New Mars Forums

Official discussion forum of The Mars Society plus New Mars Image Server

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

#8976 Re: Life support systems » Crops » 2014-01-08 11:31:34

In the case of the polar ice caps, I am thinking of them as condensers for a solar concentrating power generating system, with a fluid such as Ammonia
or Ammonia/Water mix.

If the top of the ice layer is at some very cold temperature, just a guess, 100 degrees below (Pick your units), it is not likely to vaporize, but a layer of ice of sufficient thickness, transparent or translucent could insulate the ocean, holding in the heat.  Even if the ice surface slowly vaporized, it has no where to go ultimately but back to the poles under the current tilt of the planet.

Ideally, I would prefer to just boil water, and quench it directly into ice water, but of course the sea water would be of poor quality for that, and the above surface piping would be subject to freezing during down time.  However a massive seasonal energy source that also provides a biosphere in the current Martian or improved Martian conditions has to be of interest. 

Further, just generating Oxygen and Methane and injecting them into the ocean should generate biological activity, and any Methane and Oxygen leaked to the atmosphere will simply make Mars more habitable.  It stands to reason that if such a process were running leakage would occur.

It might be that Ammonia and Ammonia/Water would freeze, but perhaps there is another suitable fluid to drive the turbines.

I would also mention that I believe that Mars gets more solar energy at it's poles than the Earth, because of the tilt.

#8977 Interplanetary transportation » Atmospheric Grazing » 2014-01-08 09:10:22

Void
Replies: 17

I wonder if the process of atmospheric grazing could support delivery of materials to Mars?

http://mars.jpl.nasa.gov/mro/news/index … NewsID=142

It has been done to help deliver automated missions to Mars already.

I guess I am thinking of an electric rocket system with solar panels.  The objective would be to reduce the required propulsion mass for the delivery, by
using the solar panels as aerobraking devices after the electric rocket gets into Martian orbit.  Grazing is a possiblity, and perhaps it could even be investigated if such solar panels could also serve as high altitude wings, but that makes it more complicated.  I don't think active surfaces would work well at high altitudes such as flaps, but still it is an interesting thought.

The method if used could help to move payloads to low orbit.  Perhaps consumables, fuel, and Oxydizers, or perhaps a lander.

Of course this would be in support of a following human mission to Mars.

It might also be involved in collecting samples from Phobos and Demos prior to achieving the low orbit.

#8978 Re: Life support systems » Crops » 2014-01-07 11:23:15

While I fully support the ideas pesented so far, there can also be this type of thing.

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

Inuit diet

From Wikipedia, the free encyclopedia

Jump to: navigation, search 
Inuit elders eating Maktaaq.Inuit consume a diet of foods that are fished, hunted, and gathered locally. This may include walrus, Ringed Seal, Bearded Seal, beluga whale, caribou, polar bear, muskoxen, birds (including their eggs) and fish. While it is not possible to cultivate native plants for food in the Arctic, the Inuit have traditionally gathered those that are naturally available. Grasses, tubers, roots, stems, berries, fireweed and seaweed (kuanniq or edible seaweed) were collected and preserved depending on the season and the location.[1][2][3][4][5][6][7]

According to Edmund Searles in his article "Food and the Making of Modern Inuit Identities," they consume this type of diet because a mostly meat diet is "effective in keeping the body warm, making the body strong, keeping the body fit, and even making that body healthy".[6]

Of course the sea mamals are not an option, and the tundra plants are iffy, but the fish and seaweed might be possible.

Enclosures could be ice covered or made of manufactured materials, or both.  In early days water would likely come from lower lattitude glaciers, but later when Mars is more developed, I see no reason not to liquify the polar caps into ice covered bodies of water, once the atmosphere becomes thick enough for stable ice, and then later after that there could be open water. 

Energy for life could be though Ice or water (Depending on the thickness of the atmosphere), and also artificial lighting underwater, and also chemicals could be manufactured to drive living things like fish and shell fish ecologies.  Such exist on Earth today.

