Stories
Slash Boxes
Comments

News for nerds, stuff that matters

Slashdot Log In

Log In

Create Account  |  Retrieve Password

Golf-Ball Sized Hail Damages Shuttle

Posted by CmdrTaco on Wed Feb 28, 2007 09:15 AM
from the don't-make-me-stop-this-thing dept.
MattSparkes writes "The Shuttles March launch has been delayed to late April after golf-ball sized hail caused 7000 pits and divots in the foam that shields the fuel tank. NASA say it's the worst damage of its kind that they have ever seen, but hail is not a new problem for the agency. In 1982, a hailstorm damaged the sensitive heat shield tiles on the Columbia's wings. The damaged tiles then absorbed about 540 kilograms of rain. Once in space, the orbiter faced the Sun to allow the tiles to dry out."
+ -
story

Related Stories

[+] NASA Optimistic About Fuel Tank Repairs 104 comments
DarkNemesis618 writes "NASA is now optimistic Atlantis' fuel tank will be able to be repaired in Florida. Due to a freak hail storm February 26 that had golf-sized hail chunks raining down on the launchpad put several thousand dings in the foam covering the external fuel tank as well as damaging 28 tiles on Atlantis' wing. 20 of the 28 tiles have been repaired and workers have started sanding down the damaged area of the tank itself. After it was decided that Atlantis needed to return to the VAB, NASA was unsure as to whether or not the tank could be repaired. But after bringing it back and doing more extensive inspections, the tank appeared to be in good enough shape that repairs could be done on the spot and a replacement was not necessary. This will allow for Atlantis to be launched late April for its construction mission to the ISS as well as not interfering with the remaining 4 launches planned this year. If the tank needed to be replaced, Atlantis would not have launched until June at the earliest."
This discussion has been archived. No new comments can be posted.
The Fine Print: The following comments are owned by whoever posted them. We are not responsible for them in any way.
 Full
 Abbreviated
 Hidden
More
Loading... please wait.
  • by Anonymous Coward

    In 1982, a hailstorm damaged the sensitive heat shield tiles on the Columbia's wings. The damaged tiles then absorbed about 540 kilograms of rain.
    Just like my chevy!

    I wonder if they're having problems getting the smell of stale McDonald's & whiskey out of their vehicle too.
  • Obviously (Score:3, Funny)

    by Rob T Firefly (844560) on Wednesday February 28 2007, @09:18AM (#18180670) Homepage Journal
    NASA is not a golfer.
    • Exactly 7000? Sounds like it was intentional.

      (just kidding)
    • Although some of the astronauts have been known to play [newscientist.com].
    • Re: (Score:3, Funny)

      Woo, isn't NASA supposed to be a millionaire?
      • Woo, isn't NASA supposed to be a millionaire?

        No air in space, so it would be more accurate to say NASA is a millionvacuum.
    • by aadvancedGIR (959466) on Wednesday February 28 2007, @10:01AM (#18181138)
      That foam really tied the fuel tank together, did it not?
      • by Rob T Firefly (844560) on Wednesday February 28 2007, @10:26AM (#18181392) Homepage Journal
        You want foam? I can get you foam. Believe me, there are ways, dude..
      • Re: (Score:3, Funny)

        by ajlitt (19055)
        Also, foam is not the preferred nomenclature. Insulation, please.
      • Re: (Score:3, Interesting)

        by racermd (314140)
        Maybe it's just me, and I don't claim to be a super-smrt - sorry, smart - rocket-scientist (because I'm not), but why don't they put the foam insulation on the inside of the fuel tank shell?

        I'm sure there are reasons why they don't, but can those reasons out-weigh the problems it's causing with the foam on the outside?

        Does anyone know if this has been considered? If so, why hasn't it been done, yet? Please be as specific as you can. I'm really interested in this.
        • Re: (Score:3, Informative)

          by Rei (128717)
          It's not just insulation to stop the hydrogen from boiling off; it's also an ablative TPS (Thermal Protection System) for liftoff. You'd melt the aluminium. Furthermore, I would wager that having liquid hydrogen seeping through the insulation would ruin its R-value, if the material is compatable with LH at all (I'd have to check). Plus it'd be harder (read: more expensive, slower) to apply internally. Plus it would take a redesign and recertification of the craft.
          • Re: (Score:3, Insightful)

            One possible reason - save weight. Metal is heavier than foam. Imagine a tank similar to the current one in shape, size, and internal volume. Move the metal to the outside of the foam, you need more metal to cover the greater surface area on the outside of the resulting shape than it does on the inside of the current tank, hence more weight.

            re: the liner idea - yeah, the tank was painted white for the first two or three launches. They got rid of the paint to save weight - apparently covering the foam wi
    • by saboola (655522) on Wednesday February 28 2007, @10:05AM (#18181178)
      What they need is The Ding King! [dingking.tv]. (As Seen On TV!)
  • by bad_fx (493443) on Wednesday February 28 2007, @09:20AM (#18180686) Journal
    [quote]NASA has had less serious problems with fuel tank foam as well. In 1995, a shuttle on the launch pad had to be returned to its hangar for repairs after woodpeckers punched about a dozen small holes in the tank's insulation.[/quote]

    That got a bit of a chuckle; It's in the article linked from TFA.
    • Ok, so they should move the launch site to somewhere where they don't get stupidly large hailstorms, massive amounts of ice, super strong winds! (and is barren of trees, too).

