You are not logged in.

Announcement

Announcement: This forum is accepting new registrations via email. Please see Recruiting Topic for additional information. Write newmarsmember[at_symbol]gmail.com.
  1. Index
  2. » Search
  3. » Posts by Void

#8626 Re: Human missions » SLS Rocket + Orion + Apollo LEM » 2015-03-07 15:15:43

OK, I will try to stick to the original notion and it's mirror (Why not to), and look for a mixture of the two to extend potentials.

The LEM was to get them down and to house them.  If it could be supposed that housing is already established, then the LEM can be slimmed down, but you would want an abort method, abort back to orbit in that case.  Abort being done if you could not land safely or could not land where the habitat was.

With that notion, then I would think of a spacesuit as the life support capsule, and the lander being a booster for that, and also of course the means to land and still be alive.  At first I thought that you would want a two person lander, since if one person became unable to operate the controls, then the co-pilot could.  But with the age of computers being so much more advanced than it was for Apollo, then a one person lander can have three robotic pilots to help out if not able to do the deed.

As for the lack of ability for the Orion, the vehicle, it seems to me that it would be a relatively simple matter to hire SpaceX to send a augmentation booster into LEO, to couple with the device and extend it's abilities.

As for Orion, the pulsed propulsion device, I would think it might be smart to cut it's teeth on chemical explosives first to demonstrate method, and to wait until nuclear methods were available.  It is likely that nuclear materials from Earth will not be available since it is wanted for use in power plants, and of course there are balance of power issues involved.  I am not sure when nuclear weapons in orbit might be tolerated.  Not now I think.

And so if you are going to do a chemical Orion, then it becomes silly to bring the explosives up from Earth, when rockets are developed with great power. 

So, to expand the implementation of a chemical Orion, it will be necessary to loose the restrictions on thought.  Can't get chemical explosive materials from the Moon, unless you first have the Chicken or the Egg.

#8627 Re: Life on Mars » Past and Present life on Mars » 2015-03-07 11:05:54

I more or less agree with you.  Many of the models for what was are based for lack of information on what is.

A thicker, and maybe more different atmosphere is reasonable.  Some of the asteroids in the asteroid belt still have ice and from time to time behave like comets.  Perhaps billions of years ago, they also had CO2 and Ammonia.  Then if they impacted Earth or Mars, they could contribute to a greater greenhouse effect.  To explain certain geology on Mars, such a situation would only have to exist for 25% or less of the existence of Mars.

And volcanism is presumed to be more active.  That is a double edged sword for Mars though because it is possible that super volcano's might eject atmosphere?  Then again impactors can add atmosphere or splash it away for a world like Mars.  There are a lot of variables.  And it may be true that earlier Mars had more atmospheric components to eject from volcano's than now.

But if the asteroids/comets had more CO2 and Ammonia, then it seems reasonable that they would also be likely to have had more water ice.
So, possibly Mars received quite a lot of water relative to Earth, as it is closer to the reservoir.

But it won't break my heart if facts intrude on my speculation.  I don't make a living this way.

#8628 Re: Human missions » SLS Rocket + Orion + Apollo LEM » 2015-03-07 10:53:57

If you will pardon a continued intrusion...
Argon, Radon on the Moon.  I will continue with Argon.
http://www.lunarpedia.org/index.php?title=Argon
http://sservi.nasa.gov/articles/ladee-p … st-update/

The third lunar noble gas is argon, specifically, argon-40. This isotope comes from the decay of naturally occurring radioactive potassium-40, found in the rocks of all the terrestrial planets as a leftover from formation. As potassium-40 in the moon decays, the argon-40 product is able to diffuse and percolate up to the lunar surface, where it becomes part of the tenuous atmosphere. Lunar argon behaves differently from helium and neon; it condenses on the moon’s cold nightside where temperatures drop below -280 degrees Fahrenheit (-173 Celsius). As the moon slowly rotates, and the condensed argon sees sunrise, temperatures rise and the atoms jump off the surface into the exosphere again. Some of these jumping argon atoms leap back into the cold nightside, and are re-trapped on the cold surface until sunrise occurs for that patch of real estate. But the moon’s argon exhibits other interesting behavior. LADEE discovered that argon-40 creates a local bulge above an unusual part of the moon’s surface, the region containing Mare Imbrium and Oceanus Procellarum. This happens to be the place where potassium-40 is most abundant on the surface, and there may be a connection between the atmospheric argon, the surface potassium and deep interior sources.

