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Boeing Successfully Launches Mammoth Delta-4 Heavy

Posted by timothy on Wed Dec 22, 2004 11:02 AM
from the yeah-it's-got-a-hemi dept.
nick-bts writes "CNN, the BBC and Space.com are reporting the first successful launch of the new Boeing Delta-4 Heavy, capable of lifting 23 tonnes into a low-Earth orbit (similar to the space shuttle). Personally I think the Ariane 5 and 'Satan' are way sexier..."
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  • Hungry crew (Score:5, Interesting)

    by SIGALRM (784769) * on Wednesday December 22 2004, @11:03AM (#11159039) Journal
    The Delta IV family blends new and mature technology to launch virtually any size medium or heavy payload into space
    Probably wouldn't be a bad idea to send one of these bad boys up to the ISS [boeing.com] loaded with some serious good eats [space.com] :)

    Seriously though, it appears the Delta 4 Heavy will primarily service military--rather than commercial or scientific--interests.
      • by BJZQ8 (644168) on Wednesday December 22 2004, @11:54AM (#11159655) Homepage Journal
        Boeing, though, and the development of the D-IVH, is heavily subsidized by the military. Boeing is rapidly becoming "the" defense contractor, having swallowed up McDD. Throw in some sweetheart 767 tanker leasing deals...and you can't hardly say that Boeing is anything but a large piece of the military-industrial complex. I will definately agree that it does represent a leap in technology for the USA, but is still short of the mid-80's Soviet Energia. The D-IVH can carry 28,000 [technovelgy.com] pounds to geosynchronous orbit...the Energia could lift 36,000 pounds to the same path. The D-IVH can lift 48,000 pounds to LEO, the Energia could lift 200,000. [russianspaceweb.com] So while the D-IVH is quite an accomplishment, it's not a Saturn V.
  • Delta-9 (Score:4, Funny)

    by thmclean (590355) on Wednesday December 22 2004, @11:05AM (#11159056)
    I'm waiting for the Delta-9. That would be waaay more heavy, dude.
  • NOT successful (Score:5, Informative)

    by mOoZik (698544) on Wednesday December 22 2004, @11:05AM (#11159058) Homepage
    It was not completely successful. The two dummy satellites did not make it to orbit due to a problem with the first stage. You can read about it here: Boeing Rocket Launch [newscientist.com]

    • Re:NOT successful (Score:5, Interesting)

      by Squareball (523165) on Wednesday December 22 2004, @11:12AM (#11159145)
      You beat me to it. Funny thing though, even though it wasn't a success, Boeing was on the radio saying that they consider it a success. WTF? Failure is a success now days? Sure it wasn't complete failure but had there been a real satellite on board it would be pretty much a loss now. "F = Fantastic" oh brother.
      • Yeah, another example of the government spinning an almost failure into a success. Had it exploded on the pad, they would have said, "Despite the absense of take-off, we believe the launch was a success. We are ready to commit billions of tax dollars on this rocket. I think they are so optimistic because Boeing had trouble finding commercial customers for the maiden flight, so the govt. had to finance almost the whole thing. As a result, they don't want to admit that it was a partial failure.

        • It was more successful then the first launch of arianne 5 which blew up. It got off the ground and it delivered its payload. Pretty successful to me.

          Btw, Boeing is not part of the Government. How can you call boeing's spin another example of government spinning?
      • I'd say a test launch of a rocket this size that actually made it off the launch pad for the first time ever qualifies as a success.

        If you read the back story of the project, Boeing built the first new launch facilities in the last 35 years in order to launch this series of rockets. Getting off the pad on the first try with this configuration seems like a success to me.
      • Re:NOT successful (Score:4, Insightful)

        by Zerbey (15536) * on Wednesday December 22 2004, @11:42AM (#11159513) Homepage Journal
        It didn't explode on the launch pad, and it did make it into orbit. That's a remarkable achievment in itself. This is new hardware and there's bound to be teething problems.

        The term you're looking for is "successful failure" :)
      • Failure is a success now days?

