). All of those corollary elements (4 segment SRB, 28 ft diameter shuttle ET, RS-68 engine) already exist for the Jupiter-120.

    16. Re:"A Napkin Drawing?" by Tired+and+Emotional · · Score: 2, Insightful

      Probably would have been fatal without the main tak explosion. The shuttle was going fast enough that it probably could not have survived the large changes in attitude that were likely, even if you could disconnect instantaneously, because of aerodynamic buffeting from the main tank shocks. Plus once you get way out of shape you probably are not going to be able to recover,

      --
      Squirrel!
    17. Re:"A Napkin Drawing?" by R2.0 · · Score: 1

      "It requires a long-barelled cannon packed with guncotton."

      Bull, is that you? I KNEW the Israelis didn't get you!

      --
      "As God is my witness, I thought turkeys could fly." A. Carlson
    18. Re:"A Napkin Drawing?" by K.+S.+Kyosuke · · Score: 1

      Mr. Barbicane, is that you?

      --
      Ezekiel 23:20
    19. Re:"A Napkin Drawing?" by R2.0 · · Score: 1

      "As far as simplicity, I believe the argument is it's simpler to re-use our existing equipment and infrastructure, with minor modifications, than it is to completely re-tool. Re-use of the ground-based infrastructure, re-use of the existing booster technology, re-use, re-use, re-use. What's complex about that?"

      If this were a Win7 thread you'd be crucified, for good reason. If your current product sucks, reusing it is a false economy.

      And the Shuttle, as a system, definitely sucks.

      --
      "As God is my witness, I thought turkeys could fly." A. Carlson
    20. Re:"A Napkin Drawing?" by ArsonSmith · · Score: 1

      Right now they're trying to get out of the 70s and back into the 60s with hints of the 50s, and a nice modern look.

      --
      Paying taxes to buy civilization is like paying a hooker to buy love.
    21. Re:"A Napkin Drawing?" by e03179 · · Score: 1

      A test flight of Area 1-X is scheduled for April of 2009: http://spaceflightsystems.grc.nasa.gov/LaunchSystems/flightTest.php/

      --
      -516
    22. Re:"A Napkin Drawing?" by nasor · · Score: 1

      The thing about using shuttle engines (instead of the RS-68 engines that NASA is planning to use on Ares) is that they are very expensive because they were designed to be reused. The RS-68 engine provides about 50% more thrust than a shuttle engine, but only about costs $14 million/unit vs. $50 million/unit for a shuttle engine. If your goal is to get into space ASAP, then there's something to be said for using the shuttle engine because it is already man-rated. But if you are designing something that you plan to use for a long time, the RS-68 seems like a *much* better choice, even if you have to do some work initially to get it ready for manned use. And it's not like the RS-68 is untested; it has already been used on the Delta-IV family of rockets.

    23. Re:"A Napkin Drawing?" by nacnud75 · · Score: 1

      Ares 1-X has NO commonality with the currently proposed Ares 1. Ares 1-X uses a 4 segment booster while Ares 1 will used a 5 (or more) segment booster. Ares 1-X has a dummy upper stage etc. I'm sure Ares 1-X will look good but there is no way you could call it an Ares 1 vehicle beyond it looking vaguely similar. It's a Space Shuttle solid rocket motor with a body kit.

    24. Re:"A Napkin Drawing?" by ausoleil · · Score: 1
      "Where is Ares? Oh, it's in AUTOCAD! Well, that makes ALL the difference!"

      You mean the one targetted for a test launch next March? (link)

      The same Ares that has had key components tested? (link)

      Yup, it's just in AutoCAD, or more likely Pro/E.

    25. Re:"A Napkin Drawing?" by imipak · · Score: 1

      Mate, if you think humans are going back to the moon in Ares or anything else within the next three decades, there's a bridge I'd like you to take a look at. Yes, I know there are plans, but do you really think that ginormous chunk of NASA budget will survive the economy of the next five years? Get real. It's not gonna happen. The only question is how much money they spend before it's cancelled.

    26. Re:"A Napkin Drawing?" by terraplane · · Score: 0

      Am I the only one outraged that taxpayers' money is being wasted on some Big Boys' Super Space Adventure? (or whatever they want to call it). Wake up people, your tax dollars are subsidising Trekkies.

    27. Re:"A Napkin Drawing?" by Shoeler · · Score: 4, Informative

      The external tank didn't explode. The SRB burned through its o-ring an then burned a hole into the tank, releasing its contents which then turned into vapor. http://en.wikipedia.org/wiki/Space_Shuttle_Challenger_disaster "Contrary to the flight dynamics officer's initial statement, the shuttle and external tank did not actually "explode". Instead they rapidly disintegrated under tremendous aerodynamic forces"

    28. Re:"A Napkin Drawing?" by MightyYar · · Score: 1

      So then I guess my question would be, if the external tank hadn't "rapidly disintegrated" - would it have been survivable? :)

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    29. Re:"A Napkin Drawing?" by MightyYar · · Score: 1

      I see that perspective, but I disagree with it. Politically, the crew vehicle has to be safe. A massive, complicated heavy lifter is very expensive to make safe (space shuttle, ahem). Now I agree that Jupiter is less complex than the shuttle, and they remove a stage to make the crew transport even less complicated... but it still is much, much more complicated than the NASA program's crew vehicle.

      NASA can afford to lose the heavy lifters, but they take a real hit when they lose crew. I think the simple crew vehicle is the right decision.

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    30. Re:"A Napkin Drawing?" by peragrin · · Score: 1

      for the shuttle? probably not, for a much smaller top mounted CEV? more than likely, if they survive the G forces. the capsule could probably be safely recovered. the contents are another matter depending on how the g forces hit them.

      --
      i thought once I was found, but it was only a dream.
    31. Re:"A Napkin Drawing?" by lgw · · Score: 1

      I think that's right on the mark. The most appealing part of the current NASA plan is exactly that it uses a different launch vehicle for crew than for heavy lifting. Trying to mix the two was why the shuttle was such an amazing boondoggle.

      --
      Socialism: a lie told by totalitarians and believed by fools.
    32. Re:"A Napkin Drawing?" by Anonymous Coward · · Score: 0

      I AM a trekkie, and I don't mind MY tax dollars being spent on this stuff. I CAN think of a couple of things unrelated to space exploration that I do mind my tax dollars being spent on.

    33. Re:"A Napkin Drawing?" by joggle · · Score: 1

      I'm not outraged because the amount of money being spent is nothing compared to other things that I'm much more opposed to. They are not, I repeat not, increasing the budget of NASA back to Apollo era amounts.

      Heck, the US could stand to get some of its old prestige back so I'm actually for them trying to work on this project. And if you think the Apollo program didn't have much affect on the US reputation around the world think again.

    34. Re:"A Napkin Drawing?" by pacinpm · · Score: 1

      As far as I know the crew died when they hit the water. They used most of oxygene from emergency supplies. So external tank wasn't a problem in this case.

    35. Re:"A Napkin Drawing?" by lgw · · Score: 1

      Is there any better use for my tax dollars? I always want my tax dollars to be spend on better roads, but unfortunately I live in California where such money is consumed entirely without any actual improvements to roads. At least some Big Boys' Super Space Adventure gives me *something* for my money - the entertainment value - so go for it!

      Seriosly, my share of NASA's budget is about what it costs to take my famly to the movies, if we get popcorn and drinks. If all I get is the entertainment value of watch men go cool places, I'm well served by that budget.

      --
      Socialism: a lie told by totalitarians and believed by fools.
    36. Re:"A Napkin Drawing?" by WhiplashII · · Score: 2, Interesting

      Interestingly enough - it was survivable. The astronauts (at least some of them) were alive until impact. The shuttle just didn't have very good "final redundancy" measures - because such things would greatly effect the payload capability.

      --
      while (sig==sig) sig=!sig;
    37. Re:"A Napkin Drawing?" by MightyYar · · Score: 1

      I guess I'm using the term "simple" differently. I'm using it to describe the finished product. Having fewer parts means fewer potential points of failure.

      I agree that the Jupiter seems "simpler" from a design time or cost perspective - but I hardly see where significant risk comes from in adding 20% to the booster size, building some new propellant tanks (using Apollo-era design, mind you), or modifying the J-2 (also Apollo-era).

      Further, I don't think you can just pop a man on top of a RS-68 at this point - some design change would certainly be necessary to make them man-rated. Would this be less significant than modifying the J-2 into the J-2X?

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    38. Re:"A Napkin Drawing?" by MightyYar · · Score: 1

      NASA is also planning on using the RS-68 IIRC. It will be on the cargo-only Ares V until it is man-rated, right? Then they can start to put men up with it on the Ares IV and retire Ares I.

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    39. Re:"A Napkin Drawing?" by DerekLyons · · Score: 1

      What happened the last time that NASA ignored a bunch of their engineers? I think they had plenty of time to reconsider while they were picking up Shuttle parts all over the western US.

      Which group of engineers would that be? The ones who insisted that ongoing O-ring leakage wasn't a problem because no vehicles had been lost and the engineers were working on a fix? Or the group of engineers who insisted that ongoing debris shedding by the ET wasn't a problem because there hadn't been any serious damage and the engineers were working on a fix?

    40. Re:"A Napkin Drawing?" by nasor · · Score: 1

      Right - NASA is planning to use the RS-68. These guys from the article, on the other hand, want to use the SSMEs.

    41. Re:"A Napkin Drawing?" by Beezlebub33 · · Score: 3, Insightful

      Wait a minute.

      Earlier in this discussion, we have people concerned about the flight dynamics, controllability, number of SRB's, etc. The Ares I-X will test these things, won't it?

      Maybe I'm wrong, but to me this does not seem to be a boondoggle or publicity stunt. It's a reasonable stepping stone in the project.

      --
      The more people I meet, the better I like my dog.
    42. Re:"A Napkin Drawing?" by notadoctor · · Score: 1

      Adding 20% to the length of the SRB means the entire internal grain has to be redesigned - all of it. For a motor of that size, that is equivalent to designing a new rocket. ATK is getting paid between two and three billion dollars just to develop it. Certainly, you can put a person on top of an RS-68. NASA was going to do that with the Orbital Space Plane on a Delta IV, a program which got canceled when the new administration took over. Manrating isn't so much a matter of redesign as it is a process of ensuring that a certain level of reliability is met, which can also be done through testing. As Mike Griffin has said, we launch multi-billion dollar satellites on those engines, so we take a similar level of precaution to protect those extremely expensive satellites as we would to protect people. It is when the engine doesn't meet the specified level of reliability that redesigning has to take place. The J-2X is almost totally new. The major similarities are 1) they both use a gas generator cycle (so does the RS-68, and so did the kerosene fueled F-1) and 2) they both have a name that includes "J-2". Otherwise, they are very different. Different materials, different pumps, the J-2X even uses an ablative (passively cooled) nozzle, whereas the J-2 used hundreds of tubes welded together for cooling.

    43. Re:"A Napkin Drawing?" by Medievalist · · Score: 1

      While I'm sure that it would cost less to have one vehicle instead of two, I disagree with their safety and "simpler" claim.

      I'm no rocket scientist (though I am an engineer), but a simple look at the NASA plan shows that the crew vehicle is much simpler than this Jupiter plan. The Jupiter are looking to use 2 shuttle boosters and the center fuel tank with shuttle engines mounted on it to put a crew into space, while NASA is using only one booster and one engine for the 2nd stage.

      Do I have this right? Seems to me that NASA's solution for the crew vehicle is simpler (and thus probably safer). Especially considering that there's never been a booster failure, has there? Though Challenger was arguably a booster failure, would it have been catastrophic without the center fuel tank explosion?

      Strap-on boosters are an old and well-proven technology. Delta, Titan/Centaur, and Atlas have all used them very successfully; the Delta vehicle has been in use in various forms for more than a quarter-century and I'd guess it has put more satellites in orbit than any other.

      Sending two vehicles up separately and having them join up after launch is a comparatively radical idea, with a much shorter track record. We've been doing pretty well lately with the international space station, though, and it's not really as hard as refueling a jet in flight (since you don't have to fight turbulence or weather).

      When Challenger was built, NASA insisted that we use rubber-gasketed steel composite SRBs. We wanted to use case-on-propellant technology, winding graphite fiber onto pre-cast propellant cores to make a seamless case, but NASA was on this "cheap spaceflight" kick and had a lowest-bid mentality that ruled out anything new. Since then the Deltas have used wound graphite cases very successfully (although, Wikipedia has refused to let me create a Vic Singer entry - designing the airbags for the Mars Lander on the back of a napkin isn't "notable" enough, so I don't think his case-on-propellant designs will get him in. Perhaps you have to be a minor player in a Joss Whedon flick to get props at wikipedia).

      I'm not passing judgment on either scheme, just thought I'd give you some data to munch on.

    44. Re:"A Napkin Drawing?" by rleibman · · Score: 1

      I AM a trekkie, and I don't mind MY tax dollars being spent on this stuff. I CAN think of a couple of things unrelated to space exploration that I do mind my tax dollars being spent on.

      My question to you sir, is *why* you seem to want to spend MY tax dollars so freely. If you want space exploration and think it's a laudable goal, by all means send all your money in, I'm sure nobody will give it back.
      I too am a trekkie (trekker?), I love space exploration and think that spending money on it is worth it, but where I differ with you is in putting a gun to other people's heads and asking them to share in our value system. Yes, there are worse things I can think my money could be (and is) being spent on, but that's a faulty argument for spending it on *your* pet project.

    45. Re:"A Napkin Drawing?" by rleibman · · Score: 1

      Seriosly, my share of NASA's budget is about what it costs to take my famly to the movies, if we get popcorn and drinks. If all I get is the entertainment value of watch men go cool places, I'm well served by that budget.

      As I said above, you may well be served by that budget, but forcing other people, at the point of a gun, to share your priorities is just... plain...wrong.

    46. Re:"A Napkin Drawing?" by scuba_steve_1 · · Score: 1

      Did I say all the engineers? No, I said "a bunch". Most sources seem to agree that the decision to launch Challenger was made by NASA and management...not engineering. Many Google sources agree. Example:


      From: http://en.wikipedia.org/wiki/Space_Shuttle_Challenger_disaster

      Forecasts for January 28 predicted an unusually cold morning, with temperatures close to 31 degrees F (â'1 degree C), the minimum temperature permitted for launch. The low temperature had prompted concern from engineers at Morton Thiokol, the contractor responsible for the construction and maintenance of the shuttle's SRBs. At a teleconference which took place on the evening of January 27, Thiokol engineers and managers discussed the weather conditions with NASA managers from Kennedy Space Center and Marshall Space Flight Center. Several engineers - most notably Roger Boisjoly, who had voiced similar concerns previously - expressed their concern about the effect of the temperature on the resilience of the rubber O-rings that sealed the joints of the SRBs. They argued that if the O-rings were colder than 53 degrees F (12 degrees C), there was no guarantee they would seal properly. This was an important consideration, since the O-rings had been designated as a "Criticality 1" componentâ"meaning that there was no backup for them and their failure would destroy Challenger and its crew. They also argued that the low overnight temperatures would almost certainly result in SRB temperatures below their redline of 40 ÂF (4 ÂC). However, they were overruled by Morton Thiokol management, who recommended that the launch proceed as scheduled.


      ...and...

      Although the Ice Team had worked through the night removing ice, engineers at Rockwell International, the shuttle's prime contractor, still expressed concern. Rockwell engineers watching the pad from their headquarters in Downey, California were horrified when they saw the amount of ice. They feared that during launch, ice might be shaken loose and strike the shuttle's thermal protection tiles, possibly due to the aspiration induced by the jet of exhaust gas from the SRBs. Rocco Petrone, the head of Rockwell's space transportation division, and his colleagues viewed this situation as a launch constraint, and told Rockwell's managers at the Cape that Rockwell could not support a launch. However, Rockwell's managers at the Cape voiced their concerns in a manner that led Houston-based mission manager Arnold Aldrich to go ahead with the launch. Aldrich decided to postpone the shuttle launch by an hour in order to give the Ice Team time to perform another inspection. After that last inspection, during which the ice appeared to be melting, Challenger was finally cleared to launch at 11:38 a.m. EST


      ...and...

      Feynman was so critical of flaws in NASA's "safety culture" that he threatened to remove his name from the report unless it included his personal observations on the reliability of the shuttle, which appeared as Appendix F.[32][33] In the appendix, he argued that the estimates of reliability offered by NASA management were wildly unrealistic, differing as much as a thousandfold from the estimates of working engineers. "For a successful technology," he concluded, "reality must take precedence over public relations, for nature cannot be fooled."


      Columbia?


      From http://en.wikipedia.org/wiki/Space_Shuttle_Columbia_disaster

      While Columbia was still in orbit, some engineers suspected damage, but NASA managers limited the investigation on the grounds that little could be done even if problems were found


      Granted, in the Columbia disaster, other engineers performed simulations and stated that the damage wa

    47. Re:"A Napkin Drawing?" by HornWumpus · · Score: 1

      No more wrong then 90% of the things the federal government does.

      Building roads, waging war or supporting welfare mothers; you'll always find someone who objects.

      Taxation is theft at gun point. Get over it.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    48. Re:"A Napkin Drawing?" by Rei · · Score: 2, Insightful

      I'm no rocket scientist (though I am an engineer), but a simple look at the NASA plan shows that the crew vehicle is much simpler than this Jupiter plan. The Jupiter are looking to use 2 shuttle boosters and the center fuel tank with shuttle engines mounted on it to put a crew into space, while NASA is using only one booster and one engine for the 2nd stage.