So maybe a capture method employed at first daylight when the Argon is becoming mobile, but perhaps not as excited.  Or wells at locations such as Mare imbrium or Ocianus Procellarum.  Or, I have to wonder, if Argon condenses on the Lunar night side, then why would it not condense into the cold traps at the poles.

Of course I am thinking of Argon for your SEP notions.

Then there is a new item, "BuckyBombs", apparently a nano-scale energy storage method.
http://phys.org/news/2015-03-buckybomb- … sives.html
The Moon has Carbon Monoxide in the cold traps, and so Carbon.
But there are Silicon Buckyballs also.  I don't know if they could be modified to make Silicon BuckyBombs or not.  But there is plenty of that materials around on the Moon, and it is somewhat similar to Carbon.

How BuckyBombs could be used in a propulsion device, leads to vague speculation for me at this point.  My first thought was a downsized Orion propulsion method, with a pusher plate.  Apparently the energy release is very quick when they decompose.  Then again maybe something else.
It is not as good I think as engines using Hydrogen and Oxygen, but it is something different to consider.

One other thought I had about it would be to have a cord on a spool which has segments of this isolated by non-explosive segments, it would be unreeled into a engine bell/pusher plate, and a segment ignited.  Of course, should the spool have any ignition source, the whole thing would blow up.

It is notable that this method might be suited to other dry worlds where you don't want to consume Hydrogen.  However it would need more than Carbon or Silicon, so then where does that come from?

I am more interested in the Argon.

#8629 Re: Life on Mars » Past and Present life on Mars » 2015-03-06 18:34:01

I will settle peacefully for whatever is determined to be the truth, but I think the best method to have such an ocean on Mars would be a generally glaciated southern hemisphere (High Ground), and a generally ice covered basin in the north.

Antarctica and Greenland in the south, an Arctic Ocean in the North.  Maybe some dry deserts and volcano's to kick up dust to darken the surface of the ice from time to time.

This along with an atmosphere thick enough for cold melt water to persist long enough to run down into cracks and tunnels in the southern glacier would provide the water for rivers, and perhaps open water lakes at times at the equator.  I am presuming the rivers would mostly run under the ice cap in the southern hemisphere, and might emerge from it at the lower latitudes, only then to dump into a large ice covered ocean reservoir in the north.

That is a minim requirement for an Ocean in the North I think.  It also does not take into account the changing tilt of the axis of Mars that is said to occur.  But depending on the type of atmosphere, it may be that at that time the altitude of the south was sufficient to collect snow into an ice cap regardless of the amount of tilt.

With more atmosphere (1 Bar CO2) it could be nearly as warm as the Earth (But the sun was not as hot then).  But maybe comets and asteroids impacting had some CO2.  Maybe the volcano's could keep it resupplied for a time while it was young.

It changed though probably many times, and I am open to the facts if they can be found.

I believe that the last thing I read is that the ocean is thought to have filled twice.  The first time presumably from a surface water cycle, and the second time from ground reservoirs that were thought to have been melted by geothermal processes.

The second time they think the ocean just then froze solid and then evaporated away.

However, if the Mariner rift valley really does have fossil ice in it's bottom ~1 1/2 miles thick and other locations similar, I do not dismiss the idea that the northern basin is in part the remnant of a frozen sea, and some significant ice of that sea is still their under the dirt.

I think the abundance of heavy water is 5 times as great as for Earth.

http://www.realclearscience.com/2012/12 … 50332.html

This could indicate that Mars has lost 4/5 th's of it's original water.  If their is thick layers of ice from the Amazonian Era? deep buried, then that suggests to me that Mars had a lot of water originally,  perhaps more than the suggested ocean suggests.  If their was an ice cap in the south several miles thick, and covering an area similar to Antarctica. (Or more).

I have no proof, just speculation.

#8630 Re: Life on Mars » Past and Present life on Mars » 2015-03-06 11:55:20

Geology on the planet might reveal such an era.  If Mars did get more water then why not more CO2 than Earth?

Volcanism being another issue, my understanding is that Mars has less frequent, and more violent volcanism, and it's axis is thought to move about.  So, variable climate is the normal for it, most likely, constantly moving from one behavior to another, especially when it was younger.

I am of the opinion that ground currents contribute to a heat source for volcanism, along with radio-active decay.  Ground currents stimulated by high energy photons, wind, solar magnetic wind, etc. 

So if that were true, a volcanic episode could still happen, and if it did, and it spewed out greenhouse gasses, it is not impossible that for a short time period, the atmospheric pressure could double, snows fall and melt, and temporary streams exist.

The above could also occur on a temporary basis for a proper sized impacting object.