#8979 Re: Terraformation » Methods of terraforming - How to go from bone dry & lifeless » 2013-12-23 11:18:07

I decided not to start a new topic, maybe this is an OK place.

Calalyst

http://arpa-e.energy.gov/?q=arpa-e-proj … water-fuel

I am wondering if it might be possible to find a catalyst that would operate with U.V. energy, that could be dropped as a dust onto certain locations of the Martian polar ice caps, to produce greenhouse gasses.  The "Dust" perhaps would need to be hollow so as to be likely to "float" on the surface of the ice cap when it evaporates, and not to sink into it.

If such could be created, it might persist at the location deposited, and work multiple times before degrading.

I am not compentent in chemestry, but I know what I would like, a cheep pathway actually to terraformation.  I am thinking Methane from CO2 and evaporated water, with the catalyst actived by U.V. light.

The application would not require a soft landing, but rather entry to the atmosphere without damage to the cargo, and then an atmospheric dispersal to the icy surfaces.

#8980 Re: Human missions » Scatology on Mars » 2013-12-23 09:47:19

I would make a poo heater with a solar concentrating mirror.  Sterilize it that way, maybe recover some hydrocarbon fuels.  Then add the ashes to soil to grow food, or pack the ashes away in a burried bag as previously suggested for future gardening.  Destructive distillation.

#8981 Re: Life on Mars » Ice Worms » 2013-12-23 06:55:42

I have nothing to add on Iron.  (Don't know).

But, I have been considering why life from Earth may not be surviving long term on Mars.  For instance my favorite traveler now would be a piece of sandstone from Earth that would have organisms that live a quarter of an inch or so inside the rock.  Maybe capable of photosynthisis.

I have thought that if such a rock landed on sandstone where there was a regular depositing of water ice, in the darkness, and then a warming in the day, there is the potential
of morning and sunset dews (Frosts).  Lichen can absorb mosisture directly from unmelted frost or snow.  Plus, it is possible for liquid water to exist long enough in each thaw for lichen (Or other life) to get a drink.  Then there is the possibility of a glaze of ice melting from the bottom up as mentioned in a previous post.

So I have wondered why Mars may not host such organisms.  Josh said the methane if missing, and I actually buy into that.  However, if the amount of life was very small, perhaps it could be there.

It seems that there could be small habitats that get watered even now, and it appears that when Mars has a greater tilt of axis, the Equator may be both watered, and warm enough for daily melts, cold enough for nightly snows and frosts.

That seems the best situation for life to me.

But what is Mars like if it has a Zero degree axis? (If it ever does).
http://en.wikipedia.org/wiki/Axial_tilt

Mars' obliquity is currently in a chaotic state; it varies as much as 0° to 60° over some millions of years, depending on perturbations of the planets.[16][26] The obliquities of the outer planets are considered relatively stable. Some authors dispute that Mars' obliquity is chaotic, and show that tidal dissipation and viscous core-mantle coupling are adequate for it to have reached a fully damped state, similar to Mercury and Venus.[2][27]

I am thinking that the water gets locked up in the poles, and does not experience enough warmth for thawing.  So the high lattitudes are watered (Ice) but cold, and the lower lattitudes are arid but warm.

This could be very unfavorable to surface life, if it persists for a very long time.

And as Josh has suggested the aquifers below may be very salty and unfavorable to life as well.

So, this could be a sterilization process.

Perhaps Earth life was established on the surface of Mars (Or more likely a fraction of an inch inside of sandstone) several times, only to be made extinct during such an unfavorable event as lack of axis tilt.

Aside from that I have wondered if at zero degrees axis it might be possible that the CO2 component of the atmosphere could collapse into the poles, dropping the air pressure even more than now.  Making Mars even more aggressively hostile to life.  Don't know about that.  Maybe.  It would be for the same reason the Moon is thought to have water ice in shaded spots at the poles.