      Jupiter has three times the payload capacity. Jupiter uses the normal 4-segment SRBs, while Ares uses a brand new five segment SRBs. The 5-segment SRB is really a completely different rocket; it even uses a different propellant mix with a different core shape. Even with its larger rocket, it may not be able to cut it with that. Ares has so many design flaws, it's not even funny. The whole thing is way overweight, the reentry G-forces would be like riding a centrifuge pointed backwards, the vibration loads are going to be terrible... it's just a bad design.

      But, as the Jupiter team points out, the biggest issue (cost-wise) is that while Ares may resemble the Shuttle family, most of the components are only "similar". It is constrained by what the Shuttle system was like, but doesn't benefit from all of the trial and error experience on that hardware. Even things you might think would carry over, like SRB recovery, have to be completely reworked with the new stack. They're even having to rebuilt a lot of the ground infrastructure to accomodate the changes -- the crawlers, the VAB, etc. They might as well just have started a brand new program; they would have been in a far better position. There's a reason the first crewed launch got pushed back from 2011 to 2015. With Jupiter, the components aren't just similar; they're the same; the expensive shuttle orbiter is all they're really ditching. Nothing needs to be completely re-engineered.

      --
      No, she's fine. My associate is vomiting for a totally unrelated reason.
    49. Re:"A Napkin Drawing?" by terraplane · · Score: 0

      My question to you sir, is *why* you seem to want to spend MY tax dollars so freely. If you want space exploration and think it's a laudable goal, by all means send all your money in, I'm sure nobody will give it back. I too am a trekkie (trekker?), I love space exploration and think that spending money on it is worth it, but where I differ with you is in putting a gun to other people's heads and asking them to share in our value system. Yes, there are worse things I can think my money could be (and is) being spent on, but that's a faulty argument for spending it on *your* pet project.

      After some thought, no, I'm not going to give you that.

      I am completely opposed to space exploration, whether funded privately or by the taxpayer.

    50. Re:"A Napkin Drawing?" by everphilski · · Score: 2, Insightful

      Sure, it's not 1:1 with the final vehicle, do you really expect the first test flight to be?

      You've listed the ways it is not Ares I, now list the ways it is not Shuttle. You will find the list is much longer. Yes, only four segments on FS plus a dummy stage but it's not a stock SRB. The upper stage is a mass accurate dummy, but is instrumented for re-entry. The CLV is testing an abort scenario.

      It's not a complete PR scenario ... some of us are getting * data from this launch.

      It's like driving out a Ferrari, but the body is plastic, and there's a Ford engine and a one gear forward only transmission under the hood.

      It's more like driving a concept car. It's not street legal, you won't be able to buy it, but it drives and you can get data from it to design the final product you market to the general populace. IMHO.

    51. Re:"A Napkin Drawing?" by Anonymous Coward · · Score: 0

      Why is it wrong to say something in a condescending and arrogant manner when you are right? It's not. You're the same type of ignoramus who would call someone a "know-it-all" as if it's a bad thing.

    52. Re:"A Napkin Drawing?" by Anonymous Coward · · Score: 0

      One interesting proposal I saw was that the Jupiter has enough spare launch capacity for crew that a 20 ton ballistic shield can be included to protect the crew.

    53. Re:"A Napkin Drawing?" by iamlucky13 · · Score: 2, Informative

      Easy statements first:

      Meanwhile, their brilliant project isn't expected to get anyone to the moon before, what, twenty years?

      It depends on congressional funding. Current plans are between 2018 and 2020, but first operations of the rocket for ISS and LEO operations should be about 2015. NASA can't really get cracking on this until the shuttle retires in 2010, which will free up about $3 billion/year in funding...unless congres wants to dole out some extra right now.

      How can anyone whose project is in the design stage, scoff at another that is in the conceptual stage?

      Design is definitely a step ahead of concept. To be fair, calling it a napkin drawing was a press-briefing response, not the whole story. In fact, several engineers gave it a fairly detailed going over and pointed out some problems. The Direct team then addressed those problems and developed version 2. This is all after NASA already examined the basic architecture of Direct in their ESAS study and concluded two launches of the same vehicle was workable but less than ideal for a lunar mission, and required a vehicle that was overkill for ISS operations. However, some of the assumptions in that study didn't hold true, and Direct is maintaining that NASA needs to take a another look at it.

      Neither of them EXIST yet! Where is Ares? Oh, it's in AUTOCAD! Well, that makes ALL the difference!

      Much more in-depth analysis has been conducted on Ares I/V than on Direct's Jupiter proposal. Actually, since Direct uses an essentially unmodified shuttle SRB, they can reasonably contend that some of the hardware does exist. Meanwhile however, NASA is building test hardware for the Ares I, and they've begun detailed design on quite a few components, including the J-2X 2nd stage engine and 5-segment SRB. In some ways Direct is ahead, but as far as work that's been done, Ares is ahead.

      My take on it is that Direct honestly has a pretty decent proposal. It is definitely feasible. NASA maintains that it doesn't mesh well with what they were directed to do under Bush's Vision for Space Exploration, which is intended to be scalable to Mars missions. NASA prefers the payload splits of the Ares I/V system for lunar missions, the theoretically higher safety of the Ares 1 for manned-launches, and the fewer flights needed for a Mars mission the giant Ares V would afford. Given the engineering issues they've encountered, however, I think it would be a good idea to give the "two-launch" architecture another look.

      At the same time, some are maintaining that NASA is pursuing the Ares I/V as a means of protecting jobs in important congressional districts or for major contractors like ATK who will have $billions in contracts for Ares. Others accuse NASA administrator Mike Griffin of having delusions of granduer, wanting to be the engineer responsible for creating the largest rocket ever. I see no convincing arguments for buying into those accusations.

    54. Re:"A Napkin Drawing?" by DerekLyons · · Score: 1

      Most sources seem to agree that the decision to launch Challenger was made by NASA and management...not engineering.

      That would fall under "well, duh" because making decisions is what management does. :) :) But who do you think provides the managers with the information that they base their decisions on?
       
       

      but my point was just that - don't just go with consensus when you have a vocal minority of informed engineering experts who have a different opinion.

      So, we should have listened to the vocal minority of engineering experts who insisted that landing on the moon was beyond the technology available? Or to put it another way, if you bow to every vocal minority... then nothing ever gets done.

    55. Re:"A Napkin Drawing?" by The_Rook · · Score: 1

      gee whiz, it looked like an explosion to me.

      --
      when religion is no longer the opiate of the masses, governments will resort to real opiates.
    56. Re:"A Napkin Drawing?" by isorox · · Score: 1

      Eleven years, actually (till 2019). It will take longer in practice, I'm sure, but you should check your figures before posting.

      He probably got confused over metric years

    57. Re:"A Napkin Drawing?" by darkmeridian · · Score: 1

      The NASA plan has fewer parts but it does not necessarily follow that it is safer, as it will use relatively untested technologies. The rocket in the NASA design would be the largest solid-fuel rocket engine ever used. It will be statically-unstable because it is top-heavy, which is also a first. There were problems having the solid rocket fuel burn properly all the way through. The rebel plan may have more parts but it is based on well-known technology.

      Moreover, Challenger was doomed regardless of the center fuel tank. The Challenger disaster was caused by a malfunctioning solid rocket booster, which are used by both the NASA and the rebel plans. The center fuel tank did not explode; the stack was turned sideways to the direction of travel by the booster failure, and the rapid change in aerodynamic pressures caused the stack to come apart. The big white cloud was caused by the cryogenic fuels being released into the air. Liquid oxygen and hydrogen actually burn without color in the air, so if it exploded, it would have been less spectacular. The Challenger crew survived the disintegration because manual emergency valves on their flight suits were activated. They died on impact. There were no abort modes that would have saved their lives in that instance. The vehicle was going too quickly for them to bail out.

      --
      A NYC lawyer blogs. http://www.chuangblog.com/
    58. Re:"A Napkin Drawing?" by Phairdon · · Score: 1

      You do know that the first full scale flight test for the Ares I-X is in April of 2009, right? They Ares I-X is down to the nuts and bolts, it is not a paper design. You knew this before making that comment about Ares being only in autocad, right?

    59. Re:"A Napkin Drawing?" by Phairdon · · Score: 1

      No commonality to the actual Ares I? Are you testing different wind tunnel models than I am? If so, I would like to see them. The flight test will provide very useful actual flight test data. There is only so much you can do in the wind tunnel and extract to full scale. All kinds of measurements will be taken and used to further refine the design. What I am mainly interested in personally is the sound pressure levels on the upper stage.

      You are aware of the concept of iterative design?
      You don't think taking actual flight test measurements will be helpful?

    60. Re:"A Napkin Drawing?" by MightyYar · · Score: 1

      the reentry G-forces would be like riding a centrifuge pointed backwards

      Aren't they proposing to use the same crew module?

      With Jupiter, the components aren't just similar; they're the same

      My first thought is - why not just stick with the orbiter then? The main engine cost alone would probably keep it from being cost effective. Shuttle flights are really, really expensive. And while you would be getting rid of the hard-to-maintain orbiter, you'd also be throwing away several $50 million shuttle engines each time you launched instead of fewer $15-20 million engines.

      Note that I really don't know much about this - I'm mostly in this conversation to learn. I would never be so conceited to second guess either the NASA administration OR the rouge engineers on this issue :)

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    61. Re:"A Napkin Drawing?" by camperdave · · Score: 1

      It's the difference between Bang and Woosh. The liquid hydrogen and the liquid oxygen did not combust instantaneously, or near instantaneously, but over the course of a couple of seconds.

      --
      When our name is on the back of your car, we're behind you all the way!
    62. Re:"A Napkin Drawing?" by Anonymous Coward · · Score: 0

      My design is much more safer, but unfortunately it does not fit the margin...

    63. Re:"A Napkin Drawing?" by a208returns · · Score: 1

      not main engines but "Like the planned Ares-V, DIRECT proposes
      to use the low-cost Pratt & Whitney,
      Rocketdyne RS-68 engine borrowed from the
      US Air Force's Delta-IV program" but would use them as they are now not upgraded to 106% as need for ares.

      also it is very hard if not impossible to shut down a solid fuel booster once it has started its burn. by the way i am a SF writer by trade not a Rocket scientist.

    64. Re:"A Napkin Drawing?" by a208returns · · Score: 1

      am i only one by the way who thinks we should build both ?

    65. Re:"A Napkin Drawing?" by Anonymous Coward · · Score: 0

      By the way, NASA has addressed this proposal, and they found it severely lacking.

      http://www.spaceref.com/news/viewsr.html?pid=28513

    66. Re:"A Napkin Drawing?" by Rei · · Score: 1

      My first thought is - why not just stick with the orbiter then? The main engine cost alone would probably keep it from being cost effective.

      The SSMEs are on the Shuttle, which, as I just mentioned, they're ditching.

      --
      No, she's fine. My associate is vomiting for a totally unrelated reason.
    67. Re:"A Napkin Drawing?" by Stanistani · · Score: 1

      Taxation is theft at gun point.

      Right. By that logic, any law is enslavement at gunpoint.
      Guess you must be some sort of anarchist.
      I'll be over to collect your stuff, since you won't call the police on principle.

    68. Re:"A Napkin Drawing?" by RalphTheWonderLlama · · Score: 1

      YMBNH!

      --
      simple, fast homepage with your links: http://www.ngumbi.com/
    69. Re:"A Napkin Drawing?" by RalphTheWonderLlama · · Score: 1

      I'm sure there will be future missions that don't require the heavy lift and are just for moving crew and also future missions that just need heavy lift and don't need to send a crew. They are definitely on the right track for that.

      --
      simple, fast homepage with your links: http://www.ngumbi.com/
    70. Re:"A Napkin Drawing?" by MightyYar · · Score: 1

      Ahhh, sorry - they are planning on using the same engine (though unmodified).

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    71. Re:"A Napkin Drawing?" by complete+loony · · Score: 1

      ... the fewer flights needed for a Mars mission the giant Ares V would afford

      Actually, a mars mission with Direct has the same number of required launches. Don't forget to count the Ares I launch required for the crew.

      --
      09F91102 no, 455FE104 nope, F190A1E8 uh-uh, 7A5F8A09 that's not it, C87294CE no. Ah! 452F6E403CDF10714E41DFAA257D313F.
    72. Re:"A Napkin Drawing?" by Anonymous Coward · · Score: 0

      A Mars mission or a moon mission?

      A moon mission has the same number of launches, but using 3 instead of 4 SRB's with Ares vs. Direct (considered a slightly higher risk). It also has a much different payload split, which can be difficult to accomodate, and you can't do a single cargo launch to the moon with Direct. Ares-V can launch a lander without a crew for re-supply only.

      The current baseline for a Mars mission actually requires about 600-800 tons to LEO (split up into two or three cycles so that essential habitation and return equipment is verified operable on the surface before a crew launches), plus an Orion launch. That's 5-6 Ares V launches or 8-12 Direct launches.

      Of course, that's for a 6 month surface stay with a hab, lab, power, and I think a pressurized rover. A Mars mission doesn't necessary have to be that big, but that's the scheme NASA is shooting towards.

  3. Napkin Drawing by jeffy210 · · Score: 4, Funny

    The 131 page proposal

    That's a hell of a lot of napkins...

    --
    ------
    "And may your days be long upon the earth."
    1. Re:Napkin Drawing by Anonymous Coward · · Score: 1, Insightful

      Mod parent up more. If 57 NASA Engineers (best ones out there) say something, they likely are correct. Especially when this plan really seems saner with less risks (reusing old reliable parts) and seems more independent (not bigmoney.com'ish project). That plan was made by people who care, and contains well founded criticism towards Ares.

    2. Re:Napkin Drawing by devnullkac · · Score: 1

      This is why we glorify the mental prowess of "rocket scientists". They consider a 131 page proposal with this level of detail to be the equivalent of a napkin drawing.

      Frankly, Ares management is probably right, but that's not the reason this idea won't fly, as it were. The real reason, depending on your level of cynicism, is that either (a) it has arrived too late or (b) it doesn't justify enough spending.

      --
      What do you mean they cut the power? How can they cut the power, man? They're animals!
    3. Re:Napkin Drawing by Tumbleweed · · Score: 4, Funny

      >> The 131 page proposal

      > That's a hell of a lot of napkins...

      Hardly. That's like two visits to Taco Bell.

    4. Re:Napkin Drawing by IndustrialComplex · · Score: 3, Informative

      This is why we glorify the mental prowess of "rocket scientists". They consider a 131 page proposal with this level of detail to be the equivalent of a napkin drawing.

      In the world of government and military systems, 131 pages is just enough to cover the information declarations, the acronym list, and the table of contents. Page 131 probably says "Pages 131-542 TBD".

      --
      Out of modpoints but really liked a post? 1BDkF6TtmmeZ3yqXbz9yhdYVqRYnwFoXDj
    5. Re:Napkin Drawing by bondsbw · · Score: 2, Funny

      The 131 page proposal

      That's a hell of a lot of napkins...

      Not in metric...

      --
      All my liberal friends think I'm a conservative, all my conservative friends think I'm a liberal.
    6. Re:Napkin Drawing by hypergreatthing · · Score: 4, Funny

      Are you counting the used toilet sheets after going to taco bell as well?

    7. Re:Napkin Drawing by the_skywise · · Score: 1

      That's a hell of a lot of napkins...

      Tell him about the Twinkie...

    8. Re:Napkin Drawing by elrous0 · · Score: 1

      They had better be careful. Anyone remember what happened to the poor exec that pushed the Robocop program over the ED-209 program at OCP?

      --
      SJW: Someone who has run out of real oppression, and has to fake it.
    9. Re:Napkin Drawing by slashhax0r · · Score: 1

      >>Hardly. That's like two visits to Taco Bell

      We were discussing napkins. not toilet paper.

    10. Re:Napkin Drawing by Anonymous Coward · · Score: 0

      Weâ(TM)re using Taco Bell napkins now?
      Yes they won the franchise wars - now all restaurants are Taco Bell.

  4. $35 Billion by Illbay · · Score: 3, Funny

    From the project website:

    This change to NASA's architecture completely removes the costs & risks associated with developing and operating a second launcher system, saving NASA $19 Billion in development costs, and a further $16 Billion in operational costs over the next 20 years.

    $35 Billion in savings? How much is that in napkins?

    --
    Any technology distinguishable from magic is insufficiently advanced.
    1. Re:$35 Billion by Creepy+Crawler · · Score: 1

      > $35 Billion in savings? How much is that in napkins?

      It's governmental napkins. The study cost $34.9 billion and $.1 billion for Halliburton making them.

      --
    2. Re:$35 Billion by yukk · · Score: 2, Funny

      It's about 45 football fields of napkins stacked vertically.

      --
      The trouble with the rat race is that even if you win, you're still a rat." Lily Tomlin
    3. Re:$35 Billion by shawn(at)fsu · · Score: 2, Funny

      I need this figure in LOC's or it's useless to me.

      --
      500 dollar reward for tip(s) leading to the arrest of the person(s) who stole my sig.
    4. Re:$35 Billion by mh1997 · · Score: 1

      If it's Raytheon that is writing the code, then 5 LOC for $35 Billion.

