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Messenger En Route To Mercury

Soft writes "NASA's Messenger space probe has lifted off on its second try on a Delta 2-Heavy rocket. As mentioned earlier on Slashdot, it is poised to orbit Mercury in 2011 after three flybys, as well as two flybys of Venus and one of Earth for course corrections. It will be the first probe to visit the innermost planet since Mariner 10 in 1974 and 1975. Stories on the BBC and SpaceflightNow."

120 comments

  1. 2011? by Anonymous Coward · · Score: 5, Funny

    Not exactly Instant Messenger, is it?

    1. Re:2011? by EachLennyAPenny · · Score: 0

      Brought to you by TimeWarnerNasaAol.

    2. Re:2011? by chris_sawtell · · Score: 1
      Not exactly Instant Messenger, is it?

      Indeed not, as far as I can tell it seems to be a time machine of some sort. Quoting verbatim with my emphasis.

      If all goes well, MESSENGER's main engine will fire for 15 minutes on March 18, 2001, putting the spacecraft into an elliptical orbit tilted 60 degrees to the planet's equator with a low point of about 125 miles above the northern hemisphere and a high point of 9,420 miles.
    3. Re:2011? by essreenim · · Score: 2, Interesting

      Yeah. I _KNOW_ my grandmother could get there before then. I know orbital mechanics is tricky because trying to enter orbit around Mercury is difficult with the immense speed generated by travelling towards the sun ... but come on.
      What this is like everything is a money dictated project i.e the Messenger guys have none and have had to come up with a low cost lengthy gravity controlled trip ..blah blah blah.
      Come on Nasa, start working on cutting down your mission times..

    4. Re:2011? by LooseChanj · · Score: 1

      It's harder than that, because you have to slow down enough to even get to that "immense speed generated by travelling towards the sun".

      --
      Mix the failings of Usenet with the shortcomings of the World Wide Web and the result is slashdot.
    5. Re:2011? by Lord+Omlette · · Score: 2, Funny

      It'll have to put up an away message for quite some time.

      --
      [o]_O
  2. Men are from Mars, Women are from.... by Andy+Mitchell · · Score: 1, Funny

    Men are from Mars, Women are from Venus and Small furry creatures are from Alpha Centauri.

    So what the heck is there on Mercury? :-)

    1. Re:Men are from Mars, Women are from.... by pklong · · Score: 1

      Nothing, but is is the Winged Messenger in itself.

      --

      Philip

      Signatures are broken

    2. Re:Men are from Mars, Women are from.... by adeyadey · · Score: 0

      Dental Amalgams and thermometers..

      --
      "You lied to me! There is a Swansea!"
    3. Re:Men are from Mars, Women are from.... by Anonymous Coward · · Score: 0

      Harmoniums, as any Vonnegut reader knows.

  3. I thought we knew this bit already . . . by StateOfTheUnion · · Score: 4, Interesting
    From the Spaceflight Now

    How did Mercury, believed to be 60 percent iron, end up with an oversize core, a thin shell of a crust and the highest density in the solar system? Was its crust blasted away in the distant past by a cataclysmic impact? Was it boiled away in the extreme heat of the young, nearby sun? Or were metals for some reason concentrated in the inner region of the solar nebula that coalesced to form the sun and planets?

    Perhaps my knowledge is a little dated, but I thought that the inner four planets have higher density because the sun stripped the inner solar system of light gasses like hydrogen due to the larger mass and higher gravitational field of the sun during the formation of the sun and the solar system. Outer planets are gas giants because the Sun's (or the pre-sun center of the accretion disk ) gravitational field was not strong enough to grab the light elements from the portion of the solar system that would become the gas giants (further from the center of the pre solar system accretion disk). Also, this was thought to be why Pluto is an oddball (far away from the sun, but a frozen rock of a planet) that might be an escaped moon or oort cloud refugee.

    Can anyone confirm this? Or am I citing stone age planetary science that is no longer valid?

    1. Re:I thought we knew this bit already . . . by el-spectre · · Score: 4, Interesting

      I think your science is right... what the article seems to be emphasizing is the massive iron content... Earth, whilst having an iron core, is still mostly silicon and oxygen (the mantle & crust). For some reason Mercury has more than it's fair share of iron core, compared to other inner planets. 'tis puzzling.

      --
      "Faith: Belief without evidence in what is told by one who speaks without knowledge, of things without parallel." - A.B.
    2. Re:I thought we knew this bit already . . . by Anonymous Coward · · Score: 2, Interesting

      According to the Messenger website you are largely correct, the absence of lighter gpI&II metals is down to them simply boiling away from the crust. However it goes on to say that this is unconfirmed _theory_ and one purpose of the mission is to collect more evidence to confirm/deny this. The other theory is that physical activity (impacts) have blasted away most of these elements from the early crust.

      On a sceptical note, I question the value of such a mission. Mercury is going to remain beyond our reach for many centuries so whatever we find there is of theoretical value only, and I wonder whether advances in spectroscopy and remote analysis will soon overtake the value of a probe mission.

    3. Re:I thought we knew this bit already . . . by mazarin5 · · Score: 2, Informative
      It's not so much that gas is pulled to the Sun easier, rather than it's harder to get hydrogen and helium to stay solid when large clumps of it collide. It sublimates and it's momentum is distributed. This makes it hard for the gases to build up to the velocities that planets have. With lower velocities they fall to lower orbits, most likely becoming part of the Sun.

      As far as Mercury, it is so close to the Sun that the solar wind is strong enough to blow away any atmosphere it has. It also has a very low mass, and so it has trouble resisting this. Any dust wouldn't settle into rock formations due to a lack of pressure, and would be hardly held down by the low gravity. Look at the dust storms on Mars, which is significantly larger. So dust and light materia are blown away also. This leaves a very solid, very dense core of nickle, and whatever heavy material might survive the heat of the nearby star.

      --
      Fnord.
    4. Re:I thought we knew this bit already . . . by pedroloco · · Score: 5, Informative

      Mercury is real hard to observe from Earth-based telescopes since it is so close to the Sun. In the near future, the only way to get higher resolution data is to send the telescopes to Mercury. Even the most fervent remote sensing advocate will have to admit that data quality generally improves with decreasing distance to the target.

