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Space Mars

Six Minutes of Terror - Landing Humans on Mars 410

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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Six Minutes of Terror - Landing Humans on Mars

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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) 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?
           
  • 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 ...
    • Re:Impact (Score:5, Funny)

      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: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!

  • 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 TimmyDee ( 713324 ) on Thursday July 19, 2007 @05:36PM (#19920465) Homepage Journal
      "The Hypercone is bigger and costs more."

      --Vorticity Ltd.
    • IANAE, but I think that the issue is pretty obvious. I am guessing that they want the craft to take a direct landing rather than burning up some speed in the outer atmosphere. With a parachute as soon as you open it, it takes ALL of the stress up front. IOW, you just hit your brakes in full. It is possible (and in fact probable) that you will rip the chute. With the hypercone, it will be folded up on itself. You will get less drag on the "chute", but sufficient to start a slow "slowing". As the speeds, the
    • by DeeVeeAnt ( 1002953 ) on Thursday July 19, 2007 @05:47PM (#19920617)
      Actually the difference is that a parachute would instantly shred at the supersonic speeds they are talking about. It needs a clever shape and tougher materials. They will probably need to make it out of unobtainium.
    • Some care to elaborate on the difference between this and a parachute?

      When I first saw the "hypercone" I just figured they played a lot of badminton. Squash a shuttlecock, show it to marketing, and Presto, you have a "hypercone"...
    • by ArsonSmith ( 13997 ) on Friday July 20, 2007 @02:14AM (#19923975) Journal
      I didn't read the article or anything but from what I gather this will work while a parachute wont.

  • by theurge14 ( 820596 ) on Thursday July 19, 2007 @05:32PM (#19920429)
    Just extend the space ladder from Earth to Mars.
  • 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?
    • Condom? (Score:2, Funny)

      by Anonymous Coward
      Care to explain what a condom is to the rest of us /. geeks?
  • 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)

      by bhmit1 ( 2270 )
      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?
    • Would a space elevator be more feasible on Mars with the reduced gravity and atmosphere? Yes, unfortunately Mars also has two moons with orbits that intersect the equatorial plane. Thus this means you would either have to keep the space elevator mobile ( maybe along some track on the surface ) or you would have to shift the orbit of a 22km diameter rock. Taking care of the moon the old fashion American way unfortunately won't work as the amount of scrap that would be flying around in the orbit would becom

    • The counterweight doesn't necessarily need to be a problem. A robotic ship with ion engines could probably retrieve an asteroid from the "nearby" belt to use as a counterweight. The logical course of action to reliably placing humans on Mars, would be to start with a lunar base on Deimos or Phobos (maybe both to ensure that control could be maintained while one or the other is out of radio contact, although satellites could work for that purpose as well). From there you can have robots construct a space
    • Re: (Score:3, Informative)

      by fjf33 ( 890896 )
      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.
  • Look, if it is possible to take a craft like the armadillo to Earth's LEO and back, then it will be easy enough to do the same at Mars. And yes, it is in a moon style approach. Of course, it might be better to have a better fail safe approach to it, such as the hypercone.
  • 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.
    • I suspect that the lines in the parachute would be vaporized upon entry. The cone provides a heat-shield type environment that is reasonably stable until the velocity drops to a reasonable level.

      Personally, I think this is a waste of money and time. Use probes. Why do we want to drop down a gravity well anyway? If we are going into space, go for the smaller bodies (asteroids / pseudo-comets, etc). The energetics for the earth crossing asteroids are definitely favorable and they have available mass that ca

    • 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"
    • by MikeFM ( 12491 )
      Why not split off the humans from their supplies and land in two stages? Land the supplies using some mix of the before-mentioned possibilities (rockets, chutes, and airbags) and the humans on their own. The article made it sound as if small craft might land with chutes without to hard a landing. As for the supplies - well as long as they survive the landing they don't have to be let down near as carefully as the people.