      I mean, is it me, or did they get sold some 'prime real estate' to build the launch centre?
      • Re: (Score:3, Informative)

        by saboola (655522)
        Here ya go, right from the pedia:

        Cape Canaveral [wikipedia.org]

        Cape Canaveral was chosen for rocket launches to take advantage of the earth's rotation. The centrifugal force of this rotation is greatest at the equator, and to take advantage of it, rockets are launched eastward, in the same direction of the earth's rotation. It is also highly desirable to have the downrange area sparsely populated, in case of accidents; an ocean is ideal for this. Although the United States has sites closer to the equator with expans
  • Paradigm shift (Score:5, Interesting)

    by TWX (665546) on Wednesday February 28 2007, @09:21AM (#18180698)
    Maybe there really is something to all of those science fiction movies that show space ports opening like a clamshell a few minutes before the spacecraft lifts off, especially if the air inside was temperature and humidity controlled. That kind of thing might have prevented Challenger's destruction and would keep any craft free from weather-related damage before takeoff...
    • Re:Paradigm shift (Score:5, Informative)

      by hcdejong (561314) <acmeNO@SPAMxmsnet.nl> on Wednesday February 28 2007, @09:45AM (#18180940)
      The only problem with that is keeping the clamshell (and the whole building) from being blasted to smithereens during takeoff. The noise level alone is enough to crumble concrete, add to that the temperature and pressure, and you see why rockets are usually launched in the open. True, missiles are often launched from canisters or silos, but:

      1. Smaller missiles often use a cold-gas ejection system. The motor doesn't ignite until the missile is out of the canister. Some systems (e.g. Mk 41 VLS) ignite the missile in the canister. In this case, the canister consists of an inner tube that contains the missile, and a fixed outer tube. When reloading, the inner tube is replaced. This is doable for a missile, not so much for a Shuttle-sized rocket.

      2. For larger missiles (ICBMs), a reusable launch site isn't the top priority. Damage to the silo is more acceptable here than for a NASA launch facility.
      • The Shuttle's launching off the Mobile Launcher Platform [wikipedia.org]. Unlike a clamshell it's directly below the exhaust and it is even mobile (as the name implies; btw. the parts of the clamshell would need to be "mobile" as well, to open and close that thing, but unlike the MLP the engines wouldn't need to be 5m below the SLBs.
        • The platform isn't an enclosed structure, so there's no pressure buildup. And they need 1.2 million litres of water to protect the platform (and the rest of the launch pad) during the launch. The water absorbs the heat and vibrations. A large fraction of the water is converted to steam in the 20 seconds or so from ignition to clearing the tower.
      • Nah... look at Thunderbirds. Q whacking great underground chamber that opens up just prior to launch. of course, you need to allow some time for all the NASA employees to exit the giant swimming pool before it slides out of the way ;-)
      • by Lumpy (12016)
        When reloading, the inner tube is replaced. This is doable for a missile, not so much for a Shuttle-sized rocket.

        Bah!, a foam or plastic sabot for the shuttle will solve that problem. Rifling the barrel will also help in the accuracy as well.
      • For a miserly 5,000,000 per launch, I will personally setup a gigantic tent around the Shuttle and then will dismantle it about 2 hours before the launch ;)
      • a reusable launch site isn't the top priority. Especially as it is assumed the silo is going to get hit by an incoming MIRV, which will do more damage than any launch would do.
    • Re:Paradigm shift (Score:5, Informative)

      by 140Mandak262Jamuna (970587) on Wednesday February 28 2007, @09:51AM (#18180998) Journal
      ISRO has fixed launch pads and the Vehicle assembly building moves on rails out of the way for launch. NASA has a fixed Vehicle assembly building and the rocket moves on very complex tracked vehicle a few miles to the launch site. So far ISRO has not launched anything the size NASA has. The largest payload by ISRO, a six ton Low earth orbit, 1 ton Geostationery payload (quoting from memory, pardon errors) is very small compared to what NASA has done. So the building capable of assembling something the size of space shuttle cant easily move out of the way. But the could try to create a simpler building mainly to protect the vehicle without all that expensive jigs and assembly equipment that moves out of the way on the day of launch. They would not really like to have a fueled vehicle inside a building.
    • Re: (Score:3, Interesting)

      by Mercano (826132)
      How about, say, something like this [wikipedia.org]? Though I don't know how early in the countdown then need to roll back the building.
    • by sconeu (64226)
      IIRC, that's what the shuttle facilities at Vandenberg were going to be. The stack would be raised in situ at the pad, and the "VAB" would roll away on both sides at some point during the countdown.
      • When they're not being used for spacecraft, we can use them for giant robots!
        "...and I'll form The Head!" *queue giant sword and majestic Voltron music*
      • Re:Hanger Queen (Score:4, Informative)

        by Rei (128717) on Wednesday February 28 2007, @01:55PM (#18184332) Homepage
        No, it just goes to show how easily people ignorant of the difficulties of getting to orbit can make fun of those who actually have to deal with them. Rockets must be built incredibly light. Unfortunately, for the time being, this means flimsy. Even an extra coating of paint could kill the amount of payload they could take up.

