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Six Minutes of Terror - Landing Humans on Mars

Posted by Zonk on Thu Jul 19, 2007 05:22 PM
from the our-red-buddy dept.
OriginalArlen writes "Universe Today has a fascinating article discussing the difficulty of executing EDL (entry, descent, landing) on Mars for vehicles bigger than MER, Viking and Pathfinder, and the challenges for manned craft in particular. Airbags can't be used for obvious reasons, but the atmosphere is too thin to be used for parachutes or aerobraking by large heavy vehicles. The stronger gravity (compared to the moon) makes an Apollo-style powered descent impossible. The best current idea is a huge inflatable torus called a hypercone: 'Imagine a huge donut with a skin across its surface that girdles the vehicle and inflates very quickly with gas rockets (like air bags) to create a conical shape. This would inflate about 10 kilometers above the ground while the vehicle is traveling at Mach 4 or 5, after peak heating. The Hypercone would act as an aerodynamic anchor to slow the vehicle to Mach 1.'"
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  • Why land? (Score:5, Funny)

    by Ecuador (740021) on Thursday July 19 2007, @05:26PM (#19920363) Homepage
    We don't really have to land the large vehicle. Getting within transporter range should be enough.
    Oh, wait...
    • by Tablizer (95088) on Friday July 20 2007, @12:06AM (#19923407) Homepage Journal
      We don't really have to land the large vehicle. Getting within transporter range should be enough. Oh, wait...

      Were you talking into your mouse when you said that?
           
      • by Glonoinha (587375) on Thursday July 19 2007, @06:46PM (#19921165) Journal
        Bunch of NASA whiners must have replaced 'The Right Stuff' through worthless politically correct hiring practices - this new generation of 'engineers' and 'rocket scientists' have forgotten history and thus are being forced to re-invent the wheel. The logistics of these landings were worked out years ago - as you can plainly see in this simulation [frontiernet.net].
  • Impact (Score:5, Funny)

    by eck011219 (851729) on Thursday July 19 2007, @05:27PM (#19920365)
    Landing at mach one still sounds pretty fast -- better aim for water! Oh, wait ...
    • Landing at mach one still sounds pretty fast -- better aim for water!

      Don't worry! We'll just tell Quaid to start the reactor [wikipedia.org]. Oh, wait...
      • Re:Impact (Score:5, Funny)

        by HTTP Error 403 403.9 (628865) on Thursday July 19 2007, @06:21PM (#19920873)
        Don't worry! My method will get them down in one piece. You wanted them alive? Oh, wait...
          • Re:Impact (Score:4, Interesting)

            by stuktongue (140376) <adam...grenberg@@@gmail...com> on Thursday July 19 2007, @10:53PM (#19922987)
            You bring up an interesting idea.

            This is where design validation comes in. For those not familiar with this term in the context of system engineering (and, in particular, system engineering of complex aerospace/defense systems), design validation generally refers to the activity whose purpose is to show that a design actually meets the customer's needs (i.e., that it is a 'valid' design). The effort takes design requirements into consideration, of course, but should also make use of system modelling based on the design, among other inputs.

            Assuming the statement of work includes support for design validation, and the team doing the validation is competent, a lot of the risk of incomplete requirements can be mitigated, at least in theory. However, the engineering of complex, never-been-done-before systems always has associated 'escape' risks. A lot will depend on how the development effort is phased, and whether or not sufficient system engineering is performed up front, with sufficient lead time to modify/add to the design without severely negatively affecting the overall development in terms of cost or schedule.

            In the end, of course, dealing with a competent and ethical development group is key. In my opinion, the contracts folks shouldn't "get in the way" of doing the right thing if problems surface. But in today's world, with today's financial sensitivities--and today's ethics--there are risks.
    • Re:Impact (Score:5, Insightful)

      by iknownuttin (1099999) on Thursday July 19 2007, @05:43PM (#19920571)
      Landing at mach one still sounds pretty fast -- better aim for water! Oh, wait ...

