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posted by Fnord666 on Tuesday March 14 2017, @04:43PM   Printer-friendly
from the are-the-questions-about-woodchucks? dept.

Located at the Las Campanas Observatory high in the Andes mountains of northern Chile, GMT [Giant Magellan Telescope] will be the world's largest astronomical telescope. The project is being developed by an international consortium of universities and research institutions in the U.S., Australia, Brazil, and South Korea.

GMT was designed to be a segmented mirror telescope that employs seven of today's largest stiff monolith mirrors as segments. Its six off-axis 8.4-meter segments will surround a central on-axis segment, forming a single optical surface 24.5 meters in diameter with a total collecting area of 368 square meters.

GMT is expected to be operational for many decades, enabling breakthrough science ranging from studies of the first stars and galaxies in the universe to the exploration of extrasolar alien worlds. Shelton believes that GMT has the potential to even revolutionize our understanding of astronomy.

"The GMT is poised to answer some of humanity's biggest questions about the nature of exoplanets and whether we are alone in the universe, about the beginning of the universe to understand the formation and evolution of the galaxies, about the origin of the chemical elements, and how black holes grow. The biggest discoveries that will be made by the GMT, however, will be the unexpected results that revolutionize our understanding of astronomy," Shelton told Astrowatch.net.

They may or may not put Jodie Foster in charge.


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  • (Score: 2) by Runaway1956 on Tuesday March 14 2017, @05:35PM (6 children)

    by Runaway1956 (2926) Subscriber Badge on Tuesday March 14 2017, @05:35PM (#479004) Journal

    They spend all that time, energy, and money building a better telescope - on earth.

    How 'bout they design the biggest, bestest, state of the art telescope, and send it into space?

    Yeah, it would be damned expensive. The necessity of launching the components into space would require that they be pretty tough, and that they be properly protected from the stress of takeoff. But - the world's biggest and bestest, in space. No light pollution to worry about. No deterioration from the elements. Moisture will never be a problem. No passers-by, on the ground or in the ari. No tourists begging for the opportunity to come inside to admire the equipment. Just a huge telescope, hanging on nothing, at least a few thousand miles from earth. The earth itself will obstruct only a small portion of the sky at any time, compared to most of the sky all the time here on earth. And, it can run 24/7 since there's no sunrise and no sunset.

    Then, a meteorite wipes out my dream, right?

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  • (Score: -1, Offtopic) by Anonymous Coward on Tuesday March 14 2017, @05:45PM

    by Anonymous Coward on Tuesday March 14 2017, @05:45PM (#479010)

    Can't. Those thieving Mexicans and towel heads, who certainly aren't migrants (nor is Mexican or towel head a race!), are stealing our space stuff.

  • (Score: 2) by fishybell on Tuesday March 14 2017, @05:54PM

    by fishybell (3156) on Tuesday March 14 2017, @05:54PM (#479015)

    It's not an either-or situation. They do both, typically (I'm looking at you Hawaii) only time and money restricting.

  • (Score: 2) by bob_super on Tuesday March 14 2017, @06:03PM

    by bob_super (1357) on Tuesday March 14 2017, @06:03PM (#479019)

    Considering the budget and delays of both Hubble and Webb, and the short lifespan of the latter (if it doesn't blow up on the way), I can understand why the safe bet of the Atacama is the favored choice.
    It would make sense to assemble a few telescope modules on the other side of the moon, which gives most of the benefits you want except super-long exposure times (under a couple weeks), though power could be an issue when it's dark for a couple weeks.

  • (Score: 3, Informative) by takyon on Tuesday March 14 2017, @06:38PM

    by takyon (881) <takyonNO@SPAMsoylentnews.org> on Tuesday March 14 2017, @06:38PM (#479048) Journal

    How many times do we have to mention adaptive optics? It's not a new concept.

    https://en.wikipedia.org/wiki/Adaptive_optics [wikipedia.org]

    An adaptive optics system tries to correct these distortions, using a wavefront sensor which takes some of the astronomical light, a deformable mirror that lies in the optical path, and a computer that receives input from the detector. The wavefront sensor measures the distortions the atmosphere has introduced on the timescale of a few milliseconds; the computer calculates the optimal mirror shape to correct the distortions and the surface of the deformable mirror is reshaped accordingly. For example, an 8–10 m telescope (like the VLT or Keck) can produce AO-corrected images with an angular resolution of 30–60 milliarcsecond (mas) resolution at infrared wavelengths, while the resolution without correction is of the order of 1 arcsecond.

    https://en.wikipedia.org/wiki/Giant_Magellan_Telescope [wikipedia.org]

    The Giant Magellan Telescope (GMT) [...] is expected to have the resolving power 10 times greater than the Hubble Space Telescope

    Certain wavelengths penetrate the atmosphere better than others, and thus while a gigantic space telescope would be preferred, the cost/size advantage on the ground combined with the ideal wavelengths and corrective adaptive optics makes the ground telescope superior to the space one, for the moment.