      I just find it hard to believe that among all the so called intelligent beings from Eart
    • Re: (Score:3, Interesting)

      by einhverfr ( 238914 )
      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.
    • Re: (Score:3, Interesting)

      by khallow ( 566160 )

      Overall, Mars is the hardest place to land in the inner solar system.

      Hard I suppose is relative, but as I understand it Mercury, Venus, and the Moon all require more delta V to get there once you take into account the advantages of atmospheric braking. More delta V means "harder" for me.

      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 pr

    • 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 Anonymous Coward
      Redundant Array of Inexpensive Astronauts
  • 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.

    • Re: (Score:3, Insightful)

      by R3d M3rcury ( 871886 )

      [...] 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.

      That's always the question I have. Do Probes do a "better job"?

      Now, I'll admit I disagree with your opinion on sending people to Mars. But I agree with the basic tenets about the expenses involved--probes are definitely easier and cheaper. The question I always have is--do you get better science when you send scientists versus sending probes?

      I'm not sure that question has ever been explored. Do we know more about the Moon than the Soviet Union because we sent astronauts versus robotic probes? I know w

  • by sehlat ( 180760 )
    all these worlds are yours
    except mars
    attempt no landing there
  • This is how JPL intends to land the next rover, Mars Science Laboratory: http://video.google.com/videoplay?docid=1404791803 599052711 [google.com].
  • by six11 ( 579 ) <<ude.umc> <ta> <ggosnhoj>> 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.
  • All these ideas seem to assume a heavy lander is necessary. Pack 4 of everything since you want backups anyway. Break up all the parts of the habitation module and such into separate small pieces that break up from each other just when the atmosphere is encountered so they land in roughly the same area using already proven landing mechanisms. Assemble them with the humans still in orbit using proven rovers, robotics, and UAV technology (and with local humans, minimal time delay). Make sure environmental con
  • ...for OBVIOUS reasons? This is not so obvious to me. It will obviously feel kind of funky, but some of the amusement park rides out there are pretty brutal already. Now, I know you can't just drop them like pathfinder, but the last two rovers were quite big and complex, and NASA didn't exactly want them bouncing around all over Mars -- I'm not at all convinced humans couldn't survive that, especially in combination with a partially powered descent and parachutes. At the least we should be able to model thi
    • Re: (Score:3, Funny)

      by MoodyLoner ( 76734 )

      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?
  • 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.
  • Won't ever happen (Score:2, Insightful)

    by texwtf ( 558874 )
    The original moon missions involved _enormous_ rockets. Even if you could land on Mars what is the likelihood you would be able to transport rockets big enough to get you back off there?

    Oh yeah, and have it work after being dropped from outer space.

    Maybe if they used nuclear power to lessen the wight somehow, it _might_ be possible. Otherwise it's just a long one way trip with a slow cold end.
    • Re: (Score:3, Informative)

      by VENONA ( 902751 )
      Read Zubrin's _The Case for Mars_, which goes into quite a lot of detail. It covers cancer risks, etc. It *doesn't* cover the landing issue, beyond assuming aerobraking.

      The basic scheme is to send an atmosphere converter ahead of the manned mission to create a stock of methane and oxygen propellants for the return, as most of the mass you'll need is still fuel. Mars has a surface gravity around 1/3 of Earth's, so quantities required are much lower than for the trip out. In a way, you're right about using nu
  • Why can't air bags be used? If the balloon bags that the last probes bounced around and landed with, were okay for all the sensitive equipment aboard, would they not be okay for humans? Or did those landers still take one hell of a beating, and were just tough enough to stand it? Anyone know the impact forces the gear sustained?
  • I'm sure they laugh at our measly doughnuts.
  • 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[ ].com ['ail' in gap]> 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.
  • What about Venus? (Score:3, Interesting)

    by Door-opening Fascist ( 534466 ) <skylar@cs.earlham.edu> on Thursday July 19, 2007 @09:08PM (#19922313) Homepage
    I've always thought that floating cities on Venus [wikipedia.org] would be pretty cool. You wouldn't need to break that much, because at 50km up the atmosphere is already as dense as it is on Earth at sea level.

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