#8982 Re: Life on Mars » Ice Worms » 2013-12-19 09:01:14

I will resort to lichen as the example life form that could benefit,
and agree that ice worms would require even more favor than the lichen.

Lichens have been shown to be able to survive and even like Mars like conditions in cracks in rocks, getting water,
from the dawn and dusk dews, not even needing water in ice.

But some Lichens like to grow inside of rocks in Antarctica.



Is there a condensation process that can lay clear or translucent water ice over sandstone or other rock that
lichen could grown in?

Perhaps in some climatic locations on Mars???


If so then I suggest that it can bottle pressure inside wet bubbles in the ice (Until they rupture).

This could be a repetitive watering process where ice is deposited, the sun comes up and heats the rock through
the ice, and a short period of wet occurs on the rock surface where pressurization is maintained by the ice
deposited on the rock, and then very likely a rupture.  But such a period of wetness might be all that is needed.


I do not expect life in assocation with CO2 Ice eruptions, but it's model can suggest a similar one for water ice
on a less noticible scale.
Much like the dry bubbles created with clear CO2 ice as mentioned here:
CO2  (The only reason you can see the spider-Trees is that these ruptured).
http://en.wikipedia.org/wiki/Martian_geyser

From the above reference (Strangely),  an interesting idea,  I suppose water column or container pressurization are possible.
515px-DDS_MSO.jpg

But this is all speculation.
I think the point is that it is very likely that there are temporary improvements of certain locations on Mars to the degree that it could favor life
more than normal.  How that life could be established in those locations?  Spores in the wind?

#8983 Re: Life on Mars » Ice Worms » 2013-12-18 16:22:34

Well, here I finally found something related to what I was referencing.  It seems that some persons believe that a rock falling into an ice field, can create a pocket of water, in this case while it does not hurt to have a water column, for instance on Mars, I estimate that 1 foot of water is worth about
10 mb pressurization.  The water in question if fresh would be 0 degrees C, and not much pressurized above the Martian ambient, and in fact in some locations, that air pressure approaches 12 mb at times?

But, I think they may also speculate on a bottling effect, where the ice holds temporary pressuization during high noon by it's strength, and a thin film of liquid water may form around or even inside of a rock.


http://mpainesyd.com/filechute/paine_am … permia.pdf

One is where solar radiation heats
subsurface ice which melts and the pocket of melt-water retains sufficient pressure to
avoid sublimation. This could be quite common where ice is present and is exposed to
partial sunlight.
3 Finding

Using Antarctica as an analogy, it is estimated that 12% of the ice on Mars would
be exposed to sufficient sunlight to melt sub-surface ice in summer each year
(speculative). Assuming three months of sufficient sunlight per year then, on average,
2% of all of the surface ice could be expected to have liquid water near the surface.
This means that, on average, 0.015% (2% x 0.73%) of the Mars surface has liquid
water near the surface.

This is another interesting article I encounted during the search.  It points out that the Mars climate is variable, as to pressure and tilt (Therefore location of snowfall) and that could also make ice melts more likely during variations.

http://www.planetary.org/blogs/emily-la … hesis.html

But we agree that the Methane is missing.

And please note, none of the above orignates from me (Obiously), so, I am mearly parroting things I read, no innovation being attempted here.

#8984 Re: Life on Mars » Ice Worms » 2013-12-18 15:07:54

Quote:

•Cells require liquid water to function.  On Mars, this means massive amounts of salt that would necessarily inhibit the enzymes and vital biological functions of a cell, not even to mention a more complex, megamulticellular organism

I almost entirely agree with you but on this point, water ice can be liquid without salt.  Exposed ice can serve as a greenhouse window, and articles I have read indicate that this is widly true.  Don't know how acid the ice and it's melt water would be.

With that favor I pretty much agree with you.  The lack of Methane is a killer.

Further, it is hard to see how tiny plants and worms could migrate from one isolated pocket of water to another.