#8631 Re: Human missions » SLS Rocket + Orion + Apollo LEM » 2015-03-06 09:15:05

Nasa's efforts now seem to be on asteroid capture to Earth or Moon orbit, and visit.  This is an apparent adaptation to the fact that their Moon program was diverted to Mars.  So they adapted to a useful purpose, which could be helpful to Earth/Mars transportation.  Some private companies want to take this pathway, so Nasa appears to be blazing a trail.   I think they always said the Moon first, then from that experience Mars.  Now, they intend to create a temporary moon of the Moon, and do a similar thing.

SpaceX appears to aim at Earth to LEO, and beyond that to Mars.  However, I fail to see why they would not /could not Segway to the Moon at some point.

Other upcoming private concerns appear to be specifically aimed at the Moon, and also some national space programs.

Looking at the long term, it looks like a glass half full and filling up to me.

#8632 Re: Human missions » SLS Rocket + Orion + Apollo LEM » 2015-03-05 21:41:56

I am open minded about the Mars/Moon options.  I think it should be Mars + Moon.

The Moon is turning out to be more Mars like than was supposed, and of course as you mentioned it is closer. 

If SpaceX and others succeed in generating $500.00/pound to orbit, I don't see how they and their customers would want to ignore the Moon.

Since the Moon could aid access to the rest of the solar system, why would people who want to access the rest of the solar system want to continue to ignore the Moon?

#8633 Re: Life on Mars » Past and Present life on Mars » 2015-03-05 21:37:38

Here is a similar article:
http://phys.org/news/2015-03-mars-earth … ocean.html

You drew me in on this.

I suppose that at some best time Mars could have had an ocean as is indicated.

I believe it also had a planet wide glacier, perhaps before that similar to Ceres, but to a lesser magnitude.
I agree that it seems to be indicated that much water has been lost.

They still don't know how Mars could be warm enough for rivers.  I suppose it might have been if an unusual greenhouse effect was in existence.

However, under Antarctica and Greenland are rivers.  For Mars, imagine volcanic ash blanketing this planet wide glacier, explosive processes.

In the dry valleys, all it takes is a couple of weeks of warmer temperatures, and sunlight, and ice covered lakes can be filled.  And of course under our ice caps, ground heat and pressure can make liquid water.

I feel that since Mars has more lighter elements than Earth, it should have earlier also had more water than Earth.  Again Ceres suggests this.
It is thought by some that asteroids and comets started as mudballs, with a icy crust.  Radioactive materials could keep even them partially liquid for millions of years.

If mudballs hit the Earth and gave it water, then why is it unreasonable to think that more of them would have impacted Mars?  Mars is closer to the original reservoir.

Life supposedly showing up just after the great bombardment on Earth, suggests something to me.

I think it is likely that the mudballs were generally infected with life, and that it tried to infect every planet in the solar system.  We will perhaps find out about that in time.

#8634 Re: Human missions » SLS Rocket + Orion + Apollo LEM » 2015-03-04 09:35:15

http://en.wikipedia.org/wiki/List_of_pr … _companies

Looks like a glass half empty to me.  I am thinking the Moon is actually going to be a draw pretty soon (10-20 years).

I have read that the Moon has far more resources than was supposed during the Apollo era.  Carbon Monoxide, water, etc.

I think synthetic gravity devices will be possible on the Moon, so no need for "L" stations exposed to space hazards, unless as fuel depots.
That article suggested that launching to the outer solar system from the Moon would be 25-30 times easier than what we now do.
So, if Mars does not happen before the Moon, then it seems likely that it would happen from the Moon.

I for my part am willing to wait for NASA and other government supported space efforts, and private space efforts to throw enough spitballs until some stick.

Looking at the diversity, it looks like a evolutionary process is in play.  To focus too tightly now would be to risk being drawn into a cul-de-sac.  I believe that the Bigelo operation is ramping up again.  They apparently slowed down their efforts to wait for launch platforms to come into being.  With that and the various options available, I am wondering if a baton type craft could be implemented (GW stuff, synthetic gravity), for flights to Mars.  Maybe that's why the Orion does not have to be suitable on it's own for a flight to Mars.

#8635 Re: Life on Mars » Past and Present life on Mars » 2015-03-03 11:24:08

I am actually not much in the mood for posting just now, but I had to do this one.

I ran across an article in the "New Scientist" that talks about bacteria that eat and breath electrons.  You can query for it if you like.
I think I will play it safe and not link directly to it.  No harm was intended, but perhaps that is the better way to handle it.