      Using martian studies as an analogy for mercurian (hermitian?) observations, one can see how spacecraft data provide much more detailed observations over ground-based observations. Earth-based data of Mars obtained during the last opposition last summer (when Mars was closer to Earth than Mercury ever gets) does not compare to spacecraft data in terms of resolution. Earth-based (visible-wavelength) observers of Mars have to content themselves with seeing albedo variations. The geology which caused those albedo variations was largely unknown prior to our sending spacecraft. (Please note that tha "canals" reported by Lowell were likely optical illusions - Lowell's canal maps do not correspond to locations of known martian dry channels.)

      Similarly, Earth-based spectroscopic observations of Mars have poor spatial resolutions. I remember one paper from '96 which reported 300 km/pixel resolutions. Two spectrometers currently in orbit around Mars get far better spatialresolution (Thermal Emission Spectrometer gets 3 km/pixel; THEMIS-IR gets 100 m/pixel - although, granted, that's with a low spectral resolution).

      Two advantages that Earth-based observations have over spacecraft data are: 1) Earth-based observations are a lot cheaper to obtain and 2) a network of Earth-based observers can look for changes in the target with better time continuity than a singe spacecraft (since the spacecraft may be looking at some other part of the planet).

      The true value of a Mercury mission is two-fold. Most obviously, new spacecraft observations will provide geologic context for current ground based observations (Mariner 10 only imaged ~40% of the planet). Additionally, Mercury is considered an end-member planet - a planet that likely formed close to the Sun in the solar nebula from which the solar system formed. As such, understanding how Mercury formed will provide a calibration point for models of solar system formation, which could have implications for formation in other portions of the solar nebula or the early solar system or of other planetary systems.

      No, we aren't going to be sending people to Mercury anytime soon, but neither are we going to be sending people to Mars in the near future. (Even Bush's space initiative doesn't plan a Mars landing for at least 20 years - plenty of time to get distracted by other problems.) However, even if people aren't going to those placed, there are still useful things to learn regarding the solar system in which we live.

    5. Re:I thought we knew this bit already . . . by Anonymous Coward · · Score: 2, Informative

      You're close, but not quite. It wasn't that the sun's gravity pulled in the lighter elements from the inner planets, but rather, that the solar wind from the sun blew all the lighter material outward, towards the outer solar system (which is why there was so much of it available to form the gas giants). You just have your vacuum in the wrong direction ;).

    6. Re:I thought we knew this bit already . . . by DMUTPeregrine · · Score: 1

      Could it just be very magnetic? That would make it stick faster.

      --
      Not a sentence!
    7. Re:I thought we knew this bit already . . . by CheshireCatCO · · Score: 2, Interesting

      Not quite, no.

      The inner planets are rocky/metallic because it was too hot for ices to form. Most of the proto-solar disk would have been in the form of hydrogen and helium. The next most abundant elements are oxygen, carbon, and nitrogen. With so my of these and hydrogen, hydrogen compounds (water, ammonia, methane) can do a lot of planet building if they can form solids. Near the proto-Sun, it would habe been too hot for this to happen. Somewhere around 5 AU, water ice could first freeze out. Not surprisingly, you find jovian planets starting around that point. (They have the gases because they were able to get large enough fast enough to trap some of the gas in the disk before the disk dissipated. The terrestrial planets are too small to accomplish this because they never had enough solid materials around to build themselves with.)

      You would have found that the composition of the proto-solar disk was probably pretty uniform. The acceration of gravity is higher near the center thanks to the proto-Sun, but that's a red herring. The acceleration is balanced by the orbital motion. The mass of the orbiting object doesn't factor into the motion, so hydrogen gas orbits the same as rock particles. (Well, almost. Gases are subject to gas pressures, but that wouldn't make them move inward or outward, it just slows their orbital speed some.)

    8. Re:I thought we knew this bit already . . . by Anonymous Coward · · Score: 0
      Mercury is real hard to observe from Earth-based telescopes since it is so close to the Sun.
      Why don't they observe it at night then? :-)
  4. Messenger's telemetry log... by vudufixit · · Score: 4, Funny

    8-2-3004 2:15:56.537 EST: Departure Scan, Cape Canaveral 9-5-2005 Scan Venus gravitational assist 4-22-2008 Scan First flyby 12-14-2009 Scan Second flyby 6-12-2010 Scan Third flyby 2-01-2011 Scan Orbital Insertion ADDRESSEE NOT HOME, SIGNATURE WAIVED

    1. Re:Messenger's telemetry log... by Anonymous Coward · · Score: 0

      Informative.

      "ADDRESSEE NOT HOME, SIGNATURE WAIVED": +1, Informative.

      Man, I wish I could get me some of that moderator crack...

    2. Re:Messenger's telemetry log... by vudufixit · · Score: 1

      I'm the one who made the silly comment, and even I didn't want the "+1 informative!"

  5. Re:Second try? by Kiryat+Malachi · · Score: 4, Informative

    When a launch is canceled due to mechanical failures, weather, or any other reason, it's considered a try as long as the launch procedure has been started. Since launch procedures can range from 6 hours to 6 days, there are a lot more tries than launches.

    Yoda wisdom or no Yoda wisdom, you're still wrong.

    (With rockets, if you try and don't succeed, its pretty much SOP - most things don't launch on the first attempt. Now, if you were to say "ignite" instead of try, you'd be correct - most rockets don't do too well on a second ignition.)

    --

    ---
    Mod me down, you fucking twits. Go ahead. I dare you.
    (I read with sigs off.)
  6. Re:that long? by ufoman · · Score: 4, Informative

    The spacecraft cannot fly straight to Mercury; it does not carry nearly enough fuel. So it will fly once past Earth, twice past Venus and three times past Mercury and make 15 loops around the sun before slowing enough to slip into orbit around the small, hot planet.

    --
    The following statement is false.
    The previous statement is true.
    Welcome to my world.
  7. Mercury is toxic by hugesmile · · Score: 1, Funny
    This is a very bad idea - going to Mercury and back to Earth. Haven't they read that Mercury is toxic

    Next they'll try to return from Saturn with car parts.