    5. Re:$35 Billion by Anonymous Coward · · Score: 0

      Around 4.125E+12, give or take a couple billion.

    6. Re:$35 Billion by moosesocks · · Score: 1

      Enough to print the contents of the Library of Congress on.

      --
      -- If you try to fail and succeed, which have you done? - Uli's moose
    7. Re:$35 Billion by RealGrouchy · · Score: 1

      $35 Billion in savings? How much is that in napkins?

      Enough napkins to scribble half of the contents of the Library of Congress on the back of them.

      - RG>

      --
      Hey pal, this isn't a pleasantforest, so don't waste my time with pleasantries!
    8. Re:$35 Billion by cthulhu11 · · Score: 0

      Forget napkins -- what about kwatloos?

  5. Does it come with a funky robot? by ricebowl · · Score: 2, Funny

    They are currently working on their own time developing an alternative launch system known as Jupiter

    After reading the summary the only thing that went through my head was memories of Matt Le Blanc, and the urge to cry: "Danger, Will Robinson!"

    I could probably do with a rest...

    1. Re:Does it come with a funky robot? by Farmer+Tim · · Score: 1

      the only thing that went through my head was memories of Matt Le Blanc

      Oh, a noob!

      --
      Blank until /. makes another boneheaded UI decision.
    2. Re:Does it come with a funky robot? by Chris+Mattern · · Score: 1

      Noob. *My* first thought was of Billy Mumy and the urge to cry, "Danger, Will Robinson!".

    3. Re:Does it come with a funky robot? by ricebowl · · Score: 1

      I can only apologise for my apparent n00b-ness, I wasn't intending to offend anyone while referring to the Matt Le Blanc vehicle, my intent was simply to attach the comedy value (such as there was any) of the phrase 'danger...' to the crappy remake, rather than attach any satire to the original. That and I couldn't remember the cast names. I'm not quite that old...

  6. It is all of those things, but by Iowan41 · · Score: 1

    it still uses solids for a human launch vehicle. That is a really stupid thing, which was known before Congress limited the Shuttle design, forcing the move to SRBs, and which caused the Challenger accident and loss of 7 crew.

    1. Re:It is all of those things, but by $RANDOMLUSER · · Score: 1

      NEWS BULLETIN: Flying into space in any kind of rocket is dangerous. Sometimes, even practicing is.

      --
      No folly is more costly than the folly of intolerant idealism. - Winston Churchill
    2. Re:It is all of those things, but by Anonymous Coward · · Score: 3, Insightful

      Flying into space in any kind of rocket is dangerous

      True, but in your quest to belittle the original poster, you fail to address his (completely legitimate) concerns:

      1.) SRBs can't easily be throttled

      2.) SRBs can't be shut down in flight

      Even had the Challenger crew known about the O-ring breach that was burning holes in the external tank, there'd have been exactly dick they could have done about it short of trying to blow the orbiter off the stack and hoping it remained controllable. Liquid fueled rockets are *much* safer once you're in the air, and "space flight is already dangerous" is not a good reason to avoid mitigation of risk whenever possible.

    3. Re:It is all of those things, but by director_mr · · Score: 4, Insightful

      Solid fuel launches with the shuttle seem fine from a safety standpoint. The one danger that did in a shuttle (falling Ice) came from the liquid oxygen tank, no the solid fuel. The other failure was of an O-ring connecting the booster to the liquid fuel tank. That failure was addressed.

      The falling ice problem is addressed by putting the cargo above the boosters. The O-ring has already been addressed. So the new proposal seems even safer than the shuttle. I fail to see how solid fuel rockets are inherently more dangerous than liquid fuel ones.

      Solid fuel rockets can't stop, and they have to be carefully made so there isn't any open pockets of no fuel or they explode. But if you carefully make them (Nasa has) and engineer the launch system to take into account the thing won't turn off (Nasa has), it is a great system. Liquid Fuel can be throttled or turned off, but requires a very complex (read point of failure possibility) pump system to work properly. That has its drawbacks as well. In summary Liquid Fuel and Solid Fuel have different strengths and weaknesses, and when the vehicle is engineered to handle them, it shouldn't exclude either from being used the human passengers.

    4. Re:It is all of those things, but by notadoctor · · Score: 1

      The space shuttle also didn't have an escape system. The Orion capsule will. It is safer to use liquid fueled engines that can be shut down, but if the space shuttle had been designed in such a way that the astronauts could separate their vehicle from the rocket, the Challenger crew might still have survived, even with the solid boosters on the side.

    5. Re:It is all of those things, but by $RANDOMLUSER · · Score: 1

      I reject your premise. 1) Liquid fueled rockets are only throttled for a softer liftoff than SRBs provide. Once you're clear of the tower, it's balls-out until you run out of fuel. 2) SRBs can't be shut down in flight, yes. And you would want to shut down a liquid fueled booster halfway to orbit exactly why? Challenger blew up only incidentally due to O-rings. The real cause was a middle manager screaming "What do you mean I can't ship on time???" - happens every day in factories all around the world. The notion that "Liquid fueled rockets are *much* safer once you're in the air" has no basis in fact. Your choices are a) go to orbit, b) abort & eject, or c) blow up and die. The fact is, SRBs are cheaper and MORE reliable (no moving parts) than liquid for first (and second) stage.

      --
      No folly is more costly than the folly of intolerant idealism. - Winston Churchill
    6. Re:It is all of those things, but by OhEd · · Score: 2, Informative

      It wasn't even the shock wave that caused Challenger to disintegrate, it was the sudden deviation from its course while under Max-Q. Trying to separate quickly from the stack would have been just as bad. http://en.wikipedia.org/wiki/Space_Shuttle_Challenger_disaster

    7. Re:It is all of those things, but by imipak · · Score: 1

      if you carefully make them (Nasa has) and engineer the launch system to take into account the thing won't turn off (Nasa has),

      I've always thought that a much more unpleasant failure mode is if one fails to turn ON. Can't see that being survivable.

    8. Re:It is all of those things, but by smoker2 · · Score: 1, Troll

      Insightful - bollocks !
      1)The "one" danger ? I seem to remember more than 1 dead shuttle.
      2)"The o-ring connected the booster to the liquid fuel tank" - Wrong - See AC below.
      3)"The o-ring has already been addressed" - Handwaving about an invalid point does not make it go away.
      4)"I fail to see how solid fuel rockets are inherently more dangerous than liquid fuel ones." - not surprising as you fail to see things in any kind of clarity at all.
      5)Oh here we go - " solid fuel rockets can't stop" - You just said there was nothing "inherently" more dangerous about solid fuel rockets - well there's one (quite major) thing. Not to mention that when you get into space, it's quite useful to have some, you know, FUEL, to maneuver with !
      You do realise that the shuttle uses BOTH types of propulsion simultaneously ?
      Mods - eat my shorts.

    9. Re:It is all of those things, but by alexander_686 · · Score: 1

      Not quite the whole story about the solid rockets. The issue with the o-rings is not the connection from the solid rockets to the main fuel tank. The solid fule rocket is made up of 4 segments. There is an o-ring used to seal these segemnts together. This has always been a problem and remains a problem. The conection is a high stress point so problems are more evident there, but there are issues whereever there is an o-ring. When the shuttle was first being designed NASA looked into casting the solid rockets as a single piece but that would have increased the weight too much.

    10. Re:It is all of those things, but by director_mr · · Score: 2, Informative

      There have been 294 consecutive safe solid fuel rocket launches since the O-Ring problem with the Challenger. The proposed Jupiter launcher uses both solid and liquid fuel rockets, the Solid rockets boosting the initial stage and then separating. They address the solid fuel rockets don't stop issue by providing systems that detach the solid rockets from the launch vehicle in an emergency, and detaching the launch capsule from the rest of the launch vehicle and parachuting it down.

      I'm not sure you read my post beyond just trying to spew vitriol. How is the fact a solid rocket can't stop inherently more dangerous if you engineer the launch vehicle to take that into account?

    11. Re:It is all of those things, but by WhiplashII · · Score: 1

      SRBs are not really that bad:

      1) Mission profiles don't really change - you don't need to throttle, you only need "go" and "abort". Solids are much more simple than liquids, so that can be simpler and therefore safer.

      2) You can shut down a solid - the shuttle SRMs were only allowed in the baseline design because they could be shut down in flight. Other solids that have flown have been shut down for precision orbital insertion - all you do is vent the engine (normally by blowing the forward panel). The problem with the shuttle is that the first attempt didn't work (it would have shook the shuttle to pieces), and there wasn't any money to continue the work.

      SRBs do have their challenges, but the ones you mention are not really the hard parts.

      --
      while (sig==sig) sig=!sig;
    12. Re:It is all of those things, but by WhiplashII · · Score: 1

      Not only that, but the most likely interpretation of the data says that the astronauts did survive Challenger, all the way to ground impact. If the shuttle had had survival capsules with parachutes for the crew, they would have survived - humans are very hardy, and have survived 20G+_reentries.

      When designing a system that pushes the envelope, you want to make it survive with a minimum set of stuff working. Ask yourself "what is the absolute minimum set of working equipment that gives me an alive crew?" Then work on decreasing the number of systems in the answer.

      --
      while (sig==sig) sig=!sig;
    13. Re:It is all of those things, but by old+dr+omr · · Score: 1

      I'm no rocket scientist but I thought SRBs could be jetisoned at any time which is as good as an off switch to me.

    14. Re:It is all of those things, but by Rakishi · · Score: 1

      Everything can explode, the solution is to have an escape mechanism not to use more complex (ie: unsafe) engines to mitigate an edge case. Hell if your engines need to be shut down in flight then you'll be ejecting anyways because otherwise you die when the whole thing impacts the ground.

      The Soyuz rocket I believe blew up twice without any casualties with one of them at least being a purely automatic ejection (ie: computer saw problem, capsule got ejected, rocket went boom shortly afterwards). Not pleasant on the crew (high Gs) but not exactly fatal either.

    15. Re:It is all of those things, but by OwnedByTwoCats · · Score: 1

      I wouldn't want solid rocket motor exhausts to fly right past my cryogenic tank and reentry system.

    16. Re:It is all of those things, but by Anonymous Coward · · Score: 0

      I would challenge your assessment. The failure mode of the only accident related to the SRB's was addressed, found to perform quite well, and performed more or less perfectly for the roughly 80 launches since then.

      Liquid engines can be just as dangerous as solids, and they have a lot more failure modes.

      If you look at causes of failure in both manned and unmanned launch vehicles that use SRB's, you will find very few of them were caused by the SRB.

    17. Re:It is all of those things, but by rbanffy · · Score: 1

      So, what's so wrong with the kerosene/lox choice of the Saturn V? Couldn't we build a bigger one with safer, less powerful, cheaper fuels?

  7. Build Both by Anonymous Coward · · Score: 1, Insightful

    Why build one when you can build two for twice the price?

    1. Re:Build Both by Kagura · · Score: 1

      This is a quote from Contact, and maybe something else. What is it supposed to mean? Although the sentence is easy to understand, it doesn't really make sense to me.

  8. A bit disingenuous by amliebsch · · Score: 2, Interesting

    I scoffed a bit at their description of the excess payload capacity of the crew-launch configuration as "free." I mean, you still pay for that capacity in fuel and delivery. You're not getting something for nothing. The Ares CLV has far less capacity but it should be far less expensive as well. And I'm not entirely persuaded that the costs of operating two launch systems will be that much greater than one combined system. We currently launch a wide variety of rockets for different purposes without it being cost-prohibitive. On the other hand, the Ares CLV really seems to be cutting to the bone, to the point where they've cut land-based recovery. If your goal is efficiency, reducing your CLV capacity to the point that you can only ever do expensive seaborne recovery seems like a false savings.

    --
    If you don't know where you are going, you will wind up somewhere else.
    1. Re:A bit disingenuous by notadoctor · · Score: 1

      The per launch cost of the DIRECT launcher would be lower than that of the Ares I, so in comparison, it would be free payload.

    2. Re:A bit disingenuous by rbanffy · · Score: 1

      "If your goal is efficiency, reducing your CLV capacity to the point that you can only ever do expensive seaborne recovery seems like a false savings"

      Just bill that to the navy's budget. It's not like a carrier picking up a spaceship out of the water is a whole lot more expensive than a carrier doing routine ops.

  9. I love it... by camperdave · · Score: 4, Funny

    You got to love it: By day, they are mild mannered engineers. By night, they are undercover rocket scientists who are building a rocket to go to the moon! It sounds like a pulp sci-fi story.

    --
    When our name is on the back of your car, we're behind you all the way!
    1. Re:I love it... by Anonymous Coward · · Score: 0

      Before: 2 Sith, 100s of Jedi.
      After: 2 Sith, 2 Jedi.

      Wrong.

      Before: 2 Sith, 100s of Jedi.
      In the middle: 2 Sith, 2 Jedi.
      Then: 2 Sith, 1 Jedi with a half-trained apprentice.
      Finally: 0 Sith, 1 Jedi.

      I mean, it's not like Luke offed the Emperor.

    2. Re:I love it... by R2.0 · · Score: 1

      "You got to love it: By day, they are mild mannered engineers. By night, they are undercover rocket scientists who are building a rocket to go to the moon! It sounds like a pulp sci-fi story."

      More like a juvenile, specifically "Rocketship Galileo". About as technically infeasible as you can get, but fighting Nazi's on the Moon with an M1 Garand? AWESOME!!!

      --
      "As God is my witness, I thought turkeys could fly." A. Carlson
    3. Re:I love it... by Anonymous Coward · · Score: 0

      Should be OK as long as the mission doctor isn't Zachary Smith!

  10. Engineers vs management by Fastfwd · · Score: 4, Insightful

    It's the old engineers vs management debate on who gets to make the decision. Seeing as both cost and speed are on the engineer's side I don't see why management would be against.

    oh wait I know

    Because it will make them look like they have been wasting time and money and they would rather waste even more money while looking like they are not.

    1. Re:Engineers vs management by DerekLyons · · Score: 4, Insightful

      It was engineers who did the ground work for Ares - it's not like management created the booster out of thin air and in secrecy and isolation.
       
      I often wonder how today's space fans would have reacted back in the 1960's - when the Saturn (V) initially ended up nearly a third larger than the Nova booster that was supposedly sufficient for a lunar landing mission... and then required a 20% performance increase on top of that in order to be barely able to conduct the mission.
       
      Everything is cheap and fast and easy - on paper. When you start getting off the page and bending real metal, they usually turn out not be fast, cheap, or easy.

    2. Re:Engineers vs management by Anonymous Coward · · Score: 5, Interesting

      Uh, no, actually that's exactly what happened. Griffin and Horowitz (the PHB's) came up with their Ares plan many years ago, did a 60 day "study" that came back with the recommendation to follow their plan, and ordered the MSFC engineers to build their designs, rather than the engineers' long standing plans to develop more conventional and cost-effective derivatives of the Shuttle (NLS/Magnum) or EELV.

      Back in the '60s, the NASA PHB's were at least smart enough to see that John Houbolt had come up with a solution to fix their performance gap. Today, the PHB's are too busy doing political spin to promote their preferred solution and hide the 7mT performance shortfall, the 6 year spaceflight gap, and the $1.4 billion to $2 billion per launch total cost.

      Thats one heckuva' job Mikey.

    3. Re:Engineers vs management by notadoctor · · Score: 1

      It's the management that actually chose the configuration. Most of the engineers are busting their brains trying to make the concept work, wondering why their managers didn't pick a more workable and affordable concept.

    4. Re:Engineers vs management by Thelasko · · Score: 1

      I don't know who this Anonymous Coward chap is, but it appears he may have some inside information at NASA.

      --
      One of our competitors trademarked the term "hypothesis". From now on, we will call them "boneheaded ideas".
    5. Re:Engineers vs management by strelitsa · · Score: 1

      The cynic in me screams that he's posting on company time. Your tax dollars at work.

      --
      No mod points, no meta-moderating/Firehose/all the other free work Slashdot wants me to do.
    6. Re:Engineers vs management by DerekLyons · · Score: 1

      Uh, no, actually that's exactly what happened. Griffin and Horowitz (the PHB's) came up with their Ares plan many years ago, did a 60 day "study" that came back with the recommendation to follow their plan, and ordered the MSFC engineers to build their designs,

      That's an interesting claim considering Griffin became NASA administrator only two weeks before the ESAS study was started.
       

      rather than the engineers' long standing plans to develop more conventional and cost-effective derivatives of the Shuttle (NLS/Magnum) or EELV.

      That's an interesting claim given that Magnum was an entirely brand new booster on the scale of the Saturn V (and never really was much of plan, just a few preliminary designs), and the EELV is a DoD Project - and the launchers produced under the project aren't noted for being anything resembling cost effective.
       

      Back in the '60s, the NASA PHB's were at least smart enough to see that John Houbolt had come up with a solution to fix their performance gap.

      Yet another interesting claim - especially since Houbolt's plan (LOR) required the Saturn V while the preferred plan of NASA management (EOR) required the Saturn I.
       
      Got any other ones?

    7. Re:Engineers vs management by Anonymous Coward · · Score: 0

      it's not like management created the booster out of thin air and in secrecy and isolation.

      Nope; that pretty much is what happened.

  11. Bad name. by Anonymous Coward · · Score: 0

    Am I the only one who thinks naming rockets after planets totally unrelated to their mission is stupid? Not that naming them after planets they are going to would be better...