I had also previously found articles that indicate that under UV light many materials will develop an electrical potential.

UV being unfriendly to normal Earth life, I have thought that even so, under soil particles heated, and where salt may help to depress the melting point of water, and to attract moisture.  Say duracrust.

And I also recall that supposedly UV stimulated materials may "Spark" with electrical discharge.  That as well as feeding or providing for breathing for such micro-organisms might momentarily warm them as well.

I hesitate to deviate, or to post on the same topic under life support, but I do wonder if humans having a significant electric generating machinery, might load level that (Use excess capacity) to generate a biosource from their periodic excess of electricity.

On a side note I recall speculating on electrically driven life many many years ago, and then reading a scientific article that stated absolutely that electricity was so hostile to life that life could never use it sad  So, that's an example of why things don't happen some times.  Happily it eventually happened in this case.

I might also suggest that for moons traveling through a parent planets magnetic field with radiation and solar flux acting as well, ground currents are not out of the question.  And if they traveled into the ground, then to perhaps melt some water, a habitat for life on those moons, maybe.  Europa, Ganymede?

#8636 Re: Human missions » Mars One » 2015-02-20 06:56:12

I have been told that cooking is at the heart of civilization.  He probably would be a stabilizer socially, and if he has gone to the effort of learning how to precisely do various cooking items, he would likely be very trainable.

#8637 Re: Not So Free Chat » Kim Stanley Robinson, The Mars Trilogy » 2015-02-18 23:41:23

Thanks for cheering me up smile
Good chances I will be dead first anyway.  Feel sorry for everyone else.  Yes there could be a chance, but have you had a look at the best and brightest?  Granted I am closer to 85 than 130, but as the article says, that won't matter much.

On the bright side, I have taken a look at the whole human race, it's history, and the patterns I see indicate a guiding force.  I won't go any further than that.  But I look at who is at the rudder and indeed how they (Don't) self limit, always find a reason to violate self restraint, As I said, maybe it won't be my problem.

I feel kind of sorry for the little ones though.  I hope that pattern I think I noticed will feel sorry for them also.

#8638 Re: Interplanetary transportation » Mars Colonial Transporter » 2015-02-18 14:57:08

Well, you know I am a feather weight in the ring with heavyweights here, so, I am not going to push my position very hard.  In checking and double checking I ran into this which is interesting and new (To me).

http://www.scientificamerican.com/artic … the-cheap/

#8639 Re: Science, Technology, and Astronomy » Self-Replicating Machine: Beginning Design » 2015-02-18 11:21:07

Well I will wish them success.  I expect that if they do go for it, a swarm of humans and there robotic offspring could augment that nations and businesses are doing in space.  Providing another aspect unique to non-national, and not necessarily profit harvesting (Until success).

While I was coming up with the above response, it occurred to me that factory automation followed anchored robotics is a bit like sponges and other anchored sea organisms which wait for their raw materials to float/swim by.

We are not quite to the level of paying self actuated robots which alter/manufacture objects, but it is likely to come when it does come to Earth, it would not be that hard to transfer it to other worlds.

#8640 Re: Unmanned probes » Dawn - Vesta & Ceres orbiter » 2015-02-18 06:55:21

http://www.space.com/28579-ceres-bright … hotos.html

White spots.

ceres-photos-nasa-dawn.jpg?1424202922

My eyes think that the world has two different surfaces, a smoother one and a more rugged one.

The white spots seem to be mostly on the smoother side.

That's what I see anyway.  Better pictures required I suppose.

#8641 Re: Interplanetary transportation » Mars Colonial Transporter » 2015-02-17 21:58:38

I feel as though you might be baiting me, but that's alright.
It seems that you think that Titan might be suitable for a powered descent.

I wonder though, if it some point it becomes an economic decision?  SpaceX is supposing a hoped for cost of $500/pound of mass from Earths surface to orbit.  When is fuel so cheep that you might begin to think No I don't want to rely on dangerous pushed to the limits methods for aerocapture?

The Mars colonial (I don't like the word colonial because of the historical baggage it carries, but it is their words) transport is supposed to carry up to 100 persons.  I can't imagine they intend to aerocapture that.  It's mass to surface area ratio would not be as favorable as a ship to send say 4 people in a smaller ship.  So they must intend to power to orbit, and then either power all the way down, or use a reusable transport with heat shield and canted engines.  In either case, they have partially or totally used a powered descent to get from Mars intercept orbit to Mars surface.

The stuff I presented this weekend was mostly B.S. on my part.  I thought there was little harm in it since very few people were at that time using the site.  However given the budget, even that might work.