  8. Re:Second try? by tcdk · · Score: 1

    You are correct, except the write up says:

    NASA's Messenger space probe has lifted off on its second try on a Delta 2-Heavy rocket

    Which ties "lift off" and "try" dangerously close to each other.

    And notice how you use the word "attempt" instead of "try". "Try" is simply the wrong word to use when talking about launching rockets. There's a big difference between "trying to launch" and "making a launch attempt".

    --
    TC - My Photos..
  9. Service Pack One by syntap · · Score: 2, Funny

    Too bad this isn't Microsoft Messenger... they could apply service packs to Mercury and give it an atmosphere.

    1. Re:Service Pack One by Kizzle · · Score: 0

      Microsoft + ??? = Funny Slashdot Joke!!!

    2. Re:Service Pack One by Anonymous Coward · · Score: 0

      BSOD = Blue Sky Of Death ?

  10. planet inside mercury orbit by ch-chuck · · Score: 3, Interesting

    maybe now they'll finally find Planet Vulcan

    --
    try { do() || do_not(); } catch (JediException err) { yoda(err); }
    1. Re:planet inside mercury orbit by Anonymous Coward · · Score: 0


      maybe now they'll finally find Planet Vulcan


      Didn;t you know? It disintegrated into an asteroid field.

  11. What Messenger Really Stands For . . . by StateOfTheUnion · · Score: 4, Informative
    According to JPL

    MESSENGER stands for MErcury Surface, Space ENvironment, GEochemistry and Ranging

    1. Re:What Messenger Really Stands For . . . by Anonymous Coward · · Score: 0

      And "stands for" stands for "STandard Accumulated Neutrino Density in Solar Field Of Radiation".

    2. Re:What Messenger Really Stands For . . . by Anonymous Coward · · Score: 0

      ACRONYM: Abbreviated Coded Rendition Of Name Yielding Meaning

      ...has to be my favourite.

    3. Re:What Messenger Really Stands For . . . by LrdHlmt · · Score: 2, Informative

      Also, Mercury (the god) is also called "The Winged Messenger" in Roman mithology. Hence the acronym picked for the mission.

    4. Re:What Messenger Really Stands For . . . by p3d0 · · Score: 1

      Meanwhile, MERCURY itself stands for Mineral Encrusted Round Conglomeration that is Uneven and ReallY hot.

      --
      Patrick Doyle
      I mod down every jackass who puts his moderation policy in his sig. Oh, wait a sec....
    5. Re:What Messenger Really Stands For . . . by p3d0 · · Score: 1

      Sorry, that was a bit obscure. What I'm trying to say is that MESSENGER makes for a pretty contrived acronym.

      --
      Patrick Doyle
      I mod down every jackass who puts his moderation policy in his sig. Oh, wait a sec....
  12. 2011? How long with ion drives? by adeyadey · · Score: 4, Interesting

    I dont understand why solar-powered ion drives are not used on missions like this. Probes like the ESA SMART-1 has shown that such craft can be small & economical, and there is an abundance of solar power available for free. I understand that final orbital insertion can be a problem - could a solar ion drive deliver enough "punch", or would a supplemental booster be needed? Otherwise I understand that solar would be way more fuel/time efficient over a few years compared to carrying rocket fuel & hanging around for gravity slingshots. Am I right?

    I have even read of deep-space solar-powered mission designs that head in inside mercurys orbit, grab loads of power and then head out beyond Jupiter..

    Why arnt ion drives used more?

    --
    "You lied to me! There is a Swansea!"
    1. Re:2011? How long with ion drives? by mihal · · Score: 2, Informative

      Though ion drives are really effective in terms of specific impulse (you need little fuel for gaining unit momentum), they are not much mass-effective (thrust per unit engine mass) at all. a trip to Mercury is a kind of parachute jump, you have to go really slowly or you're Sunburnt :). so if you want to get there faster, you first have to accelerate, and step on brakes afterwards. Russians say -- going slowly, get farther. :)

      --
      Sig. No Sig.
    2. Re:2011? How long with ion drives? by adeyadey · · Score: 3, Informative

      ..They are not much mass-effective (thrust per unit engine mass) at all.

      Current Ion drives can deliver >10x more power overall per Kg compared to rockets - but they do it slowly, over months/years.. Rockets can deliver "punch" at a spacific time. Advantages/Disadvantages both ways really.

      Messanger as-is carries 1/2 its weight as fuel, so if you can reduce that 10 fold, or get 10 times the power, thats a good thing. Faster missions are less expensive in terms of keeping support staff too, and less risky. I think a solar-ion mission that spirals inwards as it decelerates would be way more efficient than the current plan. And would be much less dependant on celestial mechanics for launch dates.

      Anyone from NASA here know why they dont use solar-ion drives for these missions? Is there some sort of political bias against solar & pro old fashioned rockets or nuclear? (And yes, I know nuclear (RTG) is needed for deep space - at least for electric power for the science instruments..)

      Here is a better link for SMART-1..

      --
      "You lied to me! There is a Swansea!"
    3. Re:2011? How long with ion drives? by RailRide · · Score: 1
      Current Ion drives can deliver >10x more power overall per Kg compared to rockets - but they do it slowly, over months/years.. Rockets can deliver "punch" at a specific time. Advantages/Disadvantages both ways really.

      I'm no rocket scientist, but I don't think I'd want to depend on a thruster that takes that long to develop it's 'punch' for braking while headed toward something as close to the Sun as Mercury.

      It just has "oops" written all over it :)

      ---PCJ

    4. Re:2011? How long with ion drives? by Cujo · · Score: 3, Informative

      Not power - specific impulse, which is effectively propellant ejection velocity.

      Usually specific impulse is given in units of seconds, but this is an archaic convention - it's really velocity (they divide by the acceleration of gravity at ea level to get seconds).

      There are two major problems with ion propulsion - ion thrusters need Kilowatts of power to operate (and so drive the design, mass and cost of the power subsystem), and they have very low thrust. They are also expensive and have limited life. So with ion propulsion, like everything else in engineering; if it's not necessary to do it, then it's necesary NOT to do it.