    Maybe they could, you know, not name them after planets at all?

    1. Re:Bad name. by OldeTimeGeek · · Score: 1

      Because they wanted to make a Jupiter 2?

  12. If not public, then...? by ultraexactzz · · Score: 2, Interesting

    If NASA is unwilling to consider Jupiter as an alternative to Ares, then would there be private corporations willing to invest in what appears to be a good heavy-lift flight system? You might even find Russia or the ESA willing to purchase flights, either to service the ISS in the pre-Ares years, or to service an ISS v2, if and when. Pie in the Sky, perhaps, but I'm finding this to be an intriquing proposal, and it'd be a shame if it didn't end up flying.

    --
    Never underestimate the potential of Human stupidity. -Heinlein
    1. Re:If not public, then...? by rbanffy · · Score: 2, Insightful

      To conduct both projects in parallel would require building a couple more launch pads as the current shuttle/Jupiter-compatible ones will have to be changed for the Ares rockets.

    2. Re:If not public, then...? by moosesocks · · Score: 1

      Russia has (or at least had) a good heavy-lift system in the form of the Energia rocket.

      One of the primary advantages of Russia's shuttle system was that the Energia boosters didn't necessarily need to lift a shuttle. They could lift all sorts of other cargo.

      Its makers claim that they can still build one if there is the interest for it.

      --
      -- If you try to fail and succeed, which have you done? - Uli's moose
    3. Re:If not public, then...? by GrayNimic · · Score: 1

      The US has largely gotten out of the "Pay us to launch your stuff" business (relatively speaking). It's largely for "dual use" concerns - ie, we won't launch your nice peaceful SatilliteX because we're concerned it might be possible to use it for Military_or_Technological_Purpose_We_Don't_Like, or that the information you'd acquire via use of our launch vehicle might be applicable to aformentioned purpose. Therefore, we won't do business with you - go pay Russia, ESA, or one of the emerging launch-capable nations like India and Japan. It's been argued this is a rather unfortunate policy, as it's driven business from the US to other countries, and business => $$$ => development/research funding.

    4. Re:If not public, then...? by nasor · · Score: 1

      The whole point of their proposal is that since they are basically re-using existing shuttle tech, most of the infrastructure is already present at NASA, the NASA engineers already have expertise with it, and companies are already experienced at making it. If you took the design to another country/agency that didn't already have all that infrastructure, expertise, etc. it would lose much of its usefulness.

  13. Why so little tech recycling currently? by sokoban · · Score: 1

    Can anyone explain why so little technology is recycled from current and previous generation spacecraft in designing the new generation craft.

    It makes sense to use as much shuttle technology and durable facilities in constructing the next heavy lifting vehicle as the Jupiter people are proposing, so why wasn't that a goal from the start? The proven technology is well tested, and is well known by the folks who work on it, so why is there such a desire to change it?

    Also, why are the scaled composites tier 1b and tier 2 vehicles not being considered for delivering crew to orbit, to the ISS, or to a separately launched craft for lunar expeditions?

    --
    09 F9 11 02 9D 74 E3 5B D8 41 56 C5 63 56 88 C0 is the magic number.
    1. Re:Why so little tech recycling currently? by amliebsch · · Score: 1

      One reason more shuttle components are re-used (like the main shuttle engine) is cost - the shuttle components were quite expensive. Another is different design requirements, e.g., a main shuttle engine designed to run on liquid fuel and be started at 1 atmosphere is inappropriate for a rocket whose liquid-fuel engines have to be started in space.

      --
      If you don't know where you are going, you will wind up somewhere else.
    2. Re:Why so little tech recycling currently? by nospam007 · · Score: 1

      >Can anyone explain why so little technology is recycled from current and previous generation spacecraft in designing the new generation craft.

      Shuttles and priors are 70ies tech, they can't read the tapes anymore.

    3. Re:Why so little tech recycling currently? by Anonymous Coward · · Score: 0

      why are the scaled composites tier 1b and tier 2 vehicles not being considered

      Because they are SUB-orbital craft. That means they can't actually orbit the Earth. Kinda useless for reaching ISS which is... in orbit.

      o.O

      What Scaled Composites is working toward is essentially unrelated to anything NASA might need. SpaceShipX exposure to space is measured in seconds.

    4. Re:Why so little tech recycling currently? by Burdell · · Score: 5, Informative

      You should check the designs before you criticize them. Ares I uses an extended solid rocket booster (upgraded from the Shuttle) and a J-2X engine (upgraded from the Saturn V second and third stages). Ares V uses extended SRBs and RS-68 engines (from the Delta IV).

      The Shuttle main engines (SSMEs) were considered instead of the J-2X and/or the RS-68, but the cost was too high. The SSME is a high performance engine, but it is an expensive engine. Also, one concern for using it for the Ares I is that the liquid engine is the second stage engine, which will be started in-flight and at high altitude. The SSME has never been tried like that (nor was it designed for that), while the J-2 was used that way in the Saturn.

      As for Scaled Composites Tier 1b, it is a sub-orbital vehicle (good for nothing but tourists and hype). IIRC Tier 2 may be an orbital vehicle, but that is a long way off as well, since Scaled is working on Tier 1b (Ares is much further along in development).

    5. Re:Why so little tech recycling currently? by Anonymous Coward · · Score: 0

      Several factors:
      1) Lack of documentation or suppliers. No drawings exist for, e.g., Saturn V. Mfrs of various parts are long out of business.
      2) Technology has advanced. Shuttle was designed in the 60s and 70s. Materials, etc., have improved a lot in the last 30 years. Manufacturing technology has certainly improved (CNC, etc.)
      3) Shuttle engines are probably one of the highest performance, most efficient rocket engines ever made. They are incredibly expensive to make and maintain. Maybe a bit less performance and simpler designs might be a better "systems engineering" choice? Think race tuned Ferrari engine vs cast iron Chevy small block V8.

      IIRC Scaled Composites vehicles don't have the mass to orbit capability needed. Take a look at SpaceX's Dragon for a more practical alternative.

    6. Re:Why so little tech recycling currently? by bruce_the_loon · · Score: 1

      Consider recycling the Space Shuttle Main Engines (SSME) into the new launch vehicle.

      Yes, they have a number available. Three per surviving bird plus say six spares. Nine if we're generous. That's 15 to 18 engines in total. Say we strap three to an Ares V class vehicle. That stage isn't designed to be recoverable, adds way too much weight and complexity to do so. So we get 5 to 6 launches out of the current stock of engines. Then what, we need brand-new engines.

      The SSME is widely regarded as one of the most complex engines in existence. To build a new one is an expensive process compared to the simpler design of the RS-68 engine that is in the current design.

      The RS-68 was designed to be disposable, cheaper and simpler and there is already a production line tooled up for the RS-68 for the Delta IV.

      So medium-term, ten launches of the Ares V, clearly it is better to not recycle the engines.

      We are recycling the SRB systems. New nozzles and slightly different taper to the fuel package, but same segments, seals and firing systems.

      Avionics and so forth are fixed for the vehicle they were designed for, but I guess the designs and systems are being evolved for the new vehicles.

      Launch pads, crawlers, service structures are all being reused, as is the entire mission control facility.

      And if they don't nick the robot arms from the shuttles and stick them onto the new machines, they had better have new, more capable arms.

      --
      Trying to become famous by taking photos. Visit my homepage please.
    7. Re:Why so little tech recycling currently? by Vornzog · · Score: 1

      Actually, some of the very first Ares prototypes were based on the Atlas V, and the Russian designed RD-180 engines (which slightly outperform the RS-68s, and make anything shuttle derived look like a class-D model rocket engine). My wife worked on some of the prototype ground software systems.

      At the time, Lockheed (now United Launch Alliance) put in a serious proposal to man-rate the Atlas V. NASA scoffed, which strikes me as a little strange. The shuttle technology is based on a 30 year old design, is planned to top out at about 20 total missions, and has blown up two orbiters. Both Atlas and Delta have newer flight-proven technology, better launch track records then the shuttle, lower prices, etc. Delta has the capabilities to add additional stages, Atlas intends to shortly, and both Atlas and Delta can add additional liquid or solid boosters as needed to handle huge payloads.

      There is still noise about this idea now - click here for more information. But it won't happen.

      These rockets are not in development - they exist now, and have a similar or better performance profile to anything that Ares or Jupiter have been proposed to have. Yea, you'd have to add redundancy to some of the systems, but you wouldn't have to redesign.

      Meanwhile, who does have the capabilities to put people into space right now? The Russians, on well-engineered, cheap-to-produce ballistic missile-style vehicles. And while NASA flounders around redesigning 30 year old shuttle derived technology, and watching their launch date slip out for years, if not decades, we will be dependent on the venerable Soyuz keep Americans in space.

      NASA is technologically bankrupt. All the great engineers they had 30 years ago are in private industry. But they still have some of the best bureaucracy and politics!

      --

      -V-

      Who can decide a priori? Nobody.
      -Sartre

    8. Re:Why so little tech recycling currently? by sokoban · · Score: 2, Interesting

      Meanwhile, who does have the capabilities to put people into space right now? The Russians, on well-engineered, cheap-to-produce ballistic missile-style vehicles. And while NASA flounders around redesigning 30 year old shuttle derived technology, and watching their launch date slip out for years, if not decades, we will be dependent on the venerable Soyuz keep Americans in space.

      That's one thing that has puzzled me. Why not use soyuz capsules to ferry people to and from orbit where they can meet up with a semipermanent vehicle which remains in orbit and is resupplied by cargo launch vehicles?

      Supplying durable commodity goods to orbit, moving around while in orbit, ferrying humans to orbit, and returning them from orbit seem as though they would have vastly different needs as far as vehicles are concerned. Combining the crew to orbit and reentry vehicles makes sense because for every person sent to space, you hope to have one person return, but an orbiter vehicle parked in orbit in some sort of protective garage would seem to reduce the need to lift that heavy object every time and supplies are more expendable and often more durable than people.

      --
      09 F9 11 02 9D 74 E3 5B D8 41 56 C5 63 56 88 C0 is the magic number.
    9. Re:Why so little tech recycling currently? by sokoban · · Score: 1

      You should check the designs before you criticize them. Ares I uses an extended solid rocket booster (upgraded from the Shuttle) and a J-2X engine (upgraded from the Saturn V second and third stages). Ares V uses extended SRBs and RS-68 engines (from the Delta IV).

      Yeah, the Jupiter .pdf I read made it seem like a lot more stuff was being redesigned from the ground up and that the predominant advantage to the Jupiter craft was that it reused more already certified and proven technology.

      As for Scaled Composites Tier 1b, it is a sub-orbital vehicle (good for nothing but tourists and hype). IIRC Tier 2 may be an orbital vehicle, but that is a long way off as well, since Scaled is working on Tier 1b (Ares is much further along in development).

      Yeah, the more I learn about Scaled Composites, the less interesting they seem. Heavy on marketing, but light on actual new or innovative ideas.

      --
      09 F9 11 02 9D 74 E3 5B D8 41 56 C5 63 56 88 C0 is the magic number.
    10. Re:Why so little tech recycling currently? by sokoban · · Score: 1

      From the DIRECT Summary V 2.0.2 .pdf file on the Jupiter site:

      "This "DIRECT" Shuttle-derived launcher exceeds all VSE payload and safety requirements for Crew and Cargo missions to the International Space Station (ISS). It is capable of supporting all of the far larger VSE missions to the Moon, Mars, and Beyond. Compared to Ares, it significantly reduces development costs, schedule and risks, cuts the human spaceflight gap after the Shuttle retires in 2010 from 5 to 2 years, and retains the NASA and contractor workforce.

      DIRECT achieves this by minimizing new technology requirements. The Jupiter re-uses the unchanged human-rated Space Shuttle 4-segment Solid Rocket Boosters (SRB), the USAF Delta-IV RS-68 main engines, and converts the current Space Shuttle External Tank (ET) into a Core Stage atop which flies the new Orion spacecraft. In contrast, Ares-I requires development of new 5-segment SRBâ(TM)s, new J-2X engines, new Upper Stage and all-new manufacturing and launch facilities."

      --
      09 F9 11 02 9D 74 E3 5B D8 41 56 C5 63 56 88 C0 is the magic number.
  14. LOL... Shuttle Workers Want to Keep Jobs by tjstork · · Score: 1

    Read about the argument for this chumpy:

    # Delete all risks associated with a second new launch vehicle
    # Delete all costs associated with a second new launch vehicle
    # Optimum use of the existing NASA & contractor experience
    # Enable multiple upgrade paths

    Basically, "hey, we're NASA, we're too stupid to design a new rocket, and let's just use the shuttle that, um, we already have."

    I thought the whole point of Constellation was that the shuttle sucks. If the engineers had gotten the shuttle off the ground correctly to begin with, we wouldn't be having this conversation now, would we?

    --
    This is my sig.
    1. Re:LOL... Shuttle Workers Want to Keep Jobs by notadoctor · · Score: 2, Interesting

      The initial architecture of Constellation was based on the congressional requirement that NASA actually use Shuttle derived rockets. The moment the original architecture was rolled out, though, (space shuttle main engines, four segment solid rocket boosters, 28 ft diameter tank), NASA ditched both the SSMEs and the 4 seg SRBs. They couldn't air start the SSME, so they had to develop a new engine. (The J-2X sounds like the Apollo J-2, but they have very few components in common, and the J-2X is 30% more powerful.) Then, they dumped the SSMEs for the Ares V core vehicle, and replaced them with RS-68s from the Delta IV. That was a smart move because the cost is way lower. But, since the performance is lower, they had to enlarge the tank (read develop a brand new one.) Now, it's 33 ft in diameter, and requires all new tooling and massive modifications to the manufacturing, preparation and launch facilities. That costs a lot, too. All this after developing another much smaller but equally expensive Crew Launch Vehicle. So, while the Ares now has nothing in common with the Shuttle, it costs many times more to develop, and twice as much to operate. DIRECT does have the side effect of maintaining more jobs than Ares does in the near term, but in the long run, Ares would require more employees, and that is a large part of where the cost increase comes from. The extra money saved would be used to speed up the moon missions by two years, close NASA's manned spaceflight gap by three or four years, and perform more science missions.

    2. Re:LOL... Shuttle Workers Want to Keep Jobs by FromellaSlob · · Score: 1

      I thought the whole point of Constellation was that the shuttle sucks.

      Then you thought wrong. The Shuttle Orbiter sucks for various reasons, as does the general concept of bolting your vehicle to the side rather than the top of your launch system. There was never really much wrong with the launch system itself though. The suckiest thing about it was those pesky O-rings, but they wouldn't have failed if PHBs hadn't decided to operate them out of spec, and wouldn't have resulted in tragedy but for the aforementioned side-mounting. (And were re-engineered after Challenger anyway.)

  15. Never underestimate a motivated engineer by schwit1 · · Score: 5, Interesting

    A handful of engineers and a stenographer cooped up in a hotel room over a weekend, designed and developed the B52. And its still going strong 50 years later.

    After all, it not rocket surgery.

    1. Re:Never underestimate a motivated engineer by mazarin5 · · Score: 3, Funny

      After all, it not rocket surgery.

      So easy, even a caveman could do it?

      --
      Fnord.
    2. Re:Never underestimate a motivated engineer by BvF7734 · · Score: 1

      After all, it not rocket surgery.

      So easy, even a caveman could do it?

      That describes the Air Force and not NASA...

    3. Re:Never underestimate a motivated engineer by Joe+the+Lesser · · Score: 1

      Not Cool!

      --
      "I only speak the truth"
      Karma: null(Mostly affected by an unassigned variable)
    4. Re:Never underestimate a motivated engineer by DerekLyons · · Score: 1

      A handful of engineers and a stenographer cooped up in a hotel room over a weekend, designed and developed the B52.

      Designed and developed? ROTFLMAO. They came up with a (very) rough set of specifications and concepts - and then it took four years to work out all the details and then actually build the aircraft.
       
      Like all legends, this one has grown a bit over the years.

    5. Re:Never underestimate a motivated engineer by iamlucky13 · · Score: 1

      Careful about generalizing there. They did not design and develop the B-52. They created an engineering proposal. It established the basic design and confirmed it was physically possible, but there was several more years worth of work for several hundred or perhaps thousands of engineers before the B-52 even flew, and there's been quite a bit more engineering work in the 50+ years since then to keep the B-52 up to date and in good shape.

      Regarding the reply below about brain (or rocket) surgey being so easy even a caveman could do it, interestingly enough, they did. Ok, those aren't exactly cavemen, but the idea that brain surgery predates modern medicine by about 3000 years is pretty impressive.

  16. The moon and beyond... by xpuppykickerx · · Score: 1

    The only reason to go to the Moon is to construct a base to launch further into space. Do we honestly need more rock?

    The reason for the Moon base is so these giant rockets don't use all there fuel just escaping Earth's atmosphere and gravity. Launching from the Moon would reduce the fuel use and make us that much closer to Mars and such. But I guess they need to agree on a shuttle first.

    1. Re:The moon and beyond... by Last_Available_Usern · · Score: 1

      "Do we honestly need more rock?"

      Actually, we do.

      http://science.slashdot.org/article.pl?sid=08/07/13/1610210

    2. Re:The moon and beyond... by mudetroit · · Score: 2, Insightful

      The concept of using the Moon as a launching pad to go further into space is almost completely broken from the start. What fuel source for launching rockets is present on the moon to take advantage of? None really, so it becomes an excercise of launching from earth, using more fuel to slow it down and land it on the moon, and then yet more fuel to have it take off again.