      LOL. I was once in Aruba and I rented a one of those Ski-doo things. I revved the fucker up to 55 and went off. Then I made a turn. Well, G-Forces took over and I went flying across the ocean. Now, you'd think water was soft (I know YOU don't because of your post, but others...), but when I hit it, it felt HARD. So, I went again, and did the same thing...well, look at my user name...duh! (I live up to it, man!)Oh, the water was still fucking hard at 50+ MPH!

      • Re: (Score:3, Informative)

        by Anonymous Coward
        I think the GP was probably referring to the scarcity of water on Mars rather than its hardness, but could be wrong...
  • Parachute? (Score:5, Insightful)

    by MankyD (567984) on Thursday July 19 2007, @05:28PM (#19920387) Homepage

    The Hypercone would act as an aerodynamic anchor to slow the vehicle to Mach 1.'"
    Some care to elaborate on the difference between this and a parachute?
  • by theurge14 (820596) on Thursday July 19 2007, @05:32PM (#19920429)
    Just extend the space ladder from Earth to Mars.
    • Re:Space ladder? (Score:4, Interesting)

      by BlueParrot (965239) on Thursday July 19 2007, @05:50PM (#19920649)
      A space elevator would actually not be such a bad idea. You can deploy it from orbit, and since Mars has a lower mass than earth it would significantly reduce the requirements of the cable. Getting the damned thing there might be a bit difficult thou.
  • by Change (101897) on Thursday July 19 2007, @05:32PM (#19920433)
    Dunno about the rest of you, but the Hypercone immediately reminded me of a rolled-up condom.

    I wonder when that idea...uh...arose?
  • Space Elevator? (Score:5, Interesting)

    by bhmit1 (2270) on Thursday July 19 2007, @05:35PM (#19920459) Homepage
    Would a space elevator be more feasible on Mars with the reduced gravity and atmosphere? Admittedly, you have to find a way to get a counterweight and cable all the way there, but it may be worth the tradeoff of the high speed landing with airbags, parachutes, rockets, and everything else we lug there to make it a slow crash. And surely rockets would be more useful than they say, otherwise, there's no way to get back off the planet.
    • Re: (Score:3, Interesting)

      There's also something to be said for splitting up the payload. Food and equipment can be sent ahead of time and land much faster than people need to. All the people need is a lightweight lander and some way to travel to the other equipment. Why are they determined to send it in one large complicated package?
    • Re: (Score:3, Informative)

      It has been mentioned before in both SF and Scientific Literature. It is easier because you have Olympus Mons which takes you WAAAAY up so that you avoid most/all of the little atmosphere that is there. The gravity is obviously less which helps a lot. The problem of the moon getting close to the tether was avoided by sending elevators up and down at calculated intervals to set up a resonance motion therefore making the cable undulate like a string, therefore avoiding the moon altogether.
  • Mach 3 Chute (Score:5, Informative)

    by Nyeerrmm (940927) on Thursday July 19 2007, @05:40PM (#19920529)
    I did a project on this about a year and a half ago, and the solution we came to was in fact a parachute, but one capable of opening at Mach 2 or 3, similar to what Viking used. Unfortunately, since this has little use on Earth it is a very costly development process, and anything larger than Viking is significantly different, and a higher velocity opening speed would be nice. Following this a normal parachute, retro rockets, airbags or combinations thereof are still necessary.

    Also, the problem with a retro rocket the whole way isnt just that its heavier gravity (just means more fuel,) but also the process of igniting a rocket with an incident airflow of mach 3 or higher is not a trivial problem.

    Overall, Mars is the hardest place to land in the inner solar system. the Moon and Mercury are small and have no atmosphere, so Apollo is an obvious and easy choice. Venus has an atmosphere so thick you can drop any funny shaped item in and it will drop to the surface at low speeds, assuming the static heat doesnt destroy it. Earth, obviously, you can do well enough if you're careful with the shape and throw up some parachutes at the end. Mars though has such a thin atmosphere it makes everthing hard.

    This concept sure looks interesting though.
    • Re:Mach 3 Chute (Score:4, Insightful)

      by Lumpy (12016) on Thursday July 19 2007, @06:09PM (#19920799) Homepage
      A chute opening at Mach 7 on mars is very different to a chute opening at Mach 7 here on earth. the atmospheric density is so much lower that it would be very feasable.