      --

      Helium balloons want to be free.

    5. Re:2011? How long with ion drives? by antispam_ben · · Score: 1

      Usually specific impulse is given in units of seconds, but this is an archaic convention - it's really velocity (they divide by the acceleration of gravity at ea level to get seconds).

      Thank you for that simple but insightful bit of information. I regret I have no moderation points to give you.

      I've never really understood "rocket science" even though I still remember the mechanics and physics I learned in college. Is there a good website that explains the calculations, and especially any more unobvious terms such as "seconds of specific impulse"?

      --
      Tag lost or not installed.
    6. Re:2011? How long with ion drives? by Cujo · · Score: 1

      Probably - JPL had a "Space Mechanics" tutorial online once - probably still do.

      --

      Helium balloons want to be free.

    7. Re:2011? How long with ion drives? by CXI · · Score: 3, Informative

      Why arnt ion drives used more?

      To put it in simple non-technical terms, you can't slow down fast enough. Yes, you can get a good bit of speed up over several months on a more direct trajectory, but you'd end up having to start slowing down once you're only 1/2 way there.

      To make it at all reasonable, you'd have to use a few gravity sling-shots to build up speed and possibly dump speed later. Once you're doing that, you might as well go with the old tried and true chemical propellent that gets you up to speed much quicker.

      Ion drives are great if you're going to be going in a straight line for a very long time and don't want to stop, ever. The farther you go, the faster you go, so the less reasonable it is to slow down.

      I have even read of deep-space solar-powered mission designs that head in inside mercurys orbit, grab loads of power and then head out beyond Jupiter..

      Really? Where do they store all this power? If they used an ion drive, they would need constant power for the entire trip. Sounds a little fishy to me...

    8. Re:2011? How long with ion drives? by Rei · · Score: 2, Interesting

      What calculations are you looking for, in particular? There are a lot of them, you know ;) Here's a page that has a good number of them:

      http://members.axion.net/~enrique/rocket.html

      As for myself, there is only one problem in orbital mechanics that I have been unable to track down a solution to, which has been holding up the addition of the effects of torques (and consequently, realistic effects of RCS thrusters, control surfaces, and gimballing) to my rocket simulator:

      Does anyone know how to, given a number of forces applied in arbirary positions with arbitrary angles to an object for a given amount of time, determine the rotational and linear accelerations on the object? I've checked a number of physics texts, and none of them address this problem.

      For example, picture an object in which there is a heavy, dense ball in the middle, with a long, thin, lightweight bar passing through its center. At the end of the bar on one side, you apply a force. Due to the low moment of inertia, almost all of the energy goes into rotational acceleration instead of linear acceleration. If you were to apply the force on the center of the ball, it would all go to linear motion. So, it would seem that the further out the force is applied, the larger the percent of energy goes into rotational acceleration instead of linear acceleration. However, if you apply force to *both* ends of the bar in the same direction, *all* of the energy goes into linear acceleration.

      Does anyone know the formulae related to this?

      --
      Yes, I... I've heard good things about the mud. Lots of people talking about the mud...
    9. Re:2011? How long with ion drives? by Rei · · Score: 1

      Not for braking due to gravity assist. It'll sap energy from mercury's orbit even without a burn; burns are used to adjust the trajectory going in so that it has a proper trajectory going away.

      --
      Yes, I... I've heard good things about the mud. Lots of people talking about the mud...
    10. Re:2011? How long with ion drives? by david.given · · Score: 1
      I dont understand why solar-powered ion drives are not used on missions like this. Probes like the ESA SMART-1 has shown that such craft can be small & economical, and there is an abundance of solar power available for free.

      I suspect that as far as Messenger is concerned, it doesn't use an ion drive simply because they weren't around when the project was started --- I can't find any information on when design started, but these missions routinely take well over a decade from when the paperwork starts to when pieces start getting put together.

      Actually, for the inner solar system, you really want a light sail. No fuel! Plus, they're fast; the thrust is tiny, but it never stops... isn't there supposed to be a light sail test mission some time Real Soon Now?

    11. Re:2011? How long with ion drives? by Anonymous Coward · · Score: 0

      Does anyone know how to, given a number of forces applied in arbirary positions with arbitrary angles to an object for a given amount of time, determine the rotational and linear accelerations on the object? I've checked a number of physics texts, and none of them address this problem.

      I don't remember the details, but I saw in an old physics book a long time ago that the way this is done is to convert an off-center force into an equivalent on-center force and torque. It involved adding two additional equal-and-opposite forces, so that now there are three, such that one is on-center and the others are parallel and equidistant from the center of mass. Those two can then be converted into a torque.


      Ask the guys here. This is a forum of users of what sounds like the program you want to write. Maybe it already exists, and you don't have to write it. Anyway, this program already exists, and does simulate off-center forces.

    12. Re:2011? How long with ion drives? by edunbar93 · · Score: 2, Informative

      I dont understand why solar-powered ion drives are not used on missions like this.

      Because any spacecraft headed for planets inside earth's orbit will be falling towards the sun anyway, and thus accelerating. This makes a direct trip between Earth and Mercury very difficult because in order to acheive orbit around Mercury, you'd have to slow down a whole lot - more than a chemical rocket could produce and way, way more than an ion drive. Sending a probe on a path like this would essentially give it a stupidly long elliptical orbit around the sun or around Mercury and then the sun.

      Also, you don't seriously believe that solar panels could withstand the heat and radiation on Mercury do you? At best they'd overload and burn themselves out, although a more likely scenario would be that they'd just evaporate.

      --
      "No problem. I have the capacity to do infinite work so long as you don't mind that my quality approaches zero."-Dilbert
    13. Re:2011? How long with ion drives? by Minna+Kirai · · Score: 1

      Also, you don't seriously believe that solar panels could withstand the heat and radiation on Mercury do you?

      Uh oh! You better tell NASA quickly! The solar panels that they've just launched to inside the orbit of Mecury are gonna kersplode!

    14. Re:2011? How long with ion drives? by Minna+Kirai · · Score: 1

      I've checked a number of physics texts, and none of them address this problem.