I recall that this was put forward however as a means for panspermia from Earth to Mars.  An Earth rock impacting a temperate ice field could expose clear ice, be embeded in it and for a time period have melted water around it.  So entering the Martian undergrounds.

No evidence of it though.

#8985 Terraformation » Manufactured Planet Rings » 2013-12-13 09:14:31

Void
Replies: 2

I had a notion this morning, that it might be possible to treat Saturns ring as a machine.  Much is unknown about the rings, but I do know that it has mass, gravitational, and electrical properties and is composed of a multitude of pieces which seem to work together with Saturn to maintain a form.
That form must interact with the space environment, the solar wind, and the solar flux.

Actually I would not want to damage those rings, so I am now thinking that nearer objects could be an interesting target.  Mars and Jupiter for instance.
I really don't know if manufacured rings could be created.  For Mars, it could not be of ice, but for Jupiter perhaps it could.

Dumb rings would be mostly composed of rock or ice objects.

Smart rings could be as in the often mentioned hall machine, a multitude of tiny machines.

I do not know if a ring can deflect and concentrate solar wind, but solar wind can be tapped for energy, so that is an interesting possibility.
Also rings seem to have electrical properties, so perhaps that could be tapped.
Then there is the possibility to shade or brighten parts of the environment of Mars at times.

For Jupiter, it might be possible that rings could reduce the number of dangerous particles in its radiation belts.  (Or make it worse).

But anyway trying to think of how to manufacture a planet ring might also lead to insights on how they work.

#8986 Re: Water on Mars » mars-water-discovery-curiosity-rover » 2013-12-05 15:21:23

I have no certainty that what I will suggest next can actually work on Mars, but it is worth the risk of being wrong.

http://skullsinthestars.com/2011/05/27/ … ctrifying/

http://www.asknature.org/strategy/0635d … 5947962fee

http://books.google.com/books?id=bAwVvO … nt&f=false

I a military establishment used electric currents in the ground to dry out wet ground, so that tanks could pass over it.

So, if Mars soil does have a quantity of moisture, and it is associated with salt, perhaps it is essentially a very cold brine in some cases.  If so, then two electrodes deployed might cause it to concentrate on one electrode, which could be inside of a solar still.  This would then result in steam, and that could be captured with a vacuum system (Fan/Compressor and a condenser).

Each day the soil should be replenished from the atmosphere to a degree, if the salt remains present.

Of course the salt toxic charactistic would need to be handled, if it traveled with the water vapor some how.

#8987 Re: Life support systems » Extra Oxygen? » 2013-12-04 09:24:24

As water seems to have been found even in "Dry" soils, I would suggest for the early term, making tanks or reserviors (Covered), filled with water, would allow extra oxygen to be stored in a disolved state in the water, available for emergency extraction if necessary.

Here is an article on extracting disolved oxygen:
http://en.wikipedia.org/wiki/Artificial_gills_(human)

Also such reservoirs would most likely be cold, but it might be possible to include some animal life that consumes Oxygen and Methane Seeps.  This would allow such a disolved air tank to earn it's keep when it was not serving as an emergency Oxygen supply.

I choose Methane, as the food for the animals, because if Methane were to be manufactured for fuel and as feedstock for industrial purposes, it would always be desirable to be able to manufacture more than can be stored.  In that case if excess Methane is also available it can be injected into a water tank/reservoir as discribed above to help activate a chemically driven biology.

Here is a not very related article I will connect to here.  I found it while searching for the artificial gills.  It is kind in the line of thinking anyway:
http://downloadsquad.switched.com/2007/ … ed-oxygen/

#8988 Re: Interplanetary transportation » Elastic Launch Loop (Space Elevator) » 2013-11-26 11:24:19

You guys have started talking skyhooks.  You seem to be talking about an above atmosphere skyhook process.

I have a question.  If you are going to have a loop or elivator, or spinning tether (My preference) with a hook to grab hardware, why could you not also grab atmosphere?

When hooking hardware, I presume that the hardware and hook must have a point in time of virtual zero differential speed.