      They already have designs that work, simply triple them up. They are also going to haveto do a powered decent no matter what, you are not going to get a plane to get any bite in that atmosphere at all (although a delta wing would be able to do breaking maneuvers lust like the shuttle does so it might not be a bad idea.)

      Honestly they will have to send a robotic test mission like they did with apollo unless they are willing to accept a "oops" moment as we hear the news that 7 astronauts plummeted to their death because someone divided by zero.

      The support ship will have to be huge, and the dry run with the support ship is not only a great idea, but will also tell us if the astronauts will get there with only one left and all the rest for some reason went for a walk and will be "back real soon now"
    • Re: (Score:3, Interesting)

      I had two solutions after reading the article. Both of which require rethinking the design of the CEV a bit.

      The real challenge is that no matter what you do, you are moving *fast* at the beginning of the entry to the Martian atmosphere.

      1) Very Large Heat Shields. The primary challenge to this is that it is next to impossible to launch them from earth. So don't launch them from earth-- assemble in earth orbit instead. This would require switching to more established systems after reaching mach 1.

      2) Ver
    • by iamlucky13 (795185) on Thursday July 19 2007, @07:54PM (#19921793)
      You're going to have a lot harder time landing on a body with no surface (or at least it's so deep we don't know where it becomes solid).

      I'm a little bothered that the article dismisses as useless components that in actuality will probably be used for landing on Mars and are unrelated to the problem addressed in the article, and it tends to treat each idea as a complete solution, rather than pieces of a multistate solution.

      The problem is not touching down on the surface. It's that first bit of decelleration during which you cover most of the distance to the ground. You've got to bleed off a lot of speed really fast, and Mars atmosphere isn't very conducive to accomplishing that. The article does cover this part well.

      Previous landers, especially the Mars Exploration Rovers, have used multiple stages. The first is the heat shield. Because of their small size, the MER's have a high surface area/mass ratio. The heat shield slowed them down to mach 2 and a supersonic parachute deploys. Then retrorockets fired, slowing it to a complete stop a little ways above the ground, and lastly, the cable cut, dropping it relatively gingerly onto the airbags.

      So just for the little MER's, there were actually 4 stages involved: heat shield, parachute, retro-rockets, and airbags. Although the article on focus on the airbags in its discussion of the MER, those were really only to allow a margin of error for the retrorockets (although a needed one), and were unrelated to the supersonic transition part.

      The hypercone is basically a specially-shaped parachute, but it still won't slow a lander sufficiently to survive hitting the ground. I'm expecting the final solution if we ever commit to it will include heat shield, hypersonic chute, possible a middle stage chute, main chute, retrorockets, and airbags.

      Also, you mention lighting a rocket in a supersonic airstream is hard (I'm not sure about that...the combustion chamber is static), and the article claims it would be better if Mars had no atmosphere. Regardless, if you're committing to rockets for anything more than what a modestly sized parachute leaves you travelling, then it doesn't much matter if you use the rockets down near the ground, or as part of a longer de-orbit burn. Either way you're getting rid of KE.
    • by king-manic (409855) on Thursday July 19 2007, @08:36PM (#19922093)
      Overall, Mars is the hardest place to land in the inner solar system

      I think the sun presents a greater issue.
  • by rleibman (622895) on Thursday July 19 2007, @05:40PM (#19920531) Homepage
    If the problem is that you can't land the whole crew at once because of weight... why don't you land each member separately, in tiny containers and then a big load with the unmanned portion of the mission? Another advantage of something like this is that if one of the landings fails and you lose a team member your mission is still safe.
  • by Rosco P. Coltrane (209368) on Thursday July 19 2007, @05:41PM (#19920533)
    Do we really need to land heavy stuff on Mars? "Something heavy" here means some spacecraft with human creature comfort (you know, a hull, life support systems, etc... in order to keep wetware inside alive). However, there is no need for manned flight to other planets anymore: probes do a much better job more easily, at a fraction of the cost, and a probe's survivability is much less of an issue.