      Get some better textbooks, maybe? (Say for example, Univeristy Physics by Young & Freedman- I don't have it, but at $150, it had better be good) Problems like that this are, to my recollection, standard material for a second semester college physics course.

      It's called "rigid body kinematics/dynamics". You start by studying spheres of uniform density, then consider objects composed of multiple such spheres locked together. That provides sufficient equations for many programmers, because they can represent the object as an approximation of many spheres.

      Or, if you know calculus, you can derive closed-form solutions to problems involving objects whose shape or density varies as a more complex function. A textbook will provide solved examples for handy things like cylinders, cones, or prisms.

    15. Re:2011? How long with ion drives? by Jowr · · Score: 0

      You need to know its' Inertia.

      Use vector analysis upon those forces. You will know the resultant force, and use that against inertia. There you go.

      --
      ~ Detonating a nuclear device within the city limits will result in a 500 dollar fine.
    16. Re:2011? How long with ion drives? by adeyadey · · Score: 2, Interesting

      Yes I remember that impulse was rated in seconds - I should have said per Kg of propellant - ie, I understand that an ion drive can generate 10x the thrust per Kg of propellant, it just does it slower..

      The SMART-1 mission cost $100 million in *total*, not too much in terms of space exploration. The thrusters will operate for 18 months & I think newer designs allow for multiple replacement anodes to replace old ones..

      Ion drive missions have spiral paths, in this case decellerating towards the sun. An ion drive mission could also exploit slingshot slowdowns, no?

      At points where the craft is nearer the sun, more power is available - lots more power..

      So, has anyone done the calculation for a mission profile with solar-ion propulsion?

      --
      "You lied to me! There is a Swansea!"
    17. Re:2011? How long with ion drives? by adeyadey · · Score: 1

      In reply to my own question - the up and coming ESA Bepicolombo mission to mercury will use.. yep.. Solar Electric Propulsion. It still uses gravity slingshots to slow down, and needs a small conventional rocket to kick it into Mars orbit.

      It will launch 2012 and take 4 years to get to Mercury, compared to 7 for messenger. Now the interesting part - how much is saved in the mission profile with ion engines? Do ion engines allow for more flexible mission launch windows? How will the propellant/mass profile compare to Messenger?

      --
      "You lied to me! There is a Swansea!"
    18. Re:2011? How long with ion drives? by Rei · · Score: 1

      > Or, if you know calculus, you can derive closed-form solutions to problems ... (etc)

      Seing as I already mentioned moments of inertia, I'm quite familiar with this already.

      > It's called rigid boxy kinematics/dynamics

      Yes, I'm aware of that. And with my searching thusfar, plus searching on the net, I've found plenty that discusses both linear acceleration of a free-floating body, and angular acceleration around a fixed center of mass. Neither of those are what I need. I'm dealing with both multiple forces applying both angular and linear acceleration on a free floating body at the same time here.

      Anata wa minna kirai ka?
      Minna suki yo. :)

      --
      Yes, I... I've heard good things about the mud. Lots of people talking about the mud...
    19. Re:2011? How long with ion drives? by Minna+Kirai · · Score: 1

      I'm dealing with both multiple forces applying both angular and linear acceleration on a free floating body at the same time here

      But... multiple forces just does the same thing as single forces... multiple times.

      Of course, in 3d, each force is likely to be acting about a different axis than the previous one, making bookkeeping of all the axes quite painful (even in software). But that's where tensor analysis comes in handy... or so the engineering students tell me.

      Have you tried Wiesel's Spaceflight Dynamics?

    20. Re:2011? How long with ion drives? by p3d0 · · Score: 1
      For interest's sake, here are some 0th-order approximations of the Hohmann transfer orbit patched-conic calculations...
      1. Low-earth orbit requires about 7.8kps
      2. Hohmann transfer from Earth to Mercury requires an apehelion delta-V of 7.5kps relative to Earth. Relative to low-Earth orbit, that becomes about 5.5kps.
      3. A circular near-Mercury orbit requires 70% of surface escape velocity (which is 4.3kps), or 3kps.
      4. The Hohmann transfer requires a perihelion delta-V of 8kps relative to Mercury. Relative to low-Mercury orbit, that becomes about 6kps.
      Adding these delta-Vs: 7.8 + 5.5 + 6 = 19.3kps. That is pretty large. (The last 6kph represents how much you need to slow down when you reach Mercury.)
      --
      Patrick Doyle
      I mod down every jackass who puts his moderation policy in his sig. Oh, wait a sec....
    21. Re:2011? How long with ion drives? by Rei · · Score: 1

      Actually, I just found an excelent paper last night when I went out net searching again, that covered it all. It explained the main issue that was concerning me (the question of "how much energy goes to angular and to linear momentum?"). The answer is "all of it, to both".

      Work is force times distance. The reason that you end up with more work being done when you push on the outer edge of an object is because you're having to apply the force across the combination of the distance that the object moves linearly, plus the distance that the object rotates away from you. It now seems so obvious, I don't know why I didn't think of it before. :)

      It also discussed a good way to represent the bookkeeping of the axes in 3d (actually, two ways), via an interesting trick in matrix math (and the quaternion equivalents). Neat stuff - it should work great. Thanks for your help anyways, though!

      --
      Yes, I... I've heard good things about the mud. Lots of people talking about the mud...
    22. Re:2011? How long with ion drives? by Cujo · · Score: 1

      It's actually very difficult designing a planetary rendezvous mission with very low thrust engine. I'm not even sure how you'd do it. Sure, you can use gravity assists in some cases (e.g. Galileo, Cassini, and now MESSENGER), but this helps a chemical propulsion mission as well, and doesn't solve the problem of how you match speeds with the planet. Even with 6 gravity assists, MESSENGER still needs high thrust delta-Vs, and substantial at that.

      --

      Helium balloons want to be free.

    23. Re:2011? How long with ion drives? by Cujo · · Score: 1
      At points where the craft is nearer the sun, more power is available - lots more power.

      When you get close to the sun, solar arrays have a certain problem - they get hot, and hot solar arrays are much less efficient. If you look at MESSENGER's solar arrays, you'll see that most of the solar array area is taken up with reflectors to keep the solar array from overheating.