        How about the Alamo? Texans cite and use it as a rallying point so often that it's easy to forget that it was a huge military disaster.

        In that light the "Don't mess with Texas" always made me chuckle a bit.

        (I incidentally proposed that Ohio coopt the line and make it "Don't mess with Ohio or we'll burn Atlanta down again" because while Texas lost the Alamo, we burned the south.)

      • had there been a real satellite on board it would be pretty much a loss now

        Well, doesn't that make it a success? They have an opportunity to fix a problem now, and it didn't cost them as much as it could have to expose that problem.

        I don't understand why people still insist on everything working 100% the first time, even though it has never ever worked that way. How did we somehow start expecting it?
      • > "Air Force instead paid to launch a dummy payload and a pair of small research satellites."

        Our tax dollars at work.

        Would you rather that they had put another $Billion of our tax dollars into a spy satellite that would be uselessly drifting in space right now because of the partial failure of this untested rocket?

      • by Rei (128717) on Wednesday December 22 2004, @12:27PM (#11160075) Homepage
        You post this almost every time, in almost the exact same words, on articles unrelated to China. Please stop it. It wasn't true then, and it isn't true now. China's military budget per dollar of GDP is a tiny fraction of what nations like the US spend, their military expenditures on space have been rather minimal (they have only about a dozen DF-5s, and at most two dozen - their ICBM with worldwide range); the US has 7200. Don't believe me? From the Federation of American Scientists:

        "For many years almost all sources credited China as having only four DF-5s deployed in silos, including the authoritative 1992 treatement by John Wilson Lewis and Hua Di, which asserted that as of 1992 only four DF-5 missiles on alert. However, more recent estimates suggest that some 8-11 were deployed as of 1995, and that at least 13 missiles were deployed at the end of 1997. According to the National Air Intelligence Center, as of 1998 the deployed DF-5 force consisted of "fewer than 25" missiles. As of early 1999 the total deployed DF-5 force was generally estimated at about 20 missiles. By mid-2000 some sources suggested that the total force was as many as 24 deployed missiles ["Inside The Ring" By Bill Gertz and Rowan Scarborough Washington Times July 28, 2000]."

        They're progressing on their astronaut program at about twice the rate that the US and Russians did (albeit by standing on the shoulders of giants). They've been working on space station and lunar programs. Their rockets that are being developed are liquid fuelled, making them ill suited for adaptation to missiles. I could keep going for hours. Like China or not, it's a textbook example of a space program focused on civilian efforts.

        If you want to make these claims again, don't post links to pages about Tibet, which is utterly unrelated to the topic at hand - post links to articles about China's space program.
  • by kippy (416183) on Wednesday December 22 2004, @11:05AM (#11159069)
    So what reason is there for the space shuttle now? all the heavy lifting can be done by these things and the personnel can get up in a Soyuz. These things seem "cheap" and from what I've read, this paradigm can be used to just strap on a few more rockets to get to the Moon or Mars.

    Can anyone cite a reason for continued shuttle lifetime that isn't political?
    • For one thing, the Space Shuttle is the only American man-rated launch system in service (well, nearly in service) today. The last one has not been used since the Apollo-Soyuz joint mission, and there is no tooling or production facilities to build an Apollo-style capsule or launch vehicle to carry it aloft.

      Secondly, there are still missions that require both heavy lifting and human beings. For example, if NASA were to choose to repair the HST using a non-robotic mission, it would be the Shuttle that car

    • There has never been any reason for the space shuttle, at least not as it was ultimately realized. The requirements for crewed flight and cargo are so radically different that there has never been much engineering justification for combining the two.

      A sensible launch system would have at least two components: a small, crewed vehicle type with six nines reliability, and one or more larger vehicle types for lifting cargo and blowing up.