I have been put off by the descriptions of the rigors that are imposed by the one method that seems to be most popular, that apparently is total aerocapture for the humans for reasons of radiation and presumed constraints on mass.  One of our most genuine experts seems to think that there is a major impediment to landing a large ship.  I trust that that person knows what that person is talking about.

But I am wondering if the thinking is so locked into the Apollo methods, the presumed SLS methods that they do not consider the changes that might come from lower cost fuel and Oxygen?

But I know that in the end facts are facts.  You can't just say that you will sprout wings and fly to Mars.

Even so, since you concede that Titan might allow a powered descent, how about consideration of a hybrid method for Mars.  A partial powered change in speed, might give you more liberties for the mass of the object that you hope to land, and also for the materials that it is constructed from.

#8642 Re: Life support systems » Martian industry » 2015-02-16 14:58:27

You have to define what you mean by functioning.

The Norse Greenland colony was functioning for quite some time, but climate went against them, they were isolated, and probably very specialized to do farming in land that was marginally farmable at the best times.  They were non-adaptive until it was too late.

So do you want it to be apparently functionally with help from Earth?

Or do you want it to be persistently functional into the far future even if Earth were to fall into a "Dark Ages"?

I am being a bit of a jerk about the above.

Small numbers of specialized people is a start, but they might not be persistent against adversity.  Large numbers might give enough diversity to promote adaptability.

Apparently Elon Musk is thinking 80,000 new people on Mars a year at some point in the future.

http://www.popsci.com/technology/articl … ars-colony

So, to recap: Musk wants his private spaceflight business to send 80,000 people to Mars every year. They're not going to do that themselves, probably, but the company would certainly be leading the charge.

That's going boldly.

They must have some things up their sleeve about how those people are going to get what they need.

Just thinking big, the Mariner Rift Valley is though to have ice perhaps ~1.5 miles deep.  Now that I think about it, if you could get a nuclear reactor through the soil and rock and down to that ice, you could indeed have quite a water supply there.  the top would want to sublimate but what if dust storms continually covered it with dirt which would protect the ice over a body of melt water?  The you could simply sink a well, and pump melted water up to the surface.  Yes it would loose ice mass over time but there would be plenty for a long time.  It would likely form a sinkhole with a dirty ice covering, with dust continually trying to fill the hole over time.  Perhaps other ice near the equator also exists at more accessible locations, but if you want to bootstrap a civilization on Mars and also terraform it, having a massive water supply and equatorial solar energy would have to help your chances.

Perhaps a aircraft with rocket horizontal and vertical lift methods, and a lifting body configuration/airplane configuration would be ideal for travel, if you had the fuel.  Alaska is like that where aircraft is often your best travel option.  A device to allow you to move up from the valley floor to the rims, and which also might fly nicely at a large horizontal speed once you reached altitude?

I would try to make it also have hovercraft features as well, since it would have lift engines in it's bottom.

Crashes would likely be lethal, but that's probably true for Alaska as well.  Then again if you have 80,000 persons a year arriving, surely you could have some of them devoted to rescue missions.

#8643 Re: Terraformation » Mercury » 2015-02-16 09:37:18

Just a continuation of extreme speculation.
Returning to your original solution of a dynamic sun blocker in front of the planet, then utilizing the magnetic field of the planet that I presume will be allowed to expand.  The most valuable asset will be the ability of the magnetic field and surface materials to generate water, for as long as the solar wind and planet Mercury exist.  That is at least a billion years.

For giggles however, I wonder about indeed digging the maximum allowable hole(s) at one or more poles.  While the planet has a very thick rigid crust and no tectonic movements, I read that it would have Mercury quakes from the condition where the planet is shrinking as it cools.

The point being that if you wanted to continue to remove materials from the planet you would not want the average air pressure to become very high, considerably less than that of Mars.  But there would have to be limits on how deep you could dig a hole at the poles.  It is a silly notion I know, but you did speculate on mining the whole planet completely, I would think that for the purposes of having a very long term source of water, it would be better to dig holes at the poles, just maybe deep enough to support some higher atmospheric pressure within.  And to provide materials to build that dynamic sun blocker.