      --

      Helium balloons want to be free.

  13. Mercury, messenger of the Gods? by Airw0lf · · Score: 3, Interesting

    As another poster has pointed out, officially the name is derived thus: MESSENGER stands for MErcury Surface, Space ENvironment, GEochemistry and Ranging. I was looking at this information and thought that it was a rather contrived name - kind of like the laws that the US Congress passes (PATRIOT Act, etc...) And then it occurred to me, they probably called it Messenger because in Greek mythology, Mercury was the messenger of the Gods. Or I could be completely wrong...

    1. Re:Mercury, messenger of the Gods? by Zouden · · Score: 1

      You're right. I don't know why they bother coming up with an acronym - what's wrong with simply "Messenger"? The earlier probes (Galileo, Voyager, Mariner etc) didn't need a fancy acronym. I guess there's some beaurocratic reason...

      --
      "A week in the lab saves an hour in the library"
    2. Re:Mercury, messenger of the Gods? by fuzzybunny · · Score: 2, Funny

      GALILEO--Get Awfully Lucky If it Leaves Low Earth Orbit
      VOYAGER--Vogons Observing Your Area; Get 'Em Running! (Ah, its true purpose is revealed)
      MARINER--Meet Alien Robots In Near Earth Rendez-vous

      --
      Cole's Law: Thinly sliced cabbage
    3. Re:Mercury, messenger of the Gods? by pedroloco · · Score: 1

      There's a proposed mission to the Aitken Basin in the south polar regions of the moon currently under consideration. A friend of mine who works in that group asked a number of people for suggestions of what to name the mission. One name was preemptively ruled out: South Pole Aitken Mission (SPAM)

    4. Re:Mercury, messenger of the Gods? by Anonymous Coward · · Score: 0

      HUBBLE - Hopelessly Unmaintainable Broken Baryon Leeching Engine SPIRIT - Silently Parked In Rugged Inhospitable Terrain OPPORTUNITY - .. i'm bored. you do it.

    5. Re:Mercury, messenger of the Gods? by balster+neb · · Score: 1

      Precisely my thoughts. For one thing, I have no doubt Messenger was named such because Mercury was the messenger of the Greek Gods. I've always felt that Messenger was an obvious name for a Mercury probe, so it was no surprise when I heard of this one. (Similarly, i've always thought Mercury would be a great name for an email program, instant messenger or some type of communications software, but i guess the name is too common).

      The MErcury Surface, Space ENvironment, GEochemistry and Ranging bit is obviously contrived and yes, very much like various acts (CAN-SPAM = "Controlling the Assault of Non-Solicited Pornography and Marketing")

  14. Will this joke ever grow old? by Zarhan · · Score: 3, Insightful

    Seriously, the Metric/Imperial thing happened like 1999. Since then we have had Galileo end it's mission successfully, Mars Odyssey (2001), The exploration rovers, Cassini has so far performed flawlessy, and the hard part is over (Orbit insertion), NEAR, an orbiter, landed softly on an asteroid on it's solar panels, Deep Space 1 did the comet Borrelly encounter, Stardust has successfully collected the comet material (return in 2006)..and probably others that I don't remember offhand.

    I mean, after so many successes, and some folks *still* don't let go. Now, if one of the probes were lost *again* due to a measurement system error then we could get a laugh out of it, but so far...they have not done that. Granted, in 1999 the *other* Mars probe, Polar lander was lost too, and so was Deep Space 2. But still...that's five years ago, and NASA has had loads of successes since then.

    This is kinda starting to resemble *BSD is dying trolls..

    1. Re:Will this joke ever grow old? by Anonymous Coward · · Score: 0, Funny

      BSD is dying?

    2. Re:Will this joke ever grow old? by Anonymous Coward · · Score: 0, Informative
      Will this joke ever grow old?

      I, for one, WELCOME our joke recycling overlords.

    3. Re:Will this joke ever grow old? by StalinsNotDead · · Score: 1

      Will this joke ever grow old?

      Yeah, but it'll never die. Slashdot is the old joke cryogenics facility. They come here to rest when the rest of the world has forgotten them, you insensitive clod!

      --
      Thanks to the internet, we can now all die alone together! -SomeWoman
  15. Cause this is the real world and sci-fi by Anonymous Coward · · Score: 0

    What? Ion engines? I heard theyre so fast the driver will probably die at the really high speeds... so how would the spaceship get to mercury?

  16. Re:that long? by LooseChanj · · Score: 4, Informative

    Also, remember the Earth is in orbit around the sun, so to get to the orbit of Mercury you need to lose a lot of the energy Earth's higher 'altitude' gives you to start with. Plus you need to slow down enough to where you don't need an ungodly amount of fuel to slow down into orbiting Mercury itself.

    --
    Mix the failings of Usenet with the shortcomings of the World Wide Web and the result is slashdot.
  17. So many fly by's by thbigr · · Score: 1

    I am wonder why so many fly by's. I remeber before it was increase V, but is this being used to do a gentle park around Mercury?

    --
    Come the revolution, the Bourgeois, Capitalistic, "A PARKING STICKER HOLDERS", will be first against the wall!
    1. Re:So many fly by's by Anonymous Coward · · Score: 1, Interesting

      There's no doubt that a direct flight to Mercury could have been made in theory, but it would have required a MASSIVE amount of fuel to prevent it from being sucked into the giant gravity well of the sun. There's a remarkable grace in the use of planetary fly-by's to achieve the same result much more efficiently. I actually work with the rocket scientists responsible for this planning.

    2. Re:So many fly by's by thbigr · · Score: 2, Interesting

      I am sorry I must not have phrased the question well. I do understand using a fly by to increase Velocity, but this guy is going around the sun quite few times. Mercury is inside those orbits. I am assuming it is more of a case of placement rather then speed? Right?

      --
      Come the revolution, the Bourgeois, Capitalistic, "A PARKING STICKER HOLDERS", will be first against the wall!
    3. Re:So many fly by's by Gilthalas · · Score: 3, Informative

      Actually it's a combination of *decreasing* velocity (each flyby will take speed away from the craft, causing it to have a smaller orbit) and the final position in orbit (the final orbit has to be very ellipitcal, and very near polar).