      There are some economic factors that mitigate against this mix a bit,
      • by fname (199759) on Wednesday December 22 2004, @11:47AM (#11159570) Journal
        Six nines reliability sounds nice, but that works out to one failure in a million attempts. Realistically, until you've had 1 million succesful launched with only 1 failure, you could not claim six 9s reliability. That may be a good goal for an operational vehicle, but it's unrealistic for a development vehicle. We just don't know enough about what could go wrong to assign probabilities with that degree of certitude.
    • It's needed to build the ISS. A number of the pieces of the ISS are designed to fit into the shuttle's cargo bay and to be supported by brackets within the bay during lanuch. No current expendable rocket has the same configuration. Plus the spacearm is needed for some assembly tasks.
      • so put them in the space station with Soyuz.

        plus, how much data do we need on this? We've been gathering it for decades now. The result: eat right, excersize, take it easy for a few days when you re-enter a gravity well.
      • And sometimes your satellite will need repair, so you gotta get it down somehow.

        NASA says [reston.com] the shuttle costs $2.2 billion/year to have around and $85 million per flight. Since NASA had only been making half a dozen flights a year, this equates to $500 million per flight average mission costs.

        That'd better be one important satellite you're trying to repair. We could have replaced even the Hubble Space Telescope for the price of the shuttle missions we've done to service it.

        • by DoctorPepper (92269) on Wednesday December 22 2004, @11:44AM (#11159537)
          Actually he isn't. STS-87:

          "Early in the mission, the crew deployed Spartan, a freeflying solar instrument package that was supposed to make independent observations of the sun's outer atmosphere and the solar wind. However, the equipment failed upon deployment and was unable to complete its mission. During their first spacewalk Winston Scott and Takao Doi grabbed the spacecraft by hand and berthed it in the payload bay for its return to Earth. Since landing, the Spartan satellite has been impounded for study to determine the cause of the failure."

          Granted, the mission wasn't to go up and retrieve a broken satellite, but they did, in fact, retrieve the satellite and bring it back to Earth.
        • by DoraLives (622001) on Wednesday December 22 2004, @11:57AM (#11159694)
          You're talking out of your ass.

          Concur.

          There hasn't ever been a shuttle mission which required taking a satellite out of orbit and landing it on earth.

          Incorrect. Mission 51-A [nasa.gov] and mission STS-32 [nasa.gov] both did exactly that.

          There isn't any utility in doing so either.

          While I have to wonder about the cost effectivness of bringing a pair of comsats back down for refurbishment and relaunch, the LDEF experiment absolutely REQUIRED that it be brought back down.

          Next time, check your facts a little closer, eh?

  • Sexier??? (Score:5, Funny)

    by Anonymous Coward on Wednesday December 22 2004, @11:07AM (#11159086)
    Personally I think the Ariane 5 and 'Satan' are way sexier...

    Man, you have a wierd phallic fetish going on there.
  • by 10sball (80009) on Wednesday December 22 2004, @11:07AM (#11159093) Homepage
    The bit I read this morning wasn't as positive as the story posted above...

    http://www.spacetoday.net/Summary/2713 [spacetoday.net]

    Delta 4 Heavy launch comes up short
    Posted: Wed, Dec 22, 2004, 9:30 AM ET (1430 GMT)
    The first Delta 4 Heavy launch vehicle lifted off Tuesday afternoon but a problem with the vehicle's first stage has apparently kept the vehicle from deploying its payload in the proper orbit. The vehicle lifted off from pad 37B at Cape Canaveral at 4:50 pm EST (2150 GMT), more than two hours into a three-hour launch window because of minor problems during pre-launch preparations, and initially the launch appeared to be normal. However, the Delta 4's first stage -- three identical core boosters -- shut down eight seconds earlier than expected. To compensate, the upper stage fired longer than planned during the second of three burns needed to place the primary payload, a demonstration satellite, into geosynchronous orbit, and as a result ran out of propellant during the final burn. Contact has also not been established with two nanosatellites that were deployed from the booster 16 minutes after launch. Despite the underperformance of the first stage, Boeing officials said they, as well as the Air Force, who paid for the flight, were pleased with the launch.

  • by stubear (130454) on Wednesday December 22 2004, @11:08AM (#11159095)
    "Personally I think the Ariane 5 and 'Satan' are way sexier..."