For Mars, which has a similar gravity field:
http://en.wikipedia.org/wiki/Atmosphere_of_Mars

Structure[edit]

Pressure comparison


Where

Pressure


Olympus Mons summit
0.03 kilopascals (0.0044 psi)

Mars average
0.6 kilopascals (0.087 psi)

Hellas Planitia bottom
1.16 kilopascals (0.168 psi)

Armstrong limit
6.25 kilopascals (0.906 psi)

Mount Everest summit[11]
33.7 kilopascals (4.89 psi)

Earth sea level
101.3 kilopascals (14.69 psi)

Mars's atmosphere is composed of the following layers:
Lower atmosphere: A warm region affected by heat from airborne dust and from the ground.
Middle atmosphere: The region in which Mars's jetstream flows
Upper atmosphere, or thermosphere: A region with very high temperatures, caused by heating from the Sun. Atmospheric gases start to separate from each other at these altitudes, rather than forming the even mix found in the lower atmospheric layers.
Exosphere: Typically stated to start at 200 km (120 mi) and higher, this region is where the last wisps of atmosphere merge into the vacuum of space. There is no distinct boundary where the atmosphere ends; it just tapers away.

There is also a complicated ionosphere,[12] and a seasonal ozone layer over the south pole.[13]

If the whole of the planet had an

Exosphere: Typically stated to start at 200 km (120 mi) and higher, this region is where the last wisps of atmosphere merge into the vacuum of space. There is no distinct boundary where the atmosphere ends; it just tapers away.

It already has a temporary and I presume on the low end of pressure, Exosphere.  If that were improved to be the highest level for an Exosphere. then the holes would need to be at least

200 km (120 mi)

deep to even think of supporting ice covered water pools.

That's pretty deep.  But if it was like a strip mining operation, maybe.  I simply don't know.  But if you could do it then you would have a location more favorable to humans, with perhaps sufficient radiation protection (Along with the magnetic field?).  And an atmosphere to do aerocapture of arriving spacecraft.  And also most likely a natural collection point for water generated by the incorporation of solar wind into the magnetic field where it the Hydrogen would combine with Oxygen from rocks, or from the puddle of atmosphere you would have at the poles.

#8644 Re: Interplanetary transportation » Amortizing reusable Mars Transports » 2015-02-16 09:18:35

I suppose you are correct.  Once they have raw materials for 3D printers and other manufacturing methods, electronic exports from Earth to Mars, will satisfy most needs.  I would think bringing in the equipment to be able to obtain those raw materials would be the extravagant part.

#8645 Re: Interplanetary transportation » DSCOVR Launch » 2015-02-15 16:19:39

They will have to profile their system, to find out what the actual expectations can be.

Yes they will have to inspect, and sometimes replace parts.

It is not a totally free booster to reuse.

I would think that they might phase them.  Use the newest best ones to launch more critical loads, and if there is such, use the old ones to launch less critical loads.  Less critical loads might be fuel and Oxygen to low Earth orbit.  Storage of such to a purpose not yet defined, but perhaps to come.

And then I have been thinking about it because of your response, what about the Moon?  As these things become less qualified for flight, perhaps use a falcon heavy without a payload, the middle booster being the marginal one.  The notion being that that one could be outfitted with a different set of landing legs, which would only be folded up once.  Send it to the Moon, where it's use would no longer involve passing through the atmosphere up and down, and also where it's engines could be operated at a lower thrust level to compensate for their marginal trust levels.

So I presume the would be lifting loads like LOX manufactured on the Moons surface.  The tanks perhaps could be wheeled over and attached to the landing legs, to make the assembly less tipsy?

Similarly of course perhaps metals could be lifted, perhaps materials suitable for a 3D printing process?

I think there would be less options for repairs, perhaps if one was no longer suitable for that purpose, it would just go to junk on the Moon, or if it could it might lift itself to a "L" location to serve a purpose.  Maybe even still as a booster that does not land.  But that would only apply if it could still do valuable work.  It seems less likely that that 3rd option would be workable.

So SpaceX might just have the Moon in it's pocket as well, if they prove their system.

I don't think they will wait for the Moon LOX to go to Mars however, but eventually it might be a part of a larger transport effort.

I am trying to use your acronyms.  Perhaps that will please the hosts.

#8646 Re: Terraformation » Mercury » 2015-02-15 12:56:21

As I was thinking about your post, it came to me also that a more ambitious mode of operation would be to put a ring in solar orbit to serve the same purpose as placing a construction in L1.  Obviously then there would be much more solar energy obtained, but also much more of Mercury would have to be mined.  Still, this is then a very tiny step towards a Dyson Sphere.  Actually for my tastes as much as should be bothered with.

Really how many people should exist anyway?  What is optimal for a stable so called civilization.  Actually we would not want it to be completely stable, but reasonably progressing, whatever progress is.  Social pressures would determine objectives as well as just thinking about it though.