      Explain why this is a good plan again?

    3. Re:The moon and beyond... by camperdave · · Score: 1

      The reason for the Moon base is so these giant rockets don't use all there fuel just escaping Earth's atmosphere and gravity. Launching from the Moon would reduce the fuel use and make us that much closer to Mars and such. But I guess they need to agree on a shuttle first.

      That makes absolutely no sense. Where are you going to get fuel on the Moon? There is none there. You'd have to bring it all from Earth. So why bring stuff up from Earth, and then down to the Moon, only to have to bring it up from the Moon, to go down to Mars, when you could just bring it up from Earth and then go down to Mars. Earth orbit is the cheapest place to launch from. Going to the Moon puts you farther away from Mars.

      --
      When our name is on the back of your car, we're behind you all the way!
    4. Re:The moon and beyond... by xpuppykickerx · · Score: 1

      way more than two jedi and sith btw.

    5. Re:The moon and beyond... by initdeep · · Score: 1

      except of course the thought that the surface of the moon (and mars too) could actually be used to create the required fuel.

      of course this is conjecture and not definitive yet.

      but it would allow for less fuel if possible.

    6. Re:The moon and beyond... by 2short · · Score: 1

      "conjecture and not definitive yet"

      Is that your way of saying "A ridiculous pipe dream with no supporting evidence whatsoever?" Mining and refining equipment is heavy, assuming there was anything on the moon to make fuel out of, which there does not appear to be to the best of our knowledge.

  17. Moon not only goal by Anonymous Coward · · Score: 1, Insightful

    Relative to the Ares I and V system, the proposed alternative "Jupiter" lacks the small lifter. Every launch, therefore, is a costly heavy lift.

    I suppose that's an improvement if your only goal is the Moon. NASA, however, has other obligations. They need a small, cheap lifter to crew and service ISS and perform other LEO only missions.

    So, yeah, you chop out half the program and save billions...

    Doesn't matter in the end. Obama will gut Ares; Ares I will be built for ISS use and Ares V will never get beyond drawings.

  18. We Already Have a Moon Rocket by Nom+du+Keyboard · · Score: 1

    We already have a man-rated safe moon rocket. It's called Saturn V.

    --
    "It's the height of ridiculousness to say for those 9 lines you get hundreds of millions."
    1. Re:We Already Have a Moon Rocket by Nimey · · Score: 3, Informative

      No, actually we don't. The tooling's been long-since destroyed, and there are no blueprints for many of the parts because they were farmed out to contractors, let alone information on things like what precise alloys to use for said parts, and other methods of manufacture.

      There are a couple Saturn Vs left, yes, but they were left out to the elements for many years and may have been scavenged for parts.

      --
      Hail Eris, full of mischief...

      E pluribus sanguinem
    2. Re:We Already Have a Moon Rocket by Anonymous Coward · · Score: 0

      We already have a man-rated safe moon rocket. It's called Saturn V.

      Actually no. Many of the original design files were lost. Engineers are disassembling and analyzing the Saturn V in order to rebuild them.

      How something was designed is not as important as why it was designed that way.

    3. Re:We Already Have a Moon Rocket by johnny+cashed · · Score: 1

      Not only that, but we used to have one example of flight rated Saturn V hardware. Of course, it had been stored outdoors for several decades, so I don't think it would be flight rated anymore. There are a few other bits and pieces of other Saturn V hardware around, but not all of it was flight rated.

    4. Re:We Already Have a Moon Rocket by Extremus · · Score: 1

      I don't know if it could be rated as SAFE. In fact, all this man-to-the-moon adventure some times sounds to me as a cheese version of that cake lie.

    5. Re:We Already Have a Moon Rocket by Amouth · · Score: 1

      i higly doubt that that is the case - i have seen alot of the work that was done on the Saturn V - there is no doubt in my mind that if they wanted to build another they would know exactly what to make and how to make it and how to put it together.

      --
      '...if only "Jumping to a Conclusion" was an event in the Olympics.'
    6. Re:We Already Have a Moon Rocket by willith · · Score: 5, Informative

      No, actually we don't. The tooling's been long-since destroyed, and there are no blueprints for many of the parts because they were farmed out to contractors, let alone information on things like what precise alloys to use for said parts, and other methods of manufacture.

      You are wrong. The blueprints for everything, down to the last nut and bolt, are on file at MSFC. Source.

      There are a couple Saturn Vs left, yes, but they were left out to the elements for many years and may have been scavenged for parts.

      You are wrong. There are three, but none of them is "one" rocket. The one at the Johnson space center, made up of three flight-rated stages from different rockets, was left out for 20+ years but has been restored to pristine (though obviously not flight-worthy) condition. The one at MSFC is all static test stages and has been similarly restored. The one at KSC is two flight stages and one test stage, and has been kept in perfect (but again, obviously not flight-worthy) condition since the day it was rolled in. NONE of the rockets were ever "scavenged" for parts--they're all property of the Smithsonian and are maintained in trust as artifacts by NASA.

      Recreating a Saturn V isn't impossible because we don't have the plans--it's impossible because the blueprints call for standard parts and items that don't exist any more (like a left-handed widget with widget gauge #12, which was used by, say, Boeing in 1960, but not any more).

    7. Re:We Already Have a Moon Rocket by khallow · · Score: 1

      I don't see where your optimism comes from. The poster you replied to has already explained why NASA doesn't have the ability to do what you say they can do. No tooling, missing blueprints, and most of the people who worked on the Saturn V are dead.

    8. Re:We Already Have a Moon Rocket by toby · · Score: 4, Funny

      How something was designed is not as important as why it was designed that way.

      You're one of those people who COMMENT THEIR CODE, aren't you! :-)

      --
      you had me at #!
    9. Re:We Already Have a Moon Rocket by khallow · · Score: 1

      Ok, I read some of other posts in this thread and NASA claims it has all the blueprints. Even assuming this is true, they still need a bunch of 60's era basic parts which currently aren't made any more.

    10. Re:We Already Have a Moon Rocket by e03179 · · Score: 2, Insightful

      If "a left-handed widget with widget gauge #12" is the "impossible" that keeping a Saturn V from flying, then I'm guessing there's a mom and pop engineering company around here somewhere that would gladly make the part for NASA.

      --
      -516
    11. Re:We Already Have a Moon Rocket by daveime · · Score: 1

      So rather than take the plans for the left hand widget and turning it out on a milling machine, we spend billions in reinventing the widget because a wodget is "so much more advanced you know, and we can definately do what we did 40 years ago in a nother 10 years minimum".

      Progress, isn't it wonderful ...

    12. Re:We Already Have a Moon Rocket by goodben · · Score: 1

      Saying that we can use Saturn V to go back to the moon is like saying we don't need new cars because the Rambler is a proven automobile.

      Saturn V used 50+ year old electronics and systems. It would take a substantial effort to redesign, remanufacture, and requalify the parts that they used. Who makes vacuum tubes any more? You could redesign a Saturn V just like you could redesign an AMC Rambler, but why would you when you can design a system based on existing technology? The Ares rockets will use engines and systems in use today rather than that last used 30 years ago.

    13. Re:We Already Have a Moon Rocket by michaelz · · Score: 1

      I don't think that's a problem. It probably wasn't mass-production anyway. Besides with projects like http://fabathome.org/ they can just print the parts ;)

    14. Re:We Already Have a Moon Rocket by isorox · · Score: 1

      How something was designed is not as important as why it was designed that way.

      You're one of those people who COMMENT THEIR CODE, aren't you! :-)

      I comment -- for example
      // WTF does this do
      // What was I thinking?
      // Function to do something

    15. Re:We Already Have a Moon Rocket by willith · · Score: 2, Insightful

      You going to find a "mom and pop engineering company" to duplicate IBM's work and make another Instrument Unit to fly it? Manufacture two tons of 1960s-vintage analog computers and gyroscopes? Rebuild equipment designed to determine the rocket's launch azimuth based on star sightings, not GPS like we'd use today? What about all the other analog and early digital equipment that's integral to the design? It's not just a giant fuel tank and some engines--it's a launch vehicle. It's got a flight manual, and it's designed to be used in conjunction with an Apollo command and service module pair flying it.

      Re-design the rocket to use new technology? By the time you've de-Apollo'd Saturn, you've made a whole new launch vehicle. Which is exactly what Ares is.

      The Saturn V is an awesome piece of technology, yes. An awesome piece of 1960s technology. Rebuilding it today would not work, period, no matter how cool it might be.

    16. Re:We Already Have a Moon Rocket by ChrisA90278 · · Score: 1

      Even if you were right and a Saturn V could be found or re-built you would not want ot use it. The saturn V was designed to place a small minimal size lander on the moon for a short stay. Now we want to send something MUCH larger to the moon.

    17. Re:We Already Have a Moon Rocket by khallow · · Score: 1

      This is unrelated, but I think it'll be a while before rapid prototyped parts are used in high performance activities like rocket launches. There isn't a lot of overengineering in rocketry and mass is extremely limited. So a rapid prototyped part might not be strong or light enough for the application. OTOH, it is easy to make peculiarly shaped parts with mass shaved from unnecessary locations.

    18. Re:We Already Have a Moon Rocket by rbanffy · · Score: 1

      It's every bit as safe as strapping yourself to a rocket that can take you to the Moon could be.

    19. Re:We Already Have a Moon Rocket by RalphTheWonderLlama · · Score: 1

      Don't come any closer with that razor!

      --
      simple, fast homepage with your links: http://www.ngumbi.com/
  19. Well, when the Jupiter 2 is built. by Anonymous Coward · · Score: 0

    They need to be careful that it doesn't get lost in space.

  20. Hope this project isn't lost. by Bocaj · · Score: 1

    Some of our best innovations come from engineers that are driven to do something different. It usually doesn't come from a corporate cog. I just hope this Jupiter isn't lost in the space between NASA directors ears.

  21. NASA will crash this into the moon by Anonymous Coward · · Score: 1, Insightful

    It will probably crash into the moon. Notice the units in the presentation are a mix of english (pounds per square foot) and metric (kilograms). Last time they did this they crashed a probe into Mars.

  22. Why not make it a real alternative by Anonymous Coward · · Score: 0

    ... and stick NERVA or DUMBO on it? Let's get rid of the excessive propellant to cargo ratios.

  23. There is benefits from this even if never used by director_mr · · Score: 1

    The beauty of this proposal is that even if it is never used, it will pressure the ares developers to do even better. Competing designs tend to improve end products.

  24. Delta IV by Anonymous Coward · · Score: 0

    I don't understand why they don't upgrade an existing and proven system like Delta IV for a crew launch vehicle... why design a new launcher at all?

  25. It is a better system than Aries by caseih · · Score: 1, Redundant

    If you look at the overviews of their ideas, you can tell right away that this launch system would have several advantages over Aries. It does not require a modification of the boosters, which is one of the more significant design challenges that Aries, especially the crew lift system, is facing. Additionally they don't call for a significantly different vehicle to lift the crew. While they do propose a few different systems for lifting cargo vs lifting cargo and people, the base vehicle engineering is the same, unlike the Aries system. In short, it really looks like this Jupiter system is more flexible, maybe cheaper, and certainly easier than Aries is turning out to be. I also think that Jupiter could be built, tested, and launched quicker than Aries.

    This group's ideas are not new though, they proposed them a few years back, but NASA seemed to be set on Aries from almost the very start for some odd reason.

    1. Re:It is a better system than Aries by 99luftballon · · Score: 1

      Agreed, the basic principles look sound and it reuses working technology rather than the Ares probe, which seems to be about reinventing the Saturn system 50 years down the line. But I fear Nasa bureaucracy will chew this idea and spit it out, because it isn't Ares and look, they have all these lovely pictures of how it might work, ten or so years down the line. Besides, engineers never have good idea, that's for officials to do.

  26. One more.... by mlwmohawk · · Score: 5, Insightful

    After getting most prized "first post" position, I have one more...

    I would trust a set of napkin drawings from dedicated engineers more than I'd trust a polished proposal from a committee of military contractors and NASA administrators.

    Think of it this way, the latter said the O rings were safe, the former tried to warn everyone of the danger.

    1. Re:One more.... by mlwmohawk · · Score: 1

      Yeah. The EXACT same people infact. Fuck you clown.

      I wasn't going to respond, but lets just say that military contractors and NASA administrators have a different set of objectives and motivations than a set of engineers and scientists. ESPECIALLY under this administration.

    2. Re:One more.... by DerekLyons · · Score: 1

      I would trust a set of napkin drawings from dedicated engineers more than I'd trust a polished proposal from a committee of military contractors and NASA administrators.
       
      Think of it this way, the latter said the O rings were safe, the former tried to warn everyone of the danger.

      That's what the urban legend would have you believe.
       
      In reality, O-ring erosion was occurring from the first static firings of the SRB - and the engineers told management that it was OK as the ring hadn't completely eroded through. Rather than fixing the problem causing the erosion (poor joint design) the engineers added a backup O-ring whose design function relied on the primary O-ring not failing during the first few dozen milliseconds after ignition. Despite ongoing problems with joint erosion - the engineers insisted it was safe to fly while they developed a fix. (Which is why after the loss of Challenger they were able to identify the failure and the fix so fast - it wasn't a miracle by the engineers, they'd been working on it for the better part of decade.)
       
      Would you trust someone who kept telling you one thing, and then at the penultimate hour changed their story?

    3. Re:One more.... by Anonymous Coward · · Score: 0

      Citation, if you please, Mr. Ass-Clown, since a previous post provided a citation showing that they are not, in fact the same people.

    4. Re:One more.... by mlwmohawk · · Score: 1

      In reality, O-ring erosion was occurring from the first static firings of the SRB - and the engineers told management that it was OK as the ring hadn't completely eroded through.

      It was an off the cuff remark, I based it on my own recollection. From my personal memory, the engineers were concerned but the administrators used the argument that they hadn't burned through so that there was a "margin of safety." The engineers were told to shut up or lose their jobs.

      We can debate the facts, and while I believe my recollection is more accurate, it isn't worth a debate. The point was that I believe that competent engineers with an idea are more likely to be right than a bunch of suits.

    5. Re:One more.... by DerekLyons · · Score: 1

      We can debate the facts, and while I believe my recollection is more accurate, it isn't worth a debate.

      Your recollection is based on years of urban legend. My recollection is based on actually studying the facts.
       
      But facts don't seem to be your long suit - you prefer bias.

      The point was that I believe that competent engineers with an idea are more likely to be right than a bunch of suits.

      Going back to your original post, who do you think prepared the proposal for the 'suits' ("a committee of military contractors and NASA administrators")?
       
      Hint: Engineers.

    6. Re:One more.... by mlwmohawk · · Score: 1

      Your recollection is based on years of urban legend. My recollection is based on actually studying the facts.

      Sigh, and which "facts" are these? Seriously, it happened a LONG time ago and while I actually watched the live broadcast, what has been written and documenting since has, at best, been contradictory.

      But facts don't seem to be your long suit - you prefer bias.
      Don't be an idiot, you know absolutely nothing about me or my preferences.

      Going back to your original post, who do you think prepared the proposal for the 'suits' ("a committee of military contractors and NASA administrators")?

      You must know that there are NO public reports that aren't carefully edited and re-written for public consumption. I'd be surprised that there was any meaningful engineering input.

      In the Reagan years, as today, public agencies like NASA were under a lot of pressure.

  27. Danger, danger...Will Robinson! by PortHaven · · Score: 1

    Worked for "Lost In Space"

  28. I don't get it... by coolmoose25 · · Score: 1

    Basically as I understand it, this Jupiter thing is essentially the same rocket as the Ares V... Both would be heavy lift boosters in the Saturn V/Energia class... So while NASA wants to build an additional simplified Ares 1 that only lifts the crew module, the Jupiter people want to essentially put the crew module on top of the EDS and put it up in one shot - ala Saturn V... But what is so different from Ares V and Jupiter? They both seem to use both SRB and Liquid rockets... Basically it seems that they are against Ares 1 - for whatever reason, they don't like having the CEV on top of a modified SRB... But lets face it, the SRB's have essentially been flawless... (Okay, I'll get modded down and pounced on by the "Don't you know that the SRB caused the Challenger to explode!" crowd. But if you think about that failure, the SRB was only the match. It cooked off the liquid propellent tank after gasses escaped through the o-ring... but Ares 1 won't have anything hooked up to its side... an o-ring leak would not be catastrophic... the cause of Challenger's problem was having an SRB NEXT TO the liquid propellent external tank... Isn't that what both Jupiter and Ares V are set up for? And if so, do you want the PEOPLE riding on that, or just the machine to take them to the moon???)

    --
    Brawndo: It's what plants crave!
    1. Re:I don't get it... by initdeep · · Score: 1

      ummm
      google delta rocket explosions.

      they are pretty catastrophic.

      and the people in cape Canaveral that had pieces fall on their cars want to talk to you.
       

    2. Re:I don't get it... by Anonymous Coward · · Score: 1, Interesting

      Looks are very deceiving in this case. Jupiter, Ares V, and the current shuttle stack all have big orange fuel tanks, and white SRB boosters. But Ares V requires billions for completely new SRB boosters and a completely new (wider and longer) fuel tank, plus billions worth of new facilities and infrastructure for handling this bigger rocket. The Direct Jupiter instead proposes retaining the exact same SRB boosters and the same size fuel tank as the Shuttle, and retaining the current shuttle infrastructure at KSC with minimal changes.