    Probes are an extension of humanity's collective intelligence, and they bring back to humanity at least as much data as a real, flesh and bone human. So why send humans at all? Of course, if we're talking about colonizing Mars for good, there's some terraforming to do, but heavy machinery isn't necessarily required for that either, and it's not going to start within our lifetime anyway, and the planet won't be ready for us in 200 years minimum anyway.

    I say forget about hauling big stuff over to Mars. The only folks who care are prez Bush, for demagogic purposes, and people who think watching a Neil Armstrong type character utter some silly piece of wisdom when setting foot on a planet is the pinnacle of human space exploration. What we need is more research into nanotechnology, so probes get smaller and lighter, and educating people.

    • by khallow (566160) on Thursday July 19 2007, @07:28PM (#19921555)

      Do we really need to land heavy stuff on Mars? "Something heavy" here means some spacecraft with human creature comfort (you know, a hull, life support systems, etc... in order to keep wetware inside alive). However, there is no need for manned flight to other planets anymore: probes do a much better job more easily, at a fraction of the cost, and a probe's survivability is much less of an issue.

      Probes don't do a better job of colonizing other planets. Terraforming Mars is only a step in its colonization. The first and most important step is having people live on Mars. Second, there are all sorts of unpleasant things that can happen to people on Earth. In addition to the small chances of extinction, I think there's a good chance that we reset civilization in the next century or two. Aggressive space colonization can get us a foothold in space before nuclear war, a biological weapon, or other human-made disaster can set back Earth-side civilization to the early industrial age or earlier. Alternately, we could face centuries or millenia of stagnation in a "water empire" [wikipedia.org] style government. In other words, colonizing space, particular the Moon, Mars, and other select bodies is a great way to diversify the habitat of human life.

      We could wait for the next big technology advance like nanotech, or we could get started with the capabilities we currently have rather than count on the uncertain future to do our work for us.

      Another point is that we can expand our economy into space. Sure you can expand it profitably into deep ocean, Antartica, etc. No reason not too unless you're an environmental type in which case you should like the absence of an environment to harm in space. But space has the benefit that there's a lot more of it with a lot of energy and mass available, dwarfing anything available on Earth. Economic expansion past a certain point will require a presence in space.

  • by six11 (579) <johnsogg@c m u .edu> on Thursday July 19 2007, @05:44PM (#19920591) Homepage
    Perhaps I am inclined to think things like this because everybody around me has an infection for which the only antidote is "robots", but... Robots!

    We should send a massive fleet of robots down and they can build a runway of some sort. Once they've finished that, they can also build a little village complete with a bar. That way when people go to mars, they have a place to land, and then they can get a drink and maybe some munchies.
  • by ookabooka (731013) on Thursday July 19 2007, @05:52PM (#19920661)

    The Hypercone would act as an aerodynamic anchor to slow the vehicle to Mach 1.'"

    So. . a parachute then?

    On a serious note, why not use a parachute? They've been used before on many missions to mars to slow the vehicle down before the retrorockets fired. I mean I understand the hypercone would work too, but I dont understand why a larger and/or more parachutes wouldn't. Then again I'm no fluidynamicist (is that a word because it sounds really really cool).
  • One word. (Score:3, Interesting)

    by Fantom42 (174630) on Thursday July 19 2007, @06:00PM (#19920735)
    Nuclear.
  • Unit conversion (Score:5, Interesting)

    by jimmux (1096839) on Thursday July 19 2007, @06:20PM (#19920871)
    I suspect mach 1 on Mars is not the same as mach 1 on Earth (due to different speeds of sound in the planet's respective atmospheres). Which are they actually refering to in this case?
  • by monopole (44023) on Thursday July 19 2007, @06:40PM (#19921087)
    As the astronauts consider if the calculations were made in metric or imperial units.
  • by stmfreak (230369) <stmfreak@gm a i l .com> on Thursday July 19 2007, @06:47PM (#19921169) Journal
    We should focus on establishing a presence in space first. Let's get space working for lots of people, not just a select three at a time (plus celebrity). Think asteroid mining. Collecting hydrogen from the solar wind. Solar power arrays beaming clean energy back to Earth. Once we have refueling and industrial capacity in orbit or on platforms around the solar system, conquering the gravity wells of the other planets will merely be costly.
  • by slickwillie (34689) on Thursday July 19 2007, @07:13PM (#19921419)
    I thought it was going to be a story about my sex life.
    • Re:Make up your mind (Score:5, Informative)