      The number of times around the sun is merely a side effect of a) the number of flybys needed and b) the fact that Messenger needs to orbit for a while before it can reach the planet needed for flyby.

      --

      Gilthalas
      Software Engineer, Space Dept, JHU/APL
      Support Space Science!
    4. Re:So many fly by's by Waffle+Iron · · Score: 2, Informative
      I do understand using a fly by to increase Velocity

      To reach Mercury orbit, you have to decrease velocity. Remember that in outer space, it's just as hard to slow down as to speed up. (Unless you find a convenient atmosphere to help you brake, which Mercury doesn't have.)

    5. Re:So many fly by's by Anonymous Coward · · Score: 1, Insightful

      The mission planners may well have some other objectives in mind. It might be nice to have data from other angles/distances and maybe some shots of Venus, as well, especially from inside it's orbit. Ultimately, though, there is simply no huge rush to collect data on Mercury, since we aren't planning on landing people there in the near future, so you might as well cut some fuel costs.

      By the way, check out the drawings of the probe. It's pretty cool looking. It's got a big radiation shield on the side it turns to the sun, and the solar panels are actually cooled. It reminds me of the research station in Homeworld

    6. Re:So many fly by's by thbigr · · Score: 1

      Ahhhh... Thank you all.

      --
      Come the revolution, the Bourgeois, Capitalistic, "A PARKING STICKER HOLDERS", will be first against the wall!
  18. Lot of activity on ion engines at NASA too by Morgaine · · Score: 4, Informative

    Why aren't ion drives used more?

    That's actually quite a good question, given the huge amount of power available from sunlight in the inner solar system. A continuous-burn trajectory to Mercury would probably be very much shorter than the current one; the thrust may be small, but craft speed builds up rapidly under such continuous acceleration. You'd only need to carry enough conventional chemical propellant for the final orbital insertion.

    NASA has been very active on the ion-engine front -- last year it successfully completed a pretty advanced test: http://www.sciencedaily.com/releases/2003/11/03112 1072826.htm. (And enter "ion engine" at NASA's main site for a huge number of links.) So, it's not only ESA that have their fingers in this pie.

    Maybe the answer is that ion engines still need a few more years of development? Certainly not long though, since small ion thrusters are already in use, as you point out.

    --
    "The question of whether machines can think is no more interesting than [] whether submarines can swim" - Dijkstra
    1. Re:Lot of activity on ion engines at NASA too by Ignignot · · Score: 1

      Maybe it is something as simple as that they designed MESSENGER years ago when ion drives were not fully tested. Once they had designed it and started construction and programming etc., they would have been required to rebuild the thing from scratch to use ion drives, possibly costing more money than saved. Or maybe this was some big shot's pet project and it just went through. In the future I expect NASA will use more ion drives but they've got something that works now, and there is no huge rush to see Mercury close up. We are used to quick changes in the software industry but for things like rocket science, I imagine they are more conservative with the application of new ideas. (Tests, more tests, always tests!)

      --
      I submitted this story last night, and it didn't get posted.
    2. Re:Lot of activity on ion engines at NASA too by Anonymous Coward · · Score: 2, Insightful

      I'm not an expert, but I suspect that the problem with Mercury is that the environment is so hostile that you want to spend all your time close to the sun doing science rather than getting into orbit. This craft is going to swing by Mercury a few times, but it also swings out again, so until final orbital insertion it is generally quite far from the planet. With an ion drive you'd slowly spiral in towards the sun from Earth, so you'd spend a lot of time near the sun but not yet at Mercury.

      You might also still need to carry some fuel for orbital insertion. As you approach the planet its gravity accelerates you. If you don't dump your velocity quickly, you'll slingshot away again. I suppose you could potentially get yourself into a really big orbit and then slowly lower it, though, so maybe you don't need the rocket, but again, a bunch more time spent lowering your orbit to something useful.

      I think the main problem, though, is that ion engines are still considered experimental. We understand rockets. If you were chief scientist on one of these once-in-a-lifetime missions which would you rather use... an ion engine, which has only been tested in space a few times, or a rocket, which we have tested dozens of times? If you were Congress funding a $400 million mission, which would you choose? Ion engines will continue to get tested on cheap, not too important missions for a long time before anyone considers using them for the important and/or expensive stuff.

  19. Stupid rockets... :) by JCMay · · Score: 2, Interesting

    We were, of course, some of the first people to know that the Messenger launch had occurred; with TS Alex to our northeast we had winds out of the north and the noise of the launch was exceptionally clear at our house. Woke me up with rattling windows and a low rumble.

  20. Service Pack Two by fuzzybunny · · Score: 1

    they could apply service packs to Mercury and give it an atmosphere.

    Except that it'd install an atmosphere which purported to keep out all future Mercury exploration missions.

    --
    Cole's Law: Thinly sliced cabbage
  21. Re:Second try? by Kiryat+Malachi · · Score: 3, Informative

    No, there isn't. The official terminology acknowledges attempts as tries, as does the English language. Do you think trying to launch starts when they hit "Go" on the main motors? It starts a lot earlier than that; launch procedure usually starts with fueling (for liquid-fueled motors). Solid rockets have much shorter launch procedures, but are generally not used for launch all by themselves (only as strap-on boosters, for the most part).

    The writeup is correct as written. 'NASA made two launch tries, and succeeded in launching on the second try'. This sentence is equivalent to 'NASA made two launch attempts, and succeeded in launching on the second attempt.' There is no difference in the two. NONE.

    And here are the common English definitions, just to drive the point home:

    Attempt - To try to perform, make, achieve.
    Try - To make an effort to do or accomplish (something); to attempt (something).

    Admit you were wrong and move on.

    --

    ---
    Mod me down, you fucking twits. Go ahead. I dare you.
    (I read with sigs off.)
  22. Re:Useful tip for the NASA engineers .... by unknowns · · Score: 2, Interesting

    It's no joke kids.