      Rather than launching one little rocket (Ares I) and one huge rocket (Ares V) for each lunar mission (and having to pay for the billions of development and fixed costs for each of these rockets), Direct proposes launching two identical not-too-big but not-too-little Jupiter 232 rockets for each lunar mission.

      In doing so, Direct results in a rocket that NASA can afford to build and sustainably operate (unlike Saturn V or Ares V). Direct also reduces the gap between the Shuttle and its successor from 6 years down to about 2 or 3.

      The root design flaw that doomed both Challenger and Columbia was having the crew vehicle mounted in the potential debris path of the SRB and fuel tank. That's why all of these new designs show a small Orion capsule with an emergency abort system mounted on the top of the stack and as far away from the engines as possible. Direct offers the additional protection of being able to put several tons of ballistic armor between the crew capsule and the fuel tank - an option that Ares I can't provide.

    3. Re:I don't get it... by coolmoose25 · · Score: 1

      Okay... good points... but I'm still not convinced... Ares I is being designed not just for lunar missions, but for LEO missions (ex: Space Station missions) as well. If we only built Jupiter, we'd need to use it for the LEO missions, and its unnecessarily big for that. I get that the SRB's in Jupiter are reused Shuttle ones - that is a blessing in your mind, perhaps a curse though. The existing SRB's are VERY reliable (never cut out early, never blew up), but the o-rings were still problematic. Is it possible that redesigned, bigger SRB's that would essentially be Ares I could be made with better o-rings? Without better o-rings in either SRB, you run the risk of igniting the main tank. No matter how you slice it, if you ride a single SRB up to orbit, that is likely the least risky scenario for the crew. Jupiter ensures they always have that "oops, the main tank just blew up" problem. Ares I will never have that happen. Given that we KNOW it CAN fail that way, I think Ares I is the way to go.

      --
      Brawndo: It's what plants crave!
    4. Re:I don't get it... by Jeff1946 · · Score: 2, Informative

      The SRB's have a good track record. Only one failure in 100+ launches. Cause of the failure identified and fixed so it should not be factored into reliability calculations. Unless some new system is significantly cheaper in the long run,then stick with the SRB's for a heavy lift vehicle. Remember they are recovered after launch and reused. The steel cylinders (about 1/2" thick walls) are taken apart and refilled with propellant and reassembled. All the infrastructure to do this is already in place.

      Whether people need to go to the moon or Mars is another question. If not do we need heavy boosters in the first place?

    5. Re:I don't get it... by Anonymous Coward · · Score: 0

      The O-ring joints were redesigned after Challenger, and post-flight inspections of every SRB have found that problem to be well solved. Both Ares I and Jupiter would use the same existing shuttle SRB casings, with the current O-Rings. Ares, however, requires an extensive development plan for new nozzles, propellant grain design, oscillation dampers, and recovery systems.

      Both Ares I and Jupiter follow a similar strategy to reduce risk by putting the crew at the top of the pointy end of the rocket, away from the engines and fuel, instead of right beside the fuel and in the potential debris path of a rapid unscheduled disassembly. Both plan to have the crew capsule outfitted with an emergency abort motor that would pull the crew away from the rocket at very high speeds in the case of a problem.

      The Jupiter 120 will cost about $130 million per LEO mission to the ISS, compared to about $110 million for the Ares I. But despite these marginally higher variable costs from using a bigger rocket it saves about $35 billion overall in development and operating costs.

  29. Simple, as in "leverages existing systems" by OmniGeek · · Score: 5, Informative

    I *am* a rocket scientist, BTW. I read the Jupiter concept doc a few months ago, and I find it reasonably persuasive. The thing that makes the Jupiter concept "simpler" is that it reuses existing designs (specifically, main engine systems and fuel tanks) that have already been fully developed and put into use, rather than designing new ones that employ untested techniques.

    What makes a design safer isn't necessarily lowest component count; in the space business, proven designs count for a LOT in risk mitigation. Consider the Russian Proton rocket: not modern, not the most efficient, but a very reliable system that gets its job done at low cost (assuming that the recent Soyuz QA problems don't mean that their whole production infrastructure has gone rotten from lack of funds). Incremental changes are almost always faster, better, and cheaper than radical design departures (at least until the radical tech is fully worked out, which takes time).

    Indeed, a big part of the argument here is that Ares junks an existing manufacturing infrastructure THAT WORKS, just like NASA did after the Apollo program. Jupiter, on the other hand, maintains the current Shuttle-related tech base and builds on it. Having a functional tech infrastructure to build on, with suppliers who've been designing and delivering product based on the same design for many years, is an immense advantage in terms of cost, lead time, and reliability. Folks who've made the same system dozens of times make fewer mistakes than those building something brand-new with no comparable predecessor product.

    --

    "My strength is as the strength of ten men, for I am wired to the eyeballs on espresso."
    1. Re:Simple, as in "leverages existing systems" by prisoner-of-enigma · · Score: 5, Interesting

      in the space business, proven designs count for a LOT in risk mitigation.

      Very true, which is why the Shuttle continues to fly with 1970's-era technology controlling most of it.

      However, I would posit the following: the Shuttle program dumped most of Apollo in the trash bin and started with something new. I'm of the opinion that what we ended up with was not an improvement over Apollo. The Shuttle is more expensive, more finicky, less reliable, and arguably much more dangerous than Apollo ever was. So, while we have a large body of knowledge centered around Shuttle systems, the systems themselves may not be worth prolonging through to Ares. Hence the justification for breaking with the (Shuttle) past with Ares.

      The Shuttle was a great experiment, but ultimately we learned it was something we shouldn't have built. Everything it's done in the last quarter century could've been done better, faster, and cheaper with Apollo-era tech (with incremental improvements as you alluded to earlier) just as the Russians have proven with their launch systems.

      No human has been out of low Earth orbit in roughly thirty years. The last three that did, did so on top of a Saturn V. The Shuttle has had us going in circles (literally) since then. The ISS prolongs that boondoggle. Why do we need an ISS? To give the Shuttle some place to go! Why do we need a Shuttle? To build the ISS! What fantastic circular logic. What a horrific waste.

      --
      In the end they will lay their freedom at our feet and say to us, Make us your slaves, but feed us. - Fyodor Dostoyevsky
    2. Re:Simple, as in "leverages existing systems" by Thelasko · · Score: 5, Informative

      Incremental changes are almost always faster, better, and cheaper than radical design departures (at least until the radical tech is fully worked out, which takes time).

      As an engineer, I agree with that statement. I wish to add that the team knows, and has addressed the current failure modes of the technology they are planning to use by relocating the payload to the top of the craft.

      I will also point an error in the grandparent's post.

      The Jupiter are looking to use 2 shuttle boosters and the center fuel tank with shuttle engines mounted on it to put a crew into space, while NASA is using only one booster and one engine for the 2nd stage.

      They are planning to use the RS-68 engine, which is considered superior to the space shuttle main engines. These engines are currently in use on the Delta IV. The engine NASA is planning is yet to be developed, but based on the J-2 from the Saturn V.

      --
      One of our competitors trademarked the term "hypothesis". From now on, we will call them "boneheaded ideas".
    3. Re:Simple, as in "leverages existing systems" by dpilot · · Score: 2, Interesting

      > The ISS prolongs that boondoggle.

      IMHO the ISS is valuable as an engineering experiment. Yes, we're having a really tough time making the thing run, so what makes people think that we can make some different space station run better? The ISS is barely above the tin-cans-bolted-together stage, so we're a LOOOOONG way away from Von Braun's wheels.

      There is a rough maximum size we can launch from Earth, so if we want to do more, at some point we're going to have to be doing some serious construction in space. That's especially true if we want to quite sending everything up, and start using space-based resources, like asteroid mining. Maybe the ISS isn't much, but it's a first step, we're having a tough time doing it, and we have to master all of these things before we can do anything tougher. That said, I do wish the TransHab was still going to be attached.

      --
      The living have better things to do than to continue hating the dead.
    4. Re:Simple, as in "leverages existing systems" by Picass0 · · Score: 2, Interesting

      Looking at the Jupiter design and the Ares V, they look to the untrained eye to be very similar. I see a shuttle liquid oxygen tank on both designs, SRBs on both, aft skirt thrust modules on both, and similiar configurations for the upper command modules and payload.

      The Jupiter uses some delta engines. The Ares doesn't.

      Asided from that what are the major differences? More importantly, why should we feel one of these projects offers a great advantage? The Jupiter paper talks as if NASA is heading down a bad path, but it looks like they both are using shuttle bits.

    5. Re:Simple, as in "leverages existing systems" by cowscows · · Score: 2, Interesting

      While I'll agree that in the context of expanding humanity's abilities in space, the shuttle didn't live up to the hype, I don't think it's fair to say that the only thing we learned from it was that it was a bad idea. The shuttle is made up of a bunch of very well engineered components, they're just all stuck together into an overall package that isn't that useful. Sure, the next generation of spacecraft doesn't need wings. But that doesn't mean that technology developed for the shuttle's engines isn't better than Apollo era engines.

      Sometimes through great design you can end up with an end product that's greater than the sum of its parts. The flip side of that is that you can take all of the nicest parts in the world and still make a piece of junk out of it. There's lots of good technology in the shuttle, stuff that's well designed and heavily tested. I'm sure there's plenty of value in there.

      --

      One time I threw a brick at a duck.

    6. Re:Simple, as in "leverages existing systems" by MightyYar · · Score: 1

      I think it's really cool that we have a forum here where people who are actually rocket scientists participate. :)

      I was under the impression that the crew vehicle portion of Ares (Ares I?) is derived from the space shuttle and Apollo. The 1st stage is a modified booster, and the second stage engine is a modified J-2... right? I understand that there is some risk in designing the rest of the 2nd stage from scratch - but isn't that countered by this alternative proposal's doubling of boosters and engines?

      So where does Jupiter improve on Ares I from a re-use or safety perspective?

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    7. Re:Simple, as in "leverages existing systems" by Tablizer · · Score: 2, Funny

      the shuttle didn't live up to the hype

      Hell, what does?
             

    8. Re:Simple, as in "leverages existing systems" by MightyYar · · Score: 1

      IIRC, the shuttle's engines are really impressive, but the design process is taught as how NOT to run an engineering program.

      Also, with the Ares I (manned) portion of the project, efficiency takes a back seat to reliability - and I don't think there is any question that the Apollo-era engines are more reliable.

      For the heavy lifter, Ares V, efficiency is much more important. But even here, the shuttle engines are not ideal because they are very expensive and Ares V is not reusable. They are using some new engine that was developed in the 90's for other expendable launchers. The Apollo-era stuff is only being used in the upper stage, where it's performance is actually pretty good in the high altitude IIRC.

      The only problem with my little rant is that I think they eventually plan to use the heavy lifter with manned stuff (though maybe without the boosters).

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    9. Re:Simple, as in "leverages existing systems" by khallow · · Score: 3, Informative

      For starters, there is thrust oscillation. In theory, that is an issue for the Shuttle, Ares V, and DIRECT (what is called "Jupiter" in this story), but these other vehicles have much more mass relative to the sold rocket motors' (or SRM) thrust and two unsynchonized solid rocket motors. This issue won't even be properly tested until the first 5-segment Ares launches some time around 2013.

      Second, the Ares I and V use a new 5 or 5.5 segment variant of the SRM and a new rocket engine under design called the J-2X. DIRECT uses the 4 segment SRM just like the one used on the Shuttle and the well tested RS-68 motor.

      Finally, using DIRECT, there are no mass issues with the CEV. But Ares I can barely lift the CEV. Already signficant redundancy has been stripped from the lunar version of the CEV and they apparently still have a too heavy heat shield. That means that the choice to use the Ares I is at the expense of adding risk to lunar missions which are already much higher risk than launching people into space is.

    10. Re:Simple, as in "leverages existing systems" by bruce_the_loon · · Score: 1

      Ares V does use the Delta engines, same as Jupiter. RS-68's.

      Difference is that Jupiter uses Space Shuttle Main Engines as the first stages. More expensive than the RS-68 once you run out of the current stock NASA has. Jupiter replaces the J2-X second stage engine with an RS-68. Which you could do on the Ares as well if they wanted to.

      --
      Trying to become famous by taking photos. Visit my homepage please.
    11. Re:Simple, as in "leverages existing systems" by bruce_the_loon · · Score: 1

      This issue won't even be properly tested until the first 5-segment Ares launches some time around 2013.

      They have test-fired a five-segmenter horizontally already and there is a full 5-segment test, Ares 1-X, scheduled for 1st half of 2009. That will have a dummy second stage, but it is the full 5-segment rocket.

      --
      Trying to become famous by taking photos. Visit my homepage please.
    12. Re:Simple, as in "leverages existing systems" by DerekLyons · · Score: 2, Informative

      What makes a design safer isn't necessarily lowest component count; in the space business, proven designs count for a LOT in risk mitigation.

      The problem being that Jupiter/DIRECT is just as proven as Ares - that is to say, not at all. While it reuses a few components unmodified, the large remaining balance of reused components are modified (sometime considerably) which takes it right out of 'proven' category.
       
       

      Consider the Russian Proton rocket: not modern, not the most efficient, but a very reliable system that gets its job done at low cost (assuming that the recent Soyuz QA problems don't mean that their whole production infrastructure has gone rotten from lack of funds).

      Keep in mind that 'very reliable' equates to 'reliability essentially equivalent to that of the Shuttle'. One of the conundrums that various bodies and persons involved or interested in space travel shy away from examining is this paradox - cheap and limited in capability or expensive and highly capable, the failure rates keep coming out roughly the same.

    13. Re:Simple, as in "leverages existing systems" by MightyYar · · Score: 1

      I thought that Ares IV was the response to Ares I not being powerful enough?

      In any event, some work would needs to be done before the RS-68 is man-rated, right?

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    14. Re:Simple, as in "leverages existing systems" by Shivetya · · Score: 1

      I was under the impression that one of the big reasons for a new launch system was the using the Shuttle style engines was too expensive.

      --
      * Winners compare their achievements to their goals, losers compare theirs to that of others.
    15. Re:Simple, as in "leverages existing systems" by notadoctor · · Score: 1

      One difference is that Ares V doesn't use a shuttle external tank, or anything like it. It uses a much thicker and longer tank that has the same orange foam on the outside. Another difference is that Ares V doesn't use shuttle solid rocket boosters. It uses new longer boosters that (might) use the same sized steel (maybe, still up for debate) casing.

    16. Re:Simple, as in "leverages existing systems" by Anonymous Coward · · Score: 0

      No, it is NOT the same.

    17. Re:Simple, as in "leverages existing systems" by khallow · · Score: 1

      They have test-fired a five-segmenter horizontally already and there is a full 5-segment test, Ares 1-X, scheduled for 1st half of 2009. That will have a dummy second stage, but it is the full 5-segment rocket.

      Ares I-X does not test the five segment motor. It is a standard four segment motor with a dummy fifth segment and a dummy upper stage.

    18. Re:Simple, as in "leverages existing systems" by khallow · · Score: 1

      I thought that Ares IV was the response to Ares I not being powerful enough?

      Hmmm, is it being seriously considered? Just sounds like an off-the-wall idea. Any solution that requires NASA to fly three special purpose launch vehicles at once, even if they have considerable reuse of components among them, probably isn't going to work. We don't even know for sure that NASA will fly the Ares I or Ares V. But it would solve the mass problem with manned lunar missions.

      In any event, some work would needs to be done before the RS-68 is man-rated, right?

      I doubt it'll be any worse than the five segment solid rocket motor in the Ares I configuration. Plus the RS-68 flies now on the Delta IV. So there's a good record of its performance and reliability.

    19. Re:Simple, as in "leverages existing systems" by prisoner-of-enigma · · Score: 2, Insightful

      The shuttle is made up of a bunch of very well engineered components, they're just all stuck together into an overall package that isn't that useful. Sure, the next generation of spacecraft doesn't need wings. But that doesn't mean that technology developed for the shuttle's engines isn't better than Apollo era engines.

      That depends on your definition of "better." Do the SSME's produce more thrust than any other similarly-sized liquid fuel rocket yet flown? Yes. Their efficiency and power are unmatched. However, an F1 racing engine produces far more power from a 2.4L V8 than anything you can buy on your dealer's lot. It also costs 100x-1000x as much and only lasts for a few hundred miles between overhauls. Yet despite the incredible power and efficiency of the SSME's, the Shuttle can only lift a fraction of what the Saturn V could with its "primitive, inefficient, non-reusable" engines.

      What about the heat tiles? Are they "better" than ablative, non-reusable materials? Operational evidence says no. The tiles are fragile, as Columbia found out. They are difficult to maintain, requiring significant overhaul between missions.

      Other than its engines and re-usable nature, there is very little on the Shuttle that departs from the typical rocket formula (except for the wings that we no longer want or need). If I'm missing something notable, please point it out. There's nothing in it or on it that's demonstrably "better" than either its predecessor or successor. In fact, Ares pretty much repudiates the entire idea. So, I'd again say that while we learned to build some interesting things during the Shuttle program, ultimately we've gained very little from the whole experiment.