Anyway I was thinking that such a ring could then when it was not shading Mercury project energy to the Ice Giant planets Neptune, and Uranus.
By swelling their atmospheres, it might be possible to capture the atmospheres to orbital machines (Fusion).  But perhaps also shattering their moons, by causing them to drag in such an expanded atmosphere and get too close to the primary object.  Expand the atmospheres, and then drag a moon closer, contracting the atmosphere by reducing the solar energy, so that when the moon shatters, it is not dragged into the planet.

Or alternately, just dragging the moon close enough so that the balance of gravitation allows easy movement of moon materials into the L1 location?  Then however you would have to remove an enormous amount of overburden (Ices) before you got to the metals and silicates.
Triton might be a good candidate I am thinking.

And if you really want to be silly, boil off the atmospheres of Neptune and Uranus to space.  But that is wasteful.  It would also take an enormous amount of time to do that, and the glowing hot balls of rock would emit enormous amounts of gases for a very long time, and would take quite a time to cool.

Again how many people does a so called civilization need?  Granted the more people you have the better chances of a genius, and then everyone can try to copy the work of such a person, but what is a good rate of cultural/technical progression.  Can we evolve too fast with technology, and not fast enough in our abilities to co-exist?

A better use would be to consider shattering Triton, and building starships with the materials, spilling humans/machines over the local stellar area.   Perhaps if we did that alien civilizations would call an exterminator however.  If they didn't, then we would have a polynesian situation where the magnitude of each worlds power would be insufficient to wage a large enough war to make it worthwhile to war on your neighbor solar systems.  In such a situation, it is likely that while some worlds would descend into decay due to human demonic domination urges, others would forge on sensibly.  Worlds that went extinct or returned to the wild after a period of human demonic domination would then potentially be restarted by their more sensible neighbors.  In that way it is possible that some subpart will at some time reach a higher state of being, a progression that would make us as we are seem sub-human.  (But we will be long gone, so it won't hurt).

#8647 Re: Terraformation » Mercury » 2015-02-15 12:41:46

O.K.

It's not unthinkable, for a future trans human descendent population.

You made me think about it.

Once you did L1, you might as well make it into a space community with synthetic gravity habitats.  Then that has to fly in front of Mercury, as you have said, maintaining station with the assistance of solar energy, photons and/or the solar wind.

If they have a desire to simulate Earth on Mercury, then that might be possible.

You have overlooked the magnetic field of Mercury as an asset so far though.  I would think with the device being in L1, it could expand more than it is, and between the L1 protection and the Magnetic field, circumstances to keep an atmosphere would be improved.  As it is, the magnetic field temporarily captures Hydrogen, and facilitates the formation of water in the Exosphere of Mercury, but a bit of help from comets wouldn't hurt.

The situation on such a terraformed Mercury, would then however depend on good behavior of the inhabitants in L1.  Human nature historically tends to foster cultural fracturing, and when that reaches storm level, typically a binary conflict behavior.  This is apparently part of our self or directed (From somewhere) crafting/evolution process, to direct the human race(s) to a different character.  Non-Adaptive characteristics are reduced, and adaptive characteristics favored.

Perhaps Mercury would be a park/mining planet, which the bulk of people/machines would visit.  For mining purposes, the level of terraformation would only be served by Earth desert like conditions.  So the amount of water needed would be reduced.  Perhaps the poles only would be wet enough for Earth similar environments, and the rest of the planet strip mined.

#8648 Re: Interplanetary transportation » DSCOVR Launch » 2015-02-14 17:54:09

It did not occur to me before, but boosters landed in Florida, could be given a once over, partially refueled, and instructed to hop back to Texas.  No canal needed.

#8649 Re: Science, Technology, and Astronomy » Self-Replicating Machine: Beginning Design » 2015-02-14 14:54:55

Part of worm brain "Uploaded" to a robot.

http://www.cnn.com/2015/01/21/tech/mci- … index.html

So, I am thinking that some time from now, a 3D printer/Robot serving as the "Queen".

Printing out little bee or ant robots.  Workers only I would think.

Then the workers go out and get grains of materials that can be "Eaten" by the "Queen" to make more workers.

Dead bees/ants recycled I presume.

But when the "Queen" malfunctioned I suppose it would have to be repaired/replaced by humans.

But even this is still far fetched.  However I might suggest that by "Digesting" a grain of soil material at a time it might be possible to find ways to purify the materials at a low energy cost.

Still a long way off though I think.

But such robots would not scare me very much, since their replication machines would be dependent on humans, and at most they would have a hive mind, and no stingers.