    I think the nick-bts needs to get out more.
  • by StateOfTheUnion (762194) on Wednesday December 22 2004, @11:10AM (#11159127) Homepage
    After 25 years of sleeping at the wheel as the Russians built new rocket motors, the US finally comes out with a new one . . .

    The RS-68's [boeing.com]on the Delta IV Heavy are the first new big rocket motor to be designed and built in the US in a long time (The space shuttle uses motors designed in the late sixties or very early seventies).

    And for the record, I think a new rocket motor qualifies as sexy . . .

  • by MufasaZX (790614) on Wednesday December 22 2004, @11:13AM (#11159152) Homepage
    To answer the obvious predictable question, no, the Delta IV Heavy doesn't even come close to the Saturn V. The Sat5 could heave 118,000kg into LEO, while the 3 booster D4H can only lift 22,000kg. There is talk of strapping on even more big candles to the D4, going up to as many as 7 main engines (the core and then 6 around it), but rough extrapolation would take that only to 51,333kg, far better than the shuttle but still a far cry from the awesome power of the Saturn V [wikipedia.org].
    • by ausoleil (322752) on Wednesday December 22 2004, @11:23AM (#11159304) Homepage
      Good points. Unfortuntely, there are no launchable S-Vs, no infrastructure, and not even many engineers familiar with the system left to build or launch one. In short, Nixon, Ford and Carter were fools for throwing away the best launch system the world has ever seen.

      Think of what may have been if Von Braun had been allowed to proceed with Nova. It made the Saturn V look like a bottle rocket.

        • by ausoleil (322752) on Wednesday December 22 2004, @02:30PM (#11161424) Homepage
          Your grasp of the history is 100% correct.

          I feel lucky that I was able to see every Saturn launch in person, the I's the V's even the Skylab and SATP. They were maginificent birds, powerful and mighty. To see one in person was to know the most awesome machine ever built in the history of humanity.

          I cite Ford and Carter because even then we had *some* of the momentum from the Apollo days, and with a little push, the engineers and technicians would have come back and had us on Mars by 1990, or 2000 at the latest. Some may scoff at that now, but simple fact is that they would have scoffed at Kennedy in 1961 on the onset of the moon effort. With Nova in service, Mars could have been had. As it is now, we cannot even launch a single astronaut into LEO with American hardware. That's something Mercury could do, but not us in 2004.

          Pitiful.
    • by NardofDoom (821951) on Wednesday December 22 2004, @11:25AM (#11159328)
      The shuttle orbiter weighs in at 99,318 kg fully loaded. [astronautix.com] I'm not sure how much of that is the engines, but if we weren't busy launching bricks-and-wings into space we'd be able to lift more than 50 metric tons to LEO. For crew return we can use a capsule with an ablative heat shield, and the crew wouldn't have to worry about finding their way out of an exploding craft moving supersonically to eject, just put an escape rocket on the capsule like with early spacecraft.

      Something tells me that would be cheaper than the shuttle, and get more done, and be more adaptable.

  • by KE1LR (206175) <ken.hoover@gmail.cDEGASom minus painter> on Wednesday December 22 2004, @11:14AM (#11159179) Homepage
    Anyone who's spent time listening to air traffic control radio near a major airport has certainly heard large aircraft identify themselves as " heavy" so my first thought was that "Delta 4 Heavy" sounded like a 747 instead of a rocket.
  • by Tackhead (54550) on Wednesday December 22 2004, @11:16AM (#11159199)
    So I read the headline:

    "Boeing Successfully Launches Mammoth Delta-4 Heavy"

    Of course, for every stupid, bizarre, or just plain wonky idea, there already exists at least a semi-serious proponent. Proof is left as an exercise for Google [google.com]

    From the second Google hit on "mammoth wooly rocket", I quote:

    Flight at mach 3.0 from rocket booster in the rump, electric beams from tusks, missiles come from the two nostrils of the trunk

    It gets weird after that.