        Also, in constant dollars, the Apollo Saturn V stack was probably more expensive; it depends on how you do your accounting. And it, too, was vulnerable to weather. NASA was simply braver (perhaps crazier) back then. They even launched once during a thunderstorm -- Apollo 12. I love the logic of that one. There's a thunderstorm, and we have a gigantic vehicle full of explosive fuel, made of highly conductive metal. Lets have it launch so that it gets up to the charge layer, with a trail of ionized exhaust gas leading straight to the ground. ;) When it was struck by lightning, it nearly caused the termination of the mission -- knocked the fuel cells offline and scrambled the data from the navigational computer. Thankfully, the computer damage could be worked around due to an electrical engineer in Mission Control who knew a workaround.
  • Rain (Score:4, Interesting)

    by saskboy (600063) on Wednesday February 28 2007, @09:23AM (#18180718) Homepage Journal
    So Columbia survived a half a ton of rain in its fragile shield, but was brought down by scarring foam. How odd space flight can be...
    • Re: (Score:3, Interesting)

      by Anonymous Coward
      What is more shocking is the fact that they deliberately took up half a ton of water up into space.

      I wonder how much such a worthless payload costs in terms of fuel needs.

      Would it not have been cheaper to dry the shuttle while on earth? and spare a couple of hundred liters of fuel?
    • by hey! (33014)
      I suppose it's because so much of engineering boils down to finding the most applicable of proven solutions. "Proven" is always relative to a set of assumptions. You might not even know what the relevant assumptions are until they are violated. It is important for engineers to pay attention to intuition, but you can't actually trust it, especially in unusual situations.
  • in a few wee Kevlar umbrellas. For the price of this shading material, which they discovered they needed more than TWO DECADES AGO, they wouldn't have multi-million dollar dent problem.
  • Exactly how hard... (Score:3, Informative)

    by joshetc (955226) on Wednesday February 28 2007, @09:31AM (#18180792)
    Exactly how hard is it to just cover the damn thing? I would think after spending so much money on something NASA would want to take care of it...
  • hang on... (Score:5, Funny)

    by symes (835608) on Wednesday February 28 2007, @09:32AM (#18180816) Journal
    Golf balls [wikipedia.org] have bumps and divots over the surface to enable longer flight times. Surely these additional bumps will also aid the shuttle's aerodynamics?
    • Golf balls have bumps and divots over the surface to enable longer flight times. Surely these additional bumps will also aid the shuttle's aerodynamics?

      Only if you're going to be whacking it with a giant hammer that's also designed to give it backspin. But that's the kind of stuff NASA wants to avoid.

    • by Scutter (18425)
      Golf balls have bumps and divots over the surface to enable longer flight times. Surely these additional bumps will also aid the shuttle's aerodynamics?

      I hear they're planning on painting red racing stripes on it, too, to make it go faster.
  • by DaveV1.0 (203135) on Wednesday February 28 2007, @09:34AM (#18180826) Journal
    All those damned retirees and there golf. Worse than kids, I tell ya!
  • I'm confused. Why would the space shuttle's heat shields need to face the sun in order to dry out water? There's no pressure in orbit. Surely water under no pressure is vapour?
    • Re: (Score:3, Insightful)

      by imsabbel (611519)
      Evaporation enthalpy.

      At 80 Kelvin, ice will be fine even in ultrahigh vacuum. So energy has to come from somewhere to allow the ice to evaporate. Those headshields are very good insulators, which leaves the sun as energy source.

    • by eln (21727)
      I'm no expert, but I'd imagine the reason they don't built it that way is weight. Heck, they even stopped painting it to save on weight.
    • >Not to be anal but you cannot measure a liquid in kilograms
      Sure you can. Stick a big bucket on some scales, fill it until the scales say 540Kgs. Not the best way of measuring it, to be sure, but you can do it.
    • Re: (Score:3, Informative)

      by Rakishi (759894)
      It's unlikely that they knew the volume but this being a rocket the mass was measurable. While you can calculate the volume from the mass, due to the rain not being perfectly pure and the temperature not being 4C the volume will not be exactly 540 liters even if the mass is exactly 540 kg (at room temp it'd be ~537 by my calculations).
        • Sorry, but spaceflight is one of those occassions where there is a rather distinctive difference between weight (N) and mass (kg).
          Hint: in orbit, the stuff still was 540Kg, but 0N....