When grabbing atmosphere a small amount of differential speed could be tollerated.

In order to keep your grabber from burning up, you either do not dip too deep into the atmosphere, or you maintain a small enough differential speed by spinning the grabber appropriatly.
What good is grabbed atmosphere?  Oxygen, Nitrogen, maybe some Argon, and other trace gasses?  To be used in chemestry, or life support, or propulsion, Chemical propulsion or condensed to liquid or ice and expelled with a linear magnetic device.

Maybe you will show me that this is not a good application, but I am inclined to think that it could be quite useful.  Sorry for the diversion from the hardware hook though.

#8989 Re: Interplanetary transportation » Paraffin, propulsion and other uses, crash-landing it. » 2013-11-21 14:55:32

I guess I could put this here as an update of notions:

So, I have the following references on Paraffin Wax, and Nitrous Oxide.

http://www.space.com/23648-new-rocket-e … video.html
http://www.youtube.com/watch?v=DMVgAB_dau4

http://en.wikipedia.org/wiki/Paraffin_wax
http://en.wikipedia.org/wiki/Nitrous_ox … _reactions

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

Rocket fuel and Oxydizer (With the option to hard land Paraffin Wax with minimal protection and still have it be useful and retrievable).

Internal engine fuel and Oxydizer (Cars, Tractors, MG Sets (Motor Generator Sets)).

Parafin Wax, other uses:
Radiation Shielding in the case of Paraffin Wax.
Candles a strange thougt, but in a lighting outage for emergencies, perhaps candles could be used in a limited fashion.
Electrical insulator for potted electrical and electronic devices.
Thermostats for process control systems.

Nitrous Oxide:
Medical use for the Nitrous Oxide
Another feature is that it can be solid or liquid form at temperatures reasonably sustainable in the Martian environment (With technological tricks
employed).  More managible than Liquid Oxygen for instance.

So, I guess the people that built this:
http://www.space.com/23648-new-rocket-e … video.html
Probablly have all those notions.

As for spacecraft shielding, I would say that your fuel tank for the Paraffin could be a tin can with a flexible bag inside.  As you use up the fuel,
you loose some of your shielding, but you create more interior space (Inside the flexible bag) that people can use.  The wax would be held between the tin
can walls and the bag.

So a mission could start with a capsule, and a totally filled Paraffin Wax tank, and then on your first burn, that would hollow out, and you could put
your sleeping quarters in it, and move some of your controlls into it.  Thereby having more space to use.

Then the insertion burn, would consume much of the balance, and you would either land the capsule to the surface of Mars and have protection there, or
if you had enough fuel you would land the whole thing, depleating your on board supply of Paraffin. 

If staying in orbit, you could refill the Paraffin tank from Paraffin blocks put in orbit by a previous supply mission (Such as an electric rocket),
or could refill them from Parraffin blocks hard landed at your intended landing site.

Could you have sent a robot to manufacture Nitrous Oxide from the Martian atmosphere also?  I am inclide to think paraffin wax would require a developed industrial base, and could not be done automatically by robot lander.

#8990 Re: Martian Chronicles » Developing Saturn » 2013-11-20 12:57:52

I think it is supposed to be a percentage of the planets size if it is formed from the planets disk.  1%????  Couldn't find the reference, any query for moon brings up our Moon.  So the bigger the planet, the bigger the moon mass.  However if Jupiter had one big moon instead of Io, Europa, Ganeymede, and Callisto, maybe that would be getting substantial.

But a planet many times bigger than Jupiter might do much better.

Then there is our moon which did not form that way apparently.  I have my own rogue notion of how it formed, I think it was condensed from the Earths spare material first as a wet object, and then was added to by rubble from impacts with the Earth.  I think that is why there is evidence of magmatic water.  I will not duke it out on that speculation however.