  • by _PimpDaddy7_ (415866) on Wednesday December 22 2004, @11:17AM (#11159215)
    who'd love these rockets [boeing.com] :)
  • by xxxJonBoyxxx (565205) on Wednesday December 22 2004, @11:21AM (#11159284)
    "Satan is sexier..."

    Yeah...good luck getting funding for your "Satan" rocket from the current crop of "values" politicians in Congress.

    Tell the marketing guys to try "Sword of Jesus" instead; you'll be in like Ron Jeremy.

  • Which units? (Score:4, Interesting)

    by Rich Klein (699591) on Wednesday December 22 2004, @11:23AM (#11159296) Homepage Journal
    ...capable of lifting 23 tonnes...

    Boeing [boeing.com] is a US company, but Nick [mailto] (and the BBC [bbc.co.uk]) used the British spelling of tonnes. What kind of tonnes are we talking about?

    The space.com story [space.com] provides some more useful numbers:
    The added engines allow the rocket to launch 50,800 pounds (23.040 kilograms) of payload into low Earth orbit and 28,950 pounds (13,130 kilograms) to geosynchronous orbits...

    That would seem to be (roughly) metric ton(ne)s; there are 2,204.623 pounds per metric ton.

    For comparison:
    1 ton, gross or long (same as a British ton) = 2,240 pounds
    1 ton, metric = 2,204.623 pounds
    1 ton, net or short = 2,000 pounds
  • Still a few problems (Score:4, Informative)

    by Fiz Ocelot (642698) <baelzharon@g[ ]l.com ['mai' in gap]> on Wednesday December 22 2004, @11:31AM (#11159389)
    There were a few glitches:

    "We had a shorter than expected first stage burn. That was compensated for by longer first and second burns in the second stage," said Dan Collins, Boeing vice president for Expendable Launch Systems,

    And: [decaturdaily.com] "The delay at five minutes was due to a loss of communication between launch control and the vehicle destruct system. Boeing spokeswoman Monty Vest described this."

  • by n9mdh (800649) on Wednesday December 22 2004, @12:18PM (#11159962)
    Calling an RS-18 missile "Satan" was a (basically US) military thing-- sorry to burst the "cool name" bubble. They (then Soviets) referred to the RS-18 as the "Voyevoda," a noun that refers to a leader-- a leader whose power is achieved by being the toughest kid on the block. It's like the west calling a tank "Patton," etc. The US/NATO used "SS" instead of "RS" to refer to Soviet missiles, so the RS-18 becomes the SS-18 in NATOspeak. Here's where the fun starts.

    OK, say it with me: s-s-eighteen... ss-eighteen... s-eighteen... s-eight-en... satan. In an era when you refer to the other side as the evil empire, cool names that emphasize the whole evil thing tend to stick.

    Just thought you might want to know...
  • First Time Gitters (Score:3, Informative)

    by gcpeart (788373) on Wednesday December 22 2004, @12:34PM (#11160149) Homepage
    Hey Boeing isn't the only one who can screw up a first launch, the 'sexier' Ariane 5 self destructed on its first launch do to a software glitch in the primary and redundent guidance systems. Of course on their site the launch log only marks the occasion with a * with no corrosponding note(see flight 88) [arianespace.com], and the milestones for the Ariane 5 [arianespace.com] makes the brief a very brief note, "The Ariane 5 501 test flight fails."
  • by Baldrson (78598) on Wednesday December 22 2004, @01:46PM (#11160969) Homepage Journal
    Figures from space.com [space.com], $140 million and 50,000 lbs, allow one to estimate the cost/lb to LEO of the Delta IV at $2800/lb when the payload bay is packed to the gills.
    • by kippy (416183) on Wednesday December 22 2004, @11:09AM (#11159115)
      if your goal is lifting a manned habitat to a Mars intersecting trajectory it's pretty damn sexy.

      Or if you want to put up some crazy, ineffective missile shield, it looks pretty good too.

      I don't think that people in the market for rockets of this scale are swayed by a name.