    --
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  • (Score: 5, Informative) by khallow on Tuesday March 14 2017, @07:17PM (1 child)

    by khallow (3766) Subscriber Badge on Tuesday March 14 2017, @07:17PM (#479081) Journal

    How 'bout they design the biggest, bestest, state of the art telescope, and send it into space?

    Because you multiply the cost by at least a factor of ten without getting ten times the science. Let's consider what it would take to put a telescope with a resolving power of a 24.5 meter telescope in orbit. First, just as on Earth, the mirror is too large to launch as a single unit for a couple of reasons. First, it's just too wide to fit in current rockets which typically has a cargo space 3-5 meters wide. Even the propose near future Falcon Heavy would have a maximum fairing size at or below 8 meters and the SLS perhaps 10 to 12 meters.

    Second, most of the mass scales roughly as the cube of the radius of the mirror (mirror and tube size in particular). The Hubble telescope massed 11 metric tons (Mt) for a mirror just under a third the size of the GMT (the GMT had an effective light gathering power 10 times as great as the Hubble). So we're looking at roughly a factor of 30 more mass, if we build the telescope in the same manner as Hubble and scale everything up, we're looking at a 300 Mt telescope in orbit. Once again, nothing launches anywhere near that amount. In theory, the SLS will eventually be able to launch around 130 Mt which may work, if enough mass can be trimmed. But a launch of the full vehicle will be at least a decade away from now (if ever) and it'll probably cost the better part of a billion dollars just by itself (I'd wager on the wrong side of a billion dollars, but we'll see).

    If we were to somehow break up this telescope and launch it on a fully reusable Falcon Heavy to low Earth orbit (LEO), the cost per kg, just for launch, might be as low as $1000 per kg, which would mean a launch cost of $300 million. For a more realistic $2-3k per kg for a rocket that isn't fully reusable, it's $600-900 million just in launch costs to LEO.

    I'll note here that while I haven't discussed any technical details of the space telescope aside from rough guesses about its mass, I have observed that launch costs tend to be a reliable piece of the overall cost, between 5-20% of the overall cost of the mission. The reason I believe this would be consistent even for a completely undetermined space telescope mission is that there is a huge trade off [arxiv.org] between mass and cost at the optimization levels of space science missions. "Low cost" payloads will refer to payloads that have a high portion of their costs in launch costs, up to the 20% figure I mentioned earlier. "High cost payloads" would have far lower portion in launch costs (5-10% for purposes of this post).

    If we assume that the space telescope is a low cost payload, then overall cost might be a factor of five higher than the launch costs ($1.5-4.5 billion). I believe here that like the Hubble and James Webb space telescopes, it'll be a high cost payload with cost about a factor of 10-20 more than launch costs. Then of course, overall costs could be much higher, up to $18 billion by my above calculations.

    Then if we look at the technical aspects of the space telescope, we're looking at complex assembly and vibration issues. Current telescope design relies strongly on both rigid optics and almost complete elimination of alignment and vibration issues. The more pieces of telescope that you have to assemble, the more complicated that part of the process will be, and the more vibration issues you introduce. And needless to say, we don't have a lot of experience with assembling things in space, much less a telescope with hard tolerance thresholds.

    In theory, a crude parabolic-shaped, vibrating sheet of mylar would suffice - as long as you know within a small fraction of a wavelength what the shape of the mirror is at any given moment (and aren't too concerned about any Doppler effects from having the mirror move like that). Then you can computationally apply a transformation filter to the optical output to reverse the effects from deviation from the perfect parabolic shape and get a near optimal image from the system.

    To summarize the benefits and costs, you're observing above most of the atmosphere which does help particular with UV and infra red imaging, both which are more strongly absorbed than visual light and have a longer observation day (by about a factor of three or so, depending on weather, etc). And you don't have to deal with light scattering in atmosphere (which is responsible for a variety of headaches including light pollution and stellar scintillation or star twinkling). But you exchange that with the above higher cost problem, a lower lifetime (several working telescopes are a century or older while the Hubble telescope has been active for about 27 years only due to numerous expensive repair missions), and a lack of repair and upgrade options that Earth-side instruments have.

    In practice, anything you can do in space, you can do for lower cost on the ground. The workarounds may sound clumsy (such as adaptive optics and building on top of a tall mountain in the Andes range), but it's still vastly cheaper than trying the same thing in space.

    • (Score: 0) by Anonymous Coward on Tuesday March 14 2017, @10:46PM

      by Anonymous Coward on Tuesday March 14 2017, @10:46PM (#479177)

      If you're willing to wait till it's ready, SpaceX's ITS (previously MCT) may be the most economical choice -- with 12m diameter stages and a maximum diameter of 17m for the intended spaceship, a cargo fairing of 20m might be feasible, and it will lift 300t to LEO in fully reusable (=cheap) mode.

      Still, it's a hard sell -- I think it's better, given the state of adaptive optics, to mostly ignore LEO for telescopes, and focus on Earth-based telescopes (and the wavelengths they can observe) for now. Once we have the manufacturing and support capabilities in place, whether that's on the moon's surface, in high orbit, or at lagrange points, we'll be able to can build some truly gargantuan instruments out there.