      --
      In the end they will lay their freedom at our feet and say to us, Make us your slaves, but feed us. - Fyodor Dostoyevsky
  30. Outsource it to Burt Ratan, Problem Solved. by deweycheetham · · Score: 1

    Why don't they just outsource it to Burt Rutan and get out of his way. I don't trust NASA to manage its back to the moon. Their track record hasn't been that good as of the last 20 years.

    1. Re:Outsource it to Burt Ratan, Problem Solved. by Waffle+Iron · · Score: 1

      Why don't they just outsource it to Burt Rutan and get out of his way.

      Because as of yet he has only achieved a small subset of what the X-15 had already accomplished by 1963.

  31. There are other small lifters. by argent · · Score: 1

    But there are other small lifters, if launching something the size of the shuttle is wasteful. Some aren't even Russian!

    Of course launching something the size of the shuttle is the only current option, isn't it?

  32. You know who else... by Anonymous Coward · · Score: 0

    ...wrote his project for humanity on a napkin?

    1. Re:You know who else... by MRe_nl · · Score: 1

      Mike Godwin?

      --
      "Kill 'em all and let Root sort 'em out"
  33. marketing by Anonymous Coward · · Score: 1, Funny

    20 years ago we had a shitload of cars that could do better than 40 mpg, now they say they can't do it without studies and mumbling hydrogen and saying maybe in 10 years or something and the price will be triple.

  34. Jupiter plan? by 192939495969798999 · · Score: 0

    I had a Jupiter plan for putting stuff in space on a napkin too, but mine was just throwing a rope out around the planet Jupiter, and using it as a pulley to hoist the stuff into space.

    --
    stuff |
  35. I'm holding out for the first remodel . . . by indytx · · Score: 1

    The Jupiter 2.

    --
    Make love, not reality television.
  36. Alternatives by Kamineko · · Score: 1

    Is this alternative moon rocket going to aimed at an alternative moon?

  37. Not going to happen by Animats · · Score: 3, Insightful

    The US can't afford a manned space program any more. The Iraq war has cost $3 trillion, we're headed into a recession, and it's going to take years to unwind the housing bubble. The next administration is going to have to focus on digging out of the hole left by the Bush administration.

    And, face it, sending a few more people to the Moon on chemical rockets doesn't really get us anywhere. Been there, done that, know what the Lunar surface is like.

    If fusion power ever works, space is worth revisiting, but with chemical rockets, we hit the limits a long time ago.

    1. Re:Not going to happen by K.+S.+Kyosuke · · Score: 1

      The US can't afford a manned space program any more. The Iraq war has cost $3 trillion, we're headed into a recession, and it's going to take years to unwind the housing bubble.

      One has to wonder how many space stations and moon bases could have been built for this money, or how many scientific discoveriess could have been done. There were not enough money for the Jupiter Icy Moon Explorer, but there seems to be always enoug money for killing people across continents. ;/ (I am not talking specifically about US, this seems to be a problem of the mankind as a whole.)

      --
      Ezekiel 23:20
    2. Re:Not going to happen by Anonymous Coward · · Score: 0

      NASA accounts for about 1%-2% of the United States' entire budget. Or about $18 billion dollars.

      You'd save more money getting rid of homeland security. [Which is costing about $34 billion.]

    3. Re:Not going to happen by Graymalkin · · Score: 1

      You have got to be joking. NASA's 2007 budget was $16.7B which was a teensy fraction of the 2007 federal budget. Of that the space operations portion of the budget was only $6.2B. Aeronautics research was $724M. NASA does not have an enormous budget nor do they spend all of that budget on manned space exploration. Canceling manned spaceflight and research would free up a scant $7B which wouldn't put a dent in the federal deficit. So for $7B that will end up getting spent in some other area we would put a bunch of engineers and technicians out of a job, potentially losing all of their domain knowledge similar to what happened with the abandonment of the Saturn/Apollo programs. Planting flags on the moon is of limited utility but it's not the only target in the solar system.

      --
      I'm a loner Dottie, a Rebel.
    4. Re:Not going to happen by evilviper · · Score: 2, Insightful

      The US can't afford a manned space program any more.

      But China can?

      The Iraq war has cost $3 trillion,

      The most recent figures I saw put that at $1 trillion, not 3, but either way, that's a blip on the radar. Hell, the first space race took place DURING the height of the Vietnam war, which was far more expensive and difficult in every sense of the word. The trip was also occurring with brand-new technology, no knowledge of the challenges faced, etc., etc. This time around it's going to be much cheaper, and substantially less difficult (though certainly not easy).

      we're headed into a recession, and it's going to take years to unwind the housing bubble.

      Since WWII, there have been several recessions, but none have lasted longer than 18 months. You're suggesting this is going to be an unprecedented DEPRESSION, the first in 80 years, which seems extremely unlikely...

      The next administration is going to have to focus on digging out of the hole left by the Bush administration.

      This recession should be fading by the time the next president takes office. And besides that, many administrations have had to dig out of the mess caused by their predecessors, but that doesn't stop them, or more specifically, the nation, from accomplishing other goals at the same time.

      --
      Slashdot gets worse every day... Pipedot: News for nerds, without the corporate slant
  38. The REAL problem is: Jupiter is cheaper by sehlat · · Score: 1

    Which means less pork to ladle out in key congressional districts, and a smaller effort required, which means NASA bureaucrats can't hike their status using Parkinson's Law.

  39. The question is... by Thelasko · · Score: 1
    why doesn't the NASA management support this plan?

    All TFA says is:

    "It's not feasible. We said, 'It doesn't work' and moved on,'" Cook said.

    I also want to know if the skid they plan to use to maintain Hubble is reusable, or does it burn up on reentry?

    --
    One of our competitors trademarked the term "hypothesis". From now on, we will call them "boneheaded ideas".
  40. 'simpler, safer, and sooner'? by Anonymous Coward · · Score: 0

    Is that like faster, cheaper, better? Yeah, companies always get all three at the same time...

  41. Spaaaaace meeeeeaaat by Sitnalta · · Score: 1

    The Lunar module was also a "napkin drawing."

    The best science comes from napkins. If we started publishing our scientific papers in napkin-form, then we'd have the cure for cancer, AIDS and the solution to the grand unified field theory inside a week. As well as the complete abolishment of greasy fingers at the Nobel ceremony fried chicken and chili cook-off after party.

  42. Deja Moon by Tablizer · · Score: 4, Interesting

    Wasn't the Apollo system shaped by a similar event? As I remember it, the original plan was to travel and land directly on the moon. However, a handfull of engineers felt that the launching rocket could be simpler and smaller if there was an orbital undock/docking stage. The problem was that orbital rendezvous docking was untried and required technology that didn't exist yet. The docking group eventually won out after heated discussion.

    In the end, everyone was happy except Michael Collins, who had to wait in orbit while his buddies danced on the moon for the first time. (Although perhaps felt safer being that this was all new stuff.)
         

    1. Re:Deja Moon by dukieduke · · Score: 1

      In the end, everyone was happy except Michael Collins, who had to wait in orbit while his buddies danced on the moon for the first time. (Although perhaps felt safer being that this was all new stuff.)

      Relatively speaking, this would be the safety felt by any of us climbing a shakey 100' ladder at the 99' mark. I think safety was a non-issue at that point.

  43. NASA's evaluation of DIRECT vs. Ares I/V by Ellis+D.+Tripp · · Score: 1

    NASA has evaluated the DIRECT proposal, and found it lacking compared to the Ares I/V vehicles:

    http://www.nasa.gov/pdf/256922main_Direct_vs_%20Ares%20_FINAL_62508.pdf

    --
    Remember "News for Nerds, Stuff that Matters"? Help make it a reality again! http://soylentnews.org
    1. Re:NASA's evaluation of DIRECT vs. Ares I/V by Thelasko · · Score: 1
      That was 1.0 this is 2.0. From TFA:

      The DIRECT v2.0 proposal has taken this "rebuttal" document and re-worked the architecture to baseline absolutely zero performance upgrades to the existing RS-68 engines as flown on Delta-IV. No re-optimized nozzle, no regenerative cooling, no fixes to the injector/combustion chamber. We are not even using the higher specification engine which NASA is still planning to use for Ares-V. DIRECT's Jupiter launchers do not require the additional 6% increase to existing RS-68 performance (nor the additional stresses) currently baselined for use on the Ares-V.

      --
      One of our competitors trademarked the term "hypothesis". From now on, we will call them "boneheaded ideas".
    2. Re:NASA's evaluation of DIRECT vs. Ares I/V by Thelasko · · Score: 2, Informative

      Basically what happened was the DIRECT team said their design will work if they re-optimize the RS-68 engine for high altitude.

      The Ares team said their design will work if they re-optimize the RS-68 and the J-2 engines.

      NASA management chose the Ares over the DIRECT.

      The DIRECT team reworked their design to require no engine optimizations. This resulted in DIRECT 2.0

      --
      One of our competitors trademarked the term "hypothesis". From now on, we will call them "boneheaded ideas".
  44. It's all moot anyway, wasted effort by gelfling · · Score: 0

    There will never be manned moon mission sponsored or engineered by the USA through the end of this century. NASA will be converted to a satellite only facility for the weaponization of near earth orbit space. All these big boosters will wind up being used to loft space weapons as a replacement for ICBM build downs per treaties.

    1. Re:It's all moot anyway, wasted effort by MozeeToby · · Score: 2, Insightful

      Why exactly would the powers that be use NASA to launch orbital weapons when the Air Force already has a larger total launch capacity than NASA?

    2. Re:It's all moot anyway, wasted effort by gelfling · · Score: 1

      It's not about throw weight it's about total capacity to loft multiple objects.

  45. Not Napkins... by zamboni1138 · · Score: 1

    Weren't those cigarette packages? I think they were.

    1. Re:Not Napkins... by tgd · · Score: 2, Funny

      I have no idea, and frankly the movie was awful so I am certain I'll never watch it again to find out.

      Really far more interesting at this point is how I got moderated Insightful instead of Funny or maybe a stretch to say Interesting.

      Sometimes I just don't get this place ...

  46. Even a caveman by sconeu · · Score: 1

    How would you feel if I said "So easy, even a slashdotter could do it"?

    --
    General Relativity: Space-time tells matter where to go; Matter tells space-time what shape to be.
  47. Pointless Exercise by SoupIsGood+Food · · Score: 3, Insightful

    The cold reality is that we're probably not going to send a manned mission to the moon. The cost of robotic probes drops by the day, at the same time their capabilities increase. By the time we're ready to send up more astronauts, we'll be able to send up probes that can stay longer and perform more tasks than a human in a rubber suit who has to live in a little tin can. This whole moon-shot thing was basically a PR stunt by the Bush administration - McCaine or Obama will probably kill it, as it's wasteful and frivolous.

    Humans will only return when it's time to construct something permanent there, like a telescope or automated mining equipment. (Even then, it would probably be cheaper to send unmanned probes to small asteroids, directing them to fall in the middle of the desert for harvesting.

    The realities of space exploration have changed - going just to go isn't a useful aim anymore, unless you're paying on your own hyper-rich dime for a vacation to orbit.

    1. Re:Pointless Exercise by Anonymous Coward · · Score: 0

      Bzzzzzt wrong! This is not about science.

      China has announced plans to land a man on the moon which means the Chinese would develop rights to the moon as per international law. America has to go back to it to maintain its claim it.

      If you look at the timing of the announcement by the Bush administration it was announced after China had let it be known that they would land a man on the moon.

      So long as China stays on track to land someone on the moon, America will do so too.

  48. Re:Not going to happen - Check it by Markvs · · Score: 5, Informative

    Proportionally, the Viet Nam War cost more far more: 9.4% of GDP vs. the Iraq War @ 1% of GDP. The entire military budget is 4.4% of GDP, and that's including spending on Corp of Engineer projects and other non-combat related spending. (BTW: The Department of Defense estimates a presence in Iraq through 2017 at $1.7 trillion. $3 trillion is a number came up with by some people with some VERY vested interests.) We WERE in a recession in 1957-1958 (when NASA was founded) and the housing bubble, while bad, is no where NEAR as bad a Black Monday or The Crash or perhaps even the .Com bubble. The only reason why people are bemoaning it (and rightly so!) is because people lost homes. That many of them were homes they never should have bought is another discussion. And we've gone nowhere NEAR the limits. We could easily to manned missions to Mars, set up a real scientific lab on the Moon, even have missions to asteroids all on chemical rockets and boosters. By some logic, it's never a good time to do anything. But human advancement depends on it. And NASA's budget is a mere 0.6% of the US GDP. Call me a kook, but if I wanted to save money, let's ax something really worthless like The Department of Education. It gets [b]3.3 TIMES[/b] NASA's budget, but the kids are dumber today than they were when Carter formed the DoEd thirty odd years ago!

    --
    46. The Hobo smiles, his eyes glaze over, and he burps. "Beware the man who has lived longer than the Wasteland."
  49. I'd intensify that remark by toby · · Score: 0

    It *never* comes from a corporate cog. Cog: Zune. Motivated genius: iPod.

    Ask Jonathan Ives if he considers himself a 'corporate cog', or Richard Stallman, or... any of the garage dwelling innovators.

    Skunkworks always were where it's at. :)

    --
    you had me at #!
  50. see post above by toby · · Score: 1

    With the apparent tone of an insider. Thats one heckuva' job Mikey.

    --
    you had me at #!
  51. Outer Space Fanboy by OS24Ever · · Score: 1

    Hi. I am an outer space fanboy. Since I was a small child I repeatedly copied maps of the solar system, drew them by hand, red the five or six pages about NASA in my World Book encyclopedia until the pages were tattered, manually typed (using a manual typewriter) out those pages out on paper because I was worried I'd lose them.

    In 8th grade, weeks before the challenger exploded we were taught how to write resumes and were supposed to write one 30 years from now. I had references that lived on Mars, all sorts of stupid shit.

    I wanted to be an astronaut as a child, things changed as I got older and I became a computer geek and server admin/solution designer instead.

    But deep down inside that space geek is still alive, still wanting to be out there.

    However the dream keeps dying, all you have to do is watch anything about the manned missions. This last round of stuff from Discovery Channel, you watch Mercury, Gemini, Apollo.

    They certainly glamorize it, at least listening to the interviews of the actual astronauts who are looking back at it compared to the shuttle missions which look like political fighting run amok where instead of someone dying because you were rushing they were dying because no one wanted to look bad (Challenger, Columbia)

    This just seems like another example of NASA going from the thing every little boy and girl dreams of doing to another example of the decay of base education in the states.

    So yeah I'm having a crappy day anyway so I'm pretty pessimistic at the moment, but after reading several different versions of articles on this it seems to me that what you have here is a revolt going on where the smart guys are saying do it this way and look we can build on what we've been doing for decades vs. someone wanting to build a legacy of something all new and shiny.

    To me the 5 years between the shuttle retiring and this new projecting moving forward this is a travesty to me. but that's the 'i want to live in space' fanboy talking, not the pessimistic mid thirties person talking.

    --

    As a rock-in-roll Physicist once said, No matter where you go, there you are.

  52. Wrong by Anonymous Coward · · Score: 2, Informative

    The O-ring failure was IN the srb. The O-ring sealed the gaps between each section of the srb, and when it failed to do so, hot gasses escaped and burned through the external tank and boom. Of course if lobbying and politics hadn't forced the boosters to be made in utah which required them to be made in sections to make the trip to the east coast, we would have never had the o-ring problem in the first place.

    1. Re:Wrong by Twanfox · · Score: 1

      One major reason cited in Discovery's latest synopsis of the space program is that the Challenger's SRB o-ring failure was aggravated/caused by the insistence that Challenger launch despite a sub-zero night preceding launch day.

  53. First Jupiter, then Saturn, after that . . . by Latent+Heat · · Score: 1

    I think there are factions on Congress having issues with the Uranus Rocket.

    1. Re:First Jupiter, then Saturn, after that . . . by Farmer+Tim · · Score: 1

      I think there are factions on Congress having issues with the Uranus Rocket.

      Calling it that, maybe; riding it, apparently not.

      --
      Blank until /. makes another boneheaded UI decision.
  54. You know by bluefoxlucid · · Score: 2, Insightful

    One person with 50 years more experience than all of you still isn't nearly as smart as 57 of you that came to the same conclusion!

  55. Not really by Anonymous Coward · · Score: 0

    A couple of the guys are mormon, so they are use to using to that many at a meal with the little ones.

  56. The rest of the story .... by Anonymous Coward · · Score: 0

    It will be powered by the newly reported "fuel" Vetrolium and be subject to faith-based physical laws.

  57. Re:Not going to happen - Check it by khallow · · Score: 2, Insightful

    Eh, I disagree on the housing bubble. First, your stock market crashes are out of order. The Crash of 1929 was by far the worst US stock market crash ever. Black Monday wasn't significant in the long run aside from increasing regulation on computer trading. And the dotcom bubble was pretty signficant in size, but not that much effect compared to other US recessions after the Second World War. The housing bubble is signficant for two reasons. First, most people have substantial assets tied up in their home and the "wealth effect" from this tends to be larger than for stocks. Second, the housing market is a bit bigger than the public stock market and with long standing expectations of growth going back probably 60 years. If that changes, we'll see a correction that might take many years to settle out. Given that the decline in the housing market and the instability in mortgage companies is still ongoing, I think it's premature to say that the housing bubble will be less significant than a minor recession. We'll just have to see what happens.