      Yeah, I know. I should get a sense of humor.
      • Not true, one of the main conditions on most planes built is that they have to look cool. If a design will you give you X amounts more lift, but makes the plane look terrible, the "sexy" looking design will win out. The stealth fighter had to be black, even though that is not the most condusive colour for stealth activities. Also, Boeings design for the Joint Strike Fighter (JSF) was ripped on because it wasn't as sexy as Lockheed's. This isn't the only reason Lockheed won out, but it was a contributing
    • by DoraLives (622001) on Wednesday December 22 2004, @12:21PM (#11159996)
      If it isn't sexy, it ain't getting my business.

      Well then, it must all be related to your point of view. From here on the beach this one was extremely sexy.

      Absolutely gorgeous day with crystal clear weather and a light breeze coming in off the Atlantic.

      Pad 37 is way back up north past the end of ICBM Row and the tip of the cape, so the bottom half of the vehicle was obscured by intervening vegatation as it sat on the pad, but as soon as they ignited the engines, the flash of orange light and the discharge of smoke from the flame deflector made things abundantly obvious as to what was going on.

      This particular bird rose at an excruciatingly lethargic pace, and even well after it had cleared the tower, it was still taking its sweet old time. Probably the slowest liftoff I've ever watched, and I've watched a bunch going all the way back to the 50's.

      The alignment of the CBC's placed them 'face on' from my point of view, and all three of them looked quite spectacular, front lit by a late afternoon sun, each core producing a beautiful orange pillar of flame.

      Finally, it really got going and started to move out like you would expect. As it did so, it reached an altitude where the LH2/Lox exhaust produced a pure white contrail that stood out in stark relief against the deep blue sky. At about the same time, the rumble arrived and it was a fine, deep-throated one that bespoke of the power being released quite well.

      For those of us used to things like The Shuttle or any of the large Titan's, outboard CBC separation seemed to take forever to finally occur. The vehicle was well downrange when this happened, but with optical aid the sudden plume as they separated was easily visible, as well as the CBC's themselves, slowly tumbling end over end as the core continued to accelerate on away from them.

      All in all, quite the sexy launch, if you ask me.

    • by kippy (416183) on Wednesday December 22 2004, @11:13AM (#11159163)
      This is a new approach.

      while it's not using antimatter or fusion or something, it makes use of "off the shelf" components to strap together a powerful rocket.

      If you want more power, just bundle another couple on. You couldn't really do this with the shuttle or the Saturn. Plus, if you have different mission parameters, you can use basically the same hardware without the need to do R&D for years for a new rocket.

      Yeah, it's still chemical propulsion but it seems like a better way of thinking to me. This is something that can actually get some economy of scale.
    • It's common to liquid rockets, particularly when you want to throttle up after achieving maximum dynamic pressure so you don't destroy your rocket against a ceiling of high-speed high-pressure atmosphere.

    • Re:Throttles (Score:4, Informative)

      by Teancum (67324) <robert_horning@n ... ER.net minus cat> on Wednesday December 22 2004, @01:34PM (#11160850) Homepage Journal
      The purpose of a throttle is to control the amount of thrust that is expended during the flight. Keep in mind that when a rocket goes up, it is throwing out the bottom a considerable amount of mass.

      The point here is that by the end of a stage, the acceleration of one of these rockets (solid or liquid fueled... it doesn't matter) can be quite high, and on ICBM's it can be as high as 20 G's or more. Sometimes a payload simply can't handle that sort of acceleration (like people, but some sattelites as well), so you need to drop the amount of thurst to lower the accleration rate.

      This is a mission requirement, and when you design a space payload you also specify what the maximum acceleration will be (usually in m/s^2 but sometimes in different units). When the flight profile is calculated, the rocket will have pre-programmed intervals to scale back the thrust requirements. This makes life fun and interesting, and why rocket scientists get the big $$$.

      The Space Shuttle's Main Engines have this feature, and it is even more important because of the human cargo, as well as bio research materials. I believe the flight profile of the shuttle is to maintain a maximum rate of about 4-5 G's. The Saturn V, by comparison, hit about 8-9 G's at the end of the 1st and 2nd stages.