    At an AAS (American Astronomical Society) meeting two years ago,I picked up a neat little reference card from the NGST (now the James Web space telescope) booth. I still have it. There's this great image of the telescope with Ball Aerospace, Northrup Grumman, and Kodak corporate logos plastered around it. On the back was a reference table with star magnitudes, colors, etc as well as some useful distance conversions; including the distance from the earth to the sun:

    "AU - Astronomical Unit - Mean distance between the Sun and Earth: 149,599,000km. 190,236,576 miles."

    Take a good hard look. Now look again with the knowledge that there are about .62 miles per kilometer! Whoops!

    Now I'm not saying that this is an apples to apples comparison. I'm sure (I hope, for the love of god) that they do a few more checks on a spacecraft propulsion system than a cheap promo. But still!

    --
    Even blind squirrels find nuts now and then.
  23. 7.9 billion km by underpar · · Score: 1

    Mercury is at most 222 hundred thousand kilometers from earth. Messenger is traveling 7.9 billion km.

    I know that there is no other good way to get it there, but I just find that interesting. I hope it has something good to read on the trip.

    1. Re:7.9 billion km by Somegeek · · Score: 1
      222 hundred thousand?

      Its 222 MILLION km for the maximum, if you insist on counting in hundred thousands, you need 2220 of them, not 222.

      --
      And as you tread the halls of sanity, You feel so glad to be, Unable to go beyond. I have a message, From another time..
    2. Re:7.9 billion km by Chuck1318 · · Score: 1

      Reporters always seem to make a big deal about the total distance, but it just comes from the fact that Messenger will be in orbit around the sun for a long time as it uses the occasional planetary swingby to adjust its orbit. In the six-and-a-half years until Messenger begins orbiting Mercury, the Earth will have travelled 6.1 billion miles in its orbit, and Mercury will have travelled 9.8 billion miles in its orbit. Since Messenger's orbital speed will be changing gradually from one to the other, naturally the total distance will be between the distances the planets travel also.

  24. Eh, I have karma to burn... by BTWR · · Score: 2, Insightful
    just mentioning all those sucesses, along with the huge ESA failure* of Beagle 2 usually shuts them up.

    *and you know you got them angry when they start whining/defending "but Beagle2 was England, not ESA!" - basically admitting it was a collossal failure but trying to shift blame elsewhere (and then throwing in a US-bashing joke for good measure).

    1. Re:Eh, I have karma to burn... by Anonymous Coward · · Score: 0

      Don't forget the software failure on the first Ariane 5 ! Especially if any mention is made of something going up on an Ariane, you know what to do...

  25. Millions! That's right! by underpar · · Score: 1

    TY

    I really shouldn't try to do math before coffee. It all started when I was converting miles to kilometers.... On the bright side.. it's correct on my website.

    Do I get brownie points for recognizing that 7.9 billion is a bigger number? That's about the best I've done today.

  26. Solar Flare strike by random+coward · · Score: 2, Interesting

    When is next solar max? What are the odds of a solar
    flare hitting it before it orbits mercury? What ar ethe odds of a solar
    Flare hitting it early on in its orbit of mercury? Isn't mercury struck by solar flares
    from time to time?

  27. 15-month ion mission to Earth's Moon by peter303 · · Score: 1

    Last September the European SMART probe was launched to the Earth's Moon. It will take 15 months to arrive there by ion drive. Manned lunar missions took three days by chemical propellant.

    1. Re:15-month ion mission to Earth's Moon by adeyadey · · Score: 1

      SMART-1 was primarily a test-bed for lots of new technologies, including ion propulsion. Going to the moon was almost a bonus - the main objective was to see if it was possible to make very small, cheap missions ($100 million, I think). It was piggy backed (cheaply) onto an existing satellite launch, hence having the minimal boost needed to get to Low Earth Orbit.. If you used a bigger rocket (smaller than Apollo) it could get there in 3 days too.

      For a bigger mission like Mercury, as you can see, it is much harder to get there quickly by chemical rocket - hence the "long burning" ion drive comes into its own..

      --
      "You lied to me! There is a Swansea!"
  28. Re:that long? by LooseChanj · · Score: 2, Informative

    http://messenger.jhuapl.edu/faq/faq_journey.html#5

    --
    Mix the failings of Usenet with the shortcomings of the World Wide Web and the result is slashdot.
  29. Re:Millions! That's right! by snake_dad · · Score: 1
    Do I get brownie points for recognizing that 7.9 billion is a bigger number? That's about the best I've done today.

    I would consider that under par for the avarage /. poster, especially on space articles.

    --
    karma capped .sig seeking available Slashdot poster for long-term relationship.
  30. Re:that long? by snake_dad · · Score: 1

    The faq briefly mentions cost as an issue. MESSENGER is a member of NASA's Discovery Program of lower cost, highly focused missions. Adding a lot of fuel would not be too expensive by itself, but then a lot bigger (and more expensive) launch vehicle would be needed, and that would be outside the scope of the Discovery Program. That is the explanation that was given on some other website, sorry, no link.

    --
    karma capped .sig seeking available Slashdot poster for long-term relationship.
  31. Gets there in 2008 actually by DumbSwede · · Score: 3, Informative
    2008 actually
    after having gone by Earth on a flyby (2005?)
    and by Venus twice on flybys (2007, 2008)
    See this link Mercury

    After a flyby of Mars in 2008, and another in 2009, it settles down for orbit in 2011.

    That last long ago (30 years) visit was only a flyby.

    So all that confusion is about getting the right orbital velocity to stay, plus we get good science all along the way.

  32. Well... it's comparable with the release schedule by leonbrooks · · Score: 1

    of MS-Windows 95 AKA Project Chicago. Does that count for anything?

    --
    Got time? Spend some of it coding or testing
  33. s/Mars orbit/Mercury orbit/ (no text) by leonbrooks · · Score: 1

    really no text

    --
    Got time? Spend some of it coding or testing
  34. Re:Useful tip for the NASA engineers .... by cjameshuff · · Score: 1

    190,236,576 miles is just barely over 2AU...I wonder if someone mistook the major diameter of Earth's orbit for its mean radius. Still a stupid error...if they didn't make an extreme conversion error, they completely screwed up the definition of the unit.