I suppose Venus and Titan might be a good place for it.  In the case of Venus, perhaps they would not so much gather materials but construct a floating hive.  The 3D printer would have to absorb materials from the atmosphere.  In the case of Titan, I am supposing that the energy source would have to be chemical, I recall mention of an existing one, involving Titan might use hydrogen and acetylene as an energy source

http://en.wikipedia.org/wiki/Life_on_Titan

But that does not seem to me to be a very vigorous energy source.

#8650 Re: Interplanetary transportation » DSCOVR Launch » 2015-02-14 13:15:44

Alright, I guess I should have said it a bit different.

VOID wrote:


So what if;
-Send a person transporter to Mars, composed of;
     -Lander without;
          -Parachute.
          -Heat Shield.
          -Canted Engines

Anything entering Mars upper atmosphere and headed towards a landing will need a heat shield of some sort and that is why Mars uses PICA rather than the heavy metal shield of orion. That said that a material must be found that can widthstand the heat of entry but be as light as possible and still get the job done is a must.

Parachutes can only be removed if you used a powered descent which can include canted engines if used for more than final 100 meter or feet of descent to touch down and a lifting body of some sorts both have there own respective penalties to make a successful landing.

http://en.wikipedia.org/wiki/SpaceX_reu … nt_program

the first-stage separation would occur at a velocity of approximately 2.0 km/s (6,500 km/h; 4,100 mph; Mach 6) rather than the 3.4 km/s (11,000 km/h; 7,000 mph; Mach 10) for an expendable Falcon 9, to provide the residual fuel necessary for the deceleration and turnaround maneuver and the controlled descent and landing

Granted, this is only a small percentage of the speed change needed to be captured to the surface of Mars, from the energy of orbit necessary to get to the vicinity of Mars.

It is a heat shield of sorts, the rocket plume.  It is cooler than the plasma generated by re-entry.  But I was thinking brut force to get rid of the other energy prior to this phase of entry.  I know that involves a lot of fuel, and so a lot of cost.

However, if SpaceX can launch for $1000.00/pound, and the tanks for storing the methane are lighter, a bigger fuel budget is possible, than for using the SLS.

As for reentering with a booster below, this might be similar to having a sky crane, but in this case it is to help deliver the lander to the atmospheric conditions it could survive in without parachutes (Which are out anyway I am supposing), and without a heat shield.  Keeping the lander light enough so that it could hop about like an aircraft later, and also to help it be able to get to orbit when that was desired.

You did force me to rethink the situation however.  I did suggest external tanks for the brute force maneuver, getting rid of the bulk of differential speed.  I suggested that the tank(s) could be discarded after empty.

I would like to play with another idea.  Perhaps if the tank(s) were a surround of the stack of the booster and lander, when filled they would be a radiation shield.  After emptied, perhaps they could serve as a heat shield, increasing the footprint size of the entry vehicle.

This would require that the tank walls be able to serve this triple purpose.  Container for radiation shield, holder of brute force fuel,  heat shield.

I recall that one method to cool a heat shield is to push a rocket engine plume in front of it.  I don't know how much such engines would be able to take as far as having hot plasma pushing against them.  Should they fail, that would be a disaster for sure I presume.

So anyway, I am presuming that;
-The tank(s) are a surround of the cylindrical stack of the booster and lander.
-The tank(s) will be emptied, by burning the fuel in them in a brute force slow down effort, to reduce the entry speed to what could be handled.
-As a precaution, prior to entering the atmosphere, it might be wise to vent the tanks to vacuum to hope to remove as much residual fuel as possible.
-The assembly would hit the atmosphere, and a rocket plume would or would not be used to cool the heat shield, and help in slowing down and navigation.
-A dangerous action after that would be to dispense with the tank(s) while at still rather high speed in the atmosphere, and then further slow down riding on the booster rocket plume.
-Then release the lander, and get the booster out of the way, to either crash, or push itself to orbit.

I know I am under qualified on this but I am interested in hearing your arguments in response.

Maybe I am out of line as far as the canted engines?  Perhaps they are best for a hopping aircraft/rocket on Mars?

As an amendment to the above.  You mentioned lifting air body.  I suppose the assembly with the external tanks might have a shape like a lifting air body, but I am sure the external tank/(Radiation shield-Fuel Tank-Heat Shield) would be dispensed with soon after re-entry, so I don't know what benefits could be derived by having it have those qualities.  But since I am not actually spending anyone's money, or hurting anything except your minds, I have included it.

  1. Index
  2. » Search
  3. » Posts by Void

Board footer

Powered by FluxBB