      by tulmad (25666) on Thursday July 19 2007, @05:42PM (#19920557)
      The current landing setup (the one used on the rovers) involves inflating airbags around the lander, then bouncing the lander into the surface at high speeds, then eventually coming to a stop after a few bounces. This is fine when your lander is filled with robotics, but would obviously be bad when the lander is filled with people.

      The landing setup they're proposing is actually more like an air-braking system. It inflates around the lander while it's still at a high enough altitude, giving the lander a considerably larger volume. This would hopefully slow the lander as it continues its descent.
          • Re:Make up your mind (Score:5, Informative)

            by halcyon1234 (834388) on Thursday July 19 2007, @06:55PM (#19921245) Journal
            Even if the atmosphere isn't as thick, it's still an atmosphere. Mach 4 is 1361.1 m/s. The escape velocity of Mars is 5.027 km/s. If you enter at Mach 4, you have nowhere to go but down. Deploy a large enough glider, and you will glide. Since the atmosphere isn't a vacuum, there will be drag. Fly around long enough, and you will slow down enough to glide safely in. I'd rather spend a few hours circling the runway than six seconds ramming into it.
    • Obviously we need to go to Mars to fight Al Qaeda. Duh. It is part of the "war on financial sanity" that Bush is waging.
    • by BlueParrot (965239) on Thursday July 19 2007, @05:43PM (#19920587)
      The main problem with landing is that you pick up quite a bit of speed from falling towards the planet. On Earth we take advantage of the air resistance in a relatively thick atmosphere to slow down the space shuttle as it returns. Mars has a MUCH thinner atmosphere so for large objects this won't work. You either end up going in at such a flat angle that you just bounce straight off the atmsophere like a skipping stone, or you go in too steep so that you are unable to lose enough speed before hitting the surface. It is possible to land on objects with no atmosphere ( like the moon ) using retro-rockets to slow down your descent, but because mars has a much stronger gravity this becomes impractical.
    • "There is no real reason to send a manned flight to Mars. None."
      wrong. More in a moment.

      "You would need to send enormous amounts of gear, several hundred tons of water
      and food and air enough for the journey, the time spent on the planet and
      the trip back. "

      and

      "You would need a "mother ship" and at least two 'landers' with return
      capability. In addition, a habitat for the humans. If you think you are a
      treehugger, imagine the colossal amounts of resources needed to get there
      and the environmental impact on Earth, just to start this type of endeavor."

      Because it's hard is why it should be done.

      "Think people. That grey matter is supposed to be used."
      You first. I mean really.
      Now back to the first part...Why?

      1) The resulting spin off products will create new spin off companies.(The taxes returned from the companies that sold products created from the Apollo missions had gotten 13 time the return in taxes then the Apollo cost.)

      2) New technologies and RnD help drive science.

      3) This would almost certianly be a global project. Big Global Projects can help bring people together.

      4) The environmental research and technology would help us develop a better understanding of enviromental controls on earth.

      5) So we can stick out our just chest and say "Been there, where to next?" Not to consider the emotional impact on people is foolish.

      6) More experience with space flight is another step towards off world mining and colonies.

      Yes, there should be robotic exploration as well.

      Personal, I would send drop ships to drop supplies before humans left for mars. Complete satellite arrays, rover to scout out select landing zones. Maybe even send the returning vessel ahead. Pack it with what they will need to return, and nudge it to mars. No rush, you can send it a couple of years ahead of time. You could also send some different landing tests.
    • It will obviously feel kind of funky, but some of the amusement park rides out there are pretty brutal already.
      Twenty gees.
      What amusement parks do you go to?