  58. And yet by WindBourne · · Score: 1

    this is being driven by those that want to do the SAME thing. They are NOT wanting to do something different. The X-33 was different. The Ares I/IX are somewhat different. The direct is designed to use all of our current guts in a new configuration. The big difference is the list of manufactures change. Lo and behold, the guys who are pushing direct happen to currently work on the space shuttle. The ones pushing constellation are from the winners of the contract.

    --
    I prefer the "u" in honour as it seems to be missing these days.
  59. Re:Outsource it to Burt Rutan, Problem Solved. by deweycheetham · · Score: 1

    Ahhmmm, I seem to be mistaken. I seem to believe Burt Rutan had Designed and built a Publicly Manned Space Vehicle (with his reputation on the line) in the last 20 year. What about Nasa?

    So the score is:

    Rutan 1 (low earth orbit vehicle on a shoe string budget), NASA 0 (with infinite resources upon a serious request).

    Give Rutan $20 billion and see what he can come up with. At least if he screws up, he will probability have change left over. Nasa has NEVER had change left over on a manned mission.

    Brought to you by letter "J" and NASA the "NON AERO SPACE ASSOCIATION".

  60. FWIW by rk · · Score: 0, Offtopic

    You don't get positive karma for Funny mods. I sometimes mod particularly funny things with insightful instead, because good humor is a kind of insight, and I'd like to issue a little extra reward for the joke.

  61. Pogo by ClientNine · · Score: 1

    The problem with Ares is the "pogo problem"-- pretty serious (as in life-threatening) vibrations caused by some interesting harmonics. The SRBs were never meant to fly alone, see.....

    Quite a hell of a lot of ballast as such will need to be flown with Ares to compensate for this. Not much has been said about it, but it's a Very Big Deal within NASA and the principle contractors.

    1. Re:Pogo by MightyYar · · Score: 1

      But they are going to fly it next year to test, right? Using a tuned mass damper and some super-absorbent shocks on the seats, IIRC :)

      Ride sounds like a joy.

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
  62. Re:Outsource it to Burt Rutan, Problem Solved. by Waffle+Iron · · Score: 2, Informative

    Rutan 1 (low earth orbit vehicle on a shoe string budget)

    He has not put a vehicle into orbit. He launched a flimsy rocketplane into a little parabola with only about 1% of the energy required to reach orbit. Nor will his next design achieve orbit.

    Get back to me when you get your basic facts straight.

  63. Challenger crew probably survived initial event by Medievalist · · Score: 4, Informative

    The data recovered after the crash suggest the crew were killed by impact with the water. I don't believe it's known how badly (if at all) the crew were injured by the orbiter's breakup. Several of the suits' emergency air supplies had been activated, however, which tends to support the idea that at least some crew members were still functional after the cabin lost pressure due to hull breach. The guys at NASA who studied the crash didn't think the forces on the cabin would have hurt anyone strapped in, but the altitude was sufficient to knock people out from lack of oxygen.

    This is dredged up from memory, so it may have been superseded by now. I was working for Morton-Thiokol when it happened, and it was not a fun time for myself or my cow-orkers.

    1. Re:Challenger crew probably survived initial event by Muad'Dave · · Score: 1

      ...myself or my cow-orkers.

      Dude, you shouldn't admit to "cow-orking" in a public forum. Post anonymously next time!

      --
      Tiller's Rule: Never use a word in written form that you've only heard and never read. You will end up looking foolish.
    2. Re:Challenger crew probably survived initial event by MightyYar · · Score: 1

      I phrased my original question poorly. I meant, would the booster have catastrophically failed or just leaked fire from it's side until it burnt out? In other words, could a bum o-ring doom Ares I? Obviously it would doom Jupiter or Ares IV and V.

      --
      W..w..W - Willy Waterloo washes Warren Wiggins who is washing Waldo Woo.
    3. Re:Challenger crew probably survived initial event by camperdave · · Score: 3, Informative
      Just off the top of my head...
      • The fire leaking from the side would cause a sideways thrust vector which could push the rocket into a corkscrew trajectory (or worse).
      • The loss of thrust out the side would mean that there isn't as much thrust out the bottom, meaning the craft probably would not attain orbit.
      • The fire leaking from the side would melt/burn a hole in the side of the booster. The aerodynamic forces acting on the compromised panel could rip it away from the booster, further damaging it.

      So, while the Ares I may not turn into a giant fireball, A side leak would likely still mean a loss of the rocket. The crew module would have a much higher chance of survival, though.

      --
      When our name is on the back of your car, we're behind you all the way!
    4. Re:Challenger crew probably survived initial event by Raenex · · Score: 1

      I was working for Morton-Thiokol when it happened, and it was not a fun time for myself or my cow-orkers.

      Were you in the conference call the night before that attempted to get NASA to scrub the launch? I saw a special on that, and the interview with the Boisjoly was chilling. Too bad, though, that despite all his heroic efforts, he fell short at the crucial moment and didn't object when the mic was open.

    5. Re:Challenger crew probably survived initial event by Medievalist · · Score: 1

      I was working for Morton-Thiokol when it happened, and it was not a fun time for myself or my cow-orkers.

      Were you in the conference call the night before that attempted to get NASA to scrub the launch? I saw a special on that, and the interview with the Boisjoly was chilling. Too bad, though, that despite all his heroic efforts, he fell short at the crucial moment and didn't object when the mic was open.

      Hell no, I wasn't involved with the shuttle SRMs at all (though I lost my job in the layoffs that resulted from the Challenger accident). I was busy helping Ronald Reagan give the Saudis nuclear weapons technology. Oh, excuse me, that didn't happen, we were developing totally peaceful "booster rockets" that were to be used in the totally peaceful "Saudi communications satellite launch program" and those missiles, er, I mean totally peaceful rocket motors, just happen to be functionally identical to state-of-the-art cruise missiles. Just a coincidence I am sure; there's no reason you wouldn't want satellite launchers to fly ten feet off the ground with a 500 lb payload.

  64. the debate was already over by heroine · · Score: 1

    This is like a dead candle which keeps getting gas thrown over it. It'll fizzle out again & next month the same thing will be on all the headlines. The debate has already been had. Lots of people build robots in their spare time. Does it mean Google & Silicon Valley are all wrong & venture capitalists should all invest in robots instead of web 2.0?

  65. Re:Outsource it to Burt Rutan, Problem Solved. by deweycheetham · · Score: 1

    Ok! If you can only think in terms of negativity. Rutan has lost 0 space vehicles in which people died, Nasa has lost 2 that we know of. How many School Teachers, Pilots, and Scientists has NASA lost in the last 20 years again? How many has Rutan lost?

    The sad part about it is that Nasa has not developed any New Manned Kind of Vehicle in the last 20 plus years. That's not Rutan's fault so don't blame him, but it is one reason he has decided to go it alone. And in doing so has proved that National Aero Space Programs from the US, Russia, China, and the EU are not the only way to go and may not be the best. In turn, That mean their budges can go too. Lets cut there(NASA) first and save the tax payers a fortune. Only someone on the payroll of the Nasa and/or its croon knee subcontractors can't see this.

    By the way how long do we have ignore private sector, private inventors, and projects like "The X Prize's" so solve the major issues of the day, because the Politicians and the Bureaucrats are beholding to the special interests that feed the originations? (Who can compete with the government(s) and unlimited monies?)

    One more thing, do you remember name of the "Candy" the that was free floating in space on the "X Prize" Winning mission that you would like to ignore, that didn't make low earth obit? Hmmm, I suddenly have a sweat tooth...

    Brought to you by letter "J" and NASA the "NON AERO SPACE ASSOCIATION".

  66. Re:Not going to happen - Check it by Markvs · · Score: 1

    That's your right of course, but *most* of the folks that lost houses didn't put in much equity to begin with, nor make many payments. So while it's bad, it's not *that* bad. I didn't say they were in any particular order, but yeah, otherwise I agree with you. I'm certainly not saying that the bubble won't be hurtful, but it's more of the secondary in the 1-2 punch with high/rising energy prices and non-core inflation for the first time in decades.

    --
    46. The Hobo smiles, his eyes glaze over, and he burps. "Beware the man who has lived longer than the Wasteland."
  67. whaaat... by toby · · Score: 1

    You haven't upgraded to VISTA yet??

    --
    you had me at #!
  68. if it's the TRUTH... by toby · · Score: 1

    Then I say, No Penalty!

    --
    you had me at #!
  69. I'd mod you.. by toby · · Score: 1

    -1, I'm Very Upset

    --
    you had me at #!
  70. Re:Outsource it to Burt Rutan, Problem Solved. by Waffle+Iron · · Score: 2, Informative

    How many School Teachers, Pilots, and Scientists has NASA lost in the last 20 years again?

    Fourteen, after having achieved several man-years in orbit

    How many has Rutan lost?

    Three, after having achieved about 5 man-minutes in a parabola

    Look, NASA has been stupid, bloated and has wasted hundreds of $billions of our money on the ISS and shuttle, which both should have been scrapped a decade ago. However, that doesn't mean that Rutan has done anything useful either. Compared to *real* space activities, he is just puttering around. By the time he builds anything that could safely get humans in and out of orbit (which would require 100X his current fuel capacity, heat shields, life support systems, etc.), his "shoestring budgets" would be totally busted.

  71. obsolete tools and "once standard" parts... by toby · · Score: 1

    I hope everyone's looking forward to digital obsolescence as it really starts to bite. Let me guess at how much data is locked behind Microsoft or other proprietary formats at NASA... Mathematica, anyone?*

    You think those "license servers" are going to stay up for the next 50 years? (Let alone the next 500.)

    (*Yes I know the notebooks were traditionally text. But the calculations themselves are behind a proprietary gatekeeper.)

    --
    you had me at #!
  72. oh, silly me by toby · · Score: 1

    the Viet Nam War cost more far more: 9.4% of GDP vs. the Iraq War @ 1% of GDP.

    Here I was thinking "that there's never a good time to start an unnecessary war of aggression on false premises costing $3-6 trillion..." How silly of me. Say, maybe the Vietnam war was bad for the US as well? Read Hersh's The Price of Power: Kissinger in the Nixon White House sometime.

    --
    you had me at #!
    1. Re:oh, silly me by Markvs · · Score: 2, Insightful

      My point was that the US could fight a war in Viet Nam that proportionally cost 9x what the Iraq wars costs *and* go to the moon *and* fund "The Great Society". The original poster saying we need to ax manned spaceflight until fusion due to cost/benefit was what I was railing against, not saying that wars are good. Sheesh!

      --
      46. The Hobo smiles, his eyes glaze over, and he burps. "Beware the man who has lived longer than the Wasteland."
  73. Re:Outsource it to Burt Rutan, Problem Solved. by deweycheetham · · Score: 1

    Why don't you give him (Rutan) the $20 billion (There by saving $15 billion) as I suggested earlier and see what he and his engineers can come up with. He doesn't seem to operate on the principle that "The jobs not done till the monies all gone". Maybe a little clear vision (instead of the Clearlake view of the world) can make a difference.

    After having personally worked for Nasa (sub contracted) and watched one of it birds drop out of the sky so hard only the worms survived(because of some 35 plus year old design flaw). I have very little faith in the organization. My guess is that too much of their work is/was directed at the "Black Programs"/money sink, and the lack of success in the "Manned Missions" for last 20 years proof enough for me.

    Brought to you by letter "J" and NASA the "NON AERO SPACE ASSOCIATION".

  74. we are being ripped off by civilian space efforts by Anonymous Coward · · Score: 0

    Nasa=freekin old tech, not needed any more. TR3 and B. google it

    they need to end the tech embargo

  75. Jupiter? by Anonymous Coward · · Score: 0

    I would be inclined to name a rocket for moon missions "Moon" instead of "Jupiter."

  76. Re:Not going to happen - Check it by evilviper · · Score: 1

    Call me a kook, but if I wanted to save money, let's ax something really worthless like The Department of Education. It gets [b]3.3 TIMES[/b] NASA's budget, but the kids are dumber today than they were when Carter formed the DoEd thirty odd years ago!

    I agreed with up until you latched onto this right-wing propaganda point...

    Adjusted for inflation, public school districts are getting slightly less money than they did 30 years ago, while at the same time, the population of school-children has increased by something like 30% (varies depending on area). K-12 Public education is in a terrible state, but it very likely has a lot to do with the fact that politicians are only too happy to squeeze money from school budgets, rather than raise taxes, or cut from anywhere else that it would be more immediately noticed (rather than 20 years later).

    --
    Slashdot gets worse every day... Pipedot: News for nerds, without the corporate slant
  77. Re:Not going to happen - Check it by khallow · · Score: 1

    That's your right of course, but *most* of the folks that lost houses didn't put in much equity to begin with, nor make many payments.

    There are two other effects. First, this is a big hit for lenders and anyone who invested in mortgage securities since there were a lot of people who had recent mortgages. Second, it depresses house prices, a combination of increasing supply and reducing demand.

  78. On Funny v. Insightful by Etherwalk · · Score: 1

    (1) Occasionally someone will see a funny post but want to give props to the author instead of just the comment. IIRC, Funny mod points increase the score of the comment, but Insightful mod points increase both the score of the comment and the user's Karma.

    (2) On rare occasions, moderating a ridiculous, comical, sarcastic, or satirical comment as informative is in itself a funny thing.

    (3) Maybe the mod in question just really needs to kill superman.

  79. I disagree with your dismissal of the housing by Anonymous Coward · · Score: 0

    crunch. I believe it is a HUGE problem because housing was our last hope (in the USA.) So much of our mfg and tech job base has gone overseas that the last thing keeping our economy going was people borrowing against the rising value of their homes. Now that that's gone, what is going to bail us out/start a recovery?
    The really cynical side of me says we can start another war or there is a conspiracy to try to sell CO2/alternative energy tech, but I doubt that our leaders are really that evil.

  80. Re:Not going to happen - Check it by Anonymous Coward · · Score: 0

    ...Viet Nam War cost more far more: 9.4% of GDP vs. the Iraq War @ 1% of GDP

    Where DID you get that 9.4% of GDP. You ARE the people with some VERY vested interests.
    http://news.bbc.co.uk/2/hi/americas/4201812.stm

  81. GP uninformative, mod parent up by aepervius · · Score: 1

    GP don't cite reference for his numbers where as at least one can argue with the numbers in the BBC article. Vietname war cost 111 billions the GDP of the US was roughly 3500+ over the years of the war so 111 billion total cost is NOWHERE near 9.4% it is at most 3% of any given year. Furthermore inflation adjusted dollar this is roughly 450 billion of today (see same GDP page as before). today gdp is 11000 billion so an estimated Irak total war cost of 500 billion is higher in percent of GDP (5% today compared to aforementionned 3%) and higher inflation adjusted.

    Anyway there is a cost which is not really counted or accountable in vietnam war : the cost of the dead and veteran (human cost) the same for the Irak war. Ples the resulting international terrorism for vietnam war was zero (or at least I am not aware of it) whereas one can certainly argue this is relatively open for Irak war and could certainly rise. Finally I am not certain comparing TOTAL cost over many years to GDP is really that useful a comparison anyway. It should be comapred to say, day to day cost of education to day to day cost of the war in both case and see what comes out. I am too lazy to do it ;).

    --
    C. Sagan : A demon haunted world:
    http://www.amazon.com/gp/product/0345409469/
    visit randi.org
  82. Re:Not going to happen - Check it by Markvs · · Score: 1

    That's total dollar amount, not % GDP, you anonymous genius you!! Or is the 2008 American economy the same size as the 1968 American economy? :-p

    --
    46. The Hobo smiles, his eyes glaze over, and he burps. "Beware the man who has lived longer than the Wasteland."
  83. Re:Not going to happen - Check it by Markvs · · Score: 1

    Um... that was sarcasm. I apologize for not putting in a [/sarcasm] at the end.

    --
    46. The Hobo smiles, his eyes glaze over, and he burps. "Beware the man who has lived longer than the Wasteland."
  84. Explosion theoretically impossible by GPS+Pilot · · Score: 1

    I have wondered about this. The H2 and O2 are stored in seperate tanks. Wouldn't they have to be well-mixed before an explosion could take place?

    --
    That that is is that that that that is not is not.
  85. O-rings are not necessary. by Medievalist · · Score: 1

    I don't know if there are any O-rings in the design, but if so they'd be made of materials that do not exhibit the well-known shortcomings of the ones used on Challenger. There haven't been any other O-ring related failures in space vehicles AFAIK. There's no need for them in a non-segmented design, of course.

    Without knowing the composition of the case, the propellant, and the O-rings in question, you can't really say. For example, some solid propellants operate within a fairly narrow pressure range, and having a hole open up in the case could drop the internal pressure enough to stop the burn. The effect on navigation is also impossible to predict without getting into ridiculous detail - is it a 3 mm hole on the port side six inches from bolt, or a 5 mm hole facing in towards the vehicle? Either way your combustion chamber will deform and the effect on surface area of the burn will cause a variation in impulse from that rocket which will mess you up, but you also might get some spin or side thrust. There are just too many variables to make a prediction... consider this analogy - what will happen to your car if a capacitor fails? Maybe you'll die, maybe you will just have to pull off the road.

    In the cause of Challenger, I'll WAG that the leak wouldn't have caused any unresolveable problems if the whole vehicle hadn't been designed like two bottle rockets strapped to a zip-lock bag of gasoline.