Then there is Triton, where it is thought it was captured.  Most likely method, was that it was a binary object, and it's partner was either ejected, or impacted Neptune.  So, maybe if you have a chaotic system forming with binary objects changing orbit, you could get a more substantial moon than if it
was a condensed moon, but it appears that that is not a common occurance.

#8991 Re: Interplanetary transportation » Beamed Propulsion Trajectory » 2013-11-18 14:55:36

GW I like it also.  Also perhaps even more if explosive materials could come from the Moon for some space activities.

Yes Josh, your arguments have merrit, but look what happened.  GW did a good one.

We do have bad natural chemestry togeather, so small doses maybe.  I am vacating this thread.  Have fun.

#8992 Re: Interplanetary transportation » Beamed Propulsion Trajectory » 2013-11-18 11:13:37

Why?

As a laboratory for the development of instrumentation.  Just because it is not good enough now does not necessarily stop it from being improved.
First you perfect your instrumentation, your laser point system.

FYI (Strike GPS, substitute, Local Postioning Systems/Instrumentation/A camera on the rocket looking at Eor, owl, Christifer Robin, and Poo Bear waving flags on the ground.)

Then bring back GPS, because it may still be useful at some point bring it back as a future better GPS.

And if you tell me that it is impossible to point a laser at a machine, then of course it is impossible to
communicate with a spacecraft orbiting the Moon.
http://www.space.com/23308-nasa-moon-la … ecord.html

Then the chemical rocket as a laboratory to study the transmission of power by energy beam to a moving object.
Laser, use the more generic “energy beam” phrase, which also allows lasers).

A chemical rocket is a moving object and moves similar to how a moving object projected by an energy beam might move.
Therefore you can build a very small scale version (Laser pointer) to test the process and define it's potential.  If the results seem positive, you can scale it up by increments as far as the reality of physics and economics will allow.

It is possible that you would eventually eliminate the chemical rocket characteristic and then have an energy beam only method, but as far as I am concerned "Why would you want to do that?".  An energy beam to project a machine upwards still needs working mass, which you must either carry with the machine, or draw from the atmosphere.  Drawing from the atmosphere comes to fault where it gets too thin.

So, if you are carrying mass in the machine for the beam to heat up, and you have a choice for that mass to carry chemical energy with it.  Such machines have already been made (Chemical Rockets).  So you have this mass which can be burned to produce thrust, and you can also project more energy into it.

As for engines not being tolerant of this, I said "I don't think existing engines could put up with this very well".  Then you told me that  "A space shuttle engine would not put up with it very well".

I say again true, that is my expectation as well.  But of course do the experiment on a very small engine.  One that can be throttled back.
Throttle it back, but try to bring the thrust level back up by adding energy from a power beam.  Is the engine going to perform well?  No it is an existing engine which was designed for a specific purpose.  However, you might learn something about designing an engine that could operate in both modes.

Mode 1: 100% chemical energy for situations where the power beam failed or was not convienient to use.

Mode 2: 50% chemical energy + 50% power beam for situations where the power beam was on line and functional.   I have previously stated a limit of 5,000 to 10,000 feet, but that was arbitrary, maybe it works 5,000 to 10,000 feet and you want to attempt to expand it upwards.

Why is this worth doing?  Because you might conserve propulsion mass if Mode2 is functioning well, and be able to bring it up to orbit along with your other payload.  It might be worth a buck or two, should it be possible to apply it to a value added service.
And finally it has been stated by that guy that owns space X, that the hardware is more valuable than the fuel.  And so they are trying to figure out how to recover booster stages.

The scheme listed above also has the potential to recover the hardware by either getting it up to orbit, or landing it on the surface of a world.

If it is power beam alone, I have a hard time figuring out what the abort modes exist that could recover the hardware.

As for economics, it seems that I have to jump through that hoop more than anyone else (Or maybe that's just my perception).

Could you get your fuel from the Moon cheaper?  Maybe, but then you could also use a hybrid system to get it to Earth orbits, conserving the finite amount of such fuels that can be gotten from the Moon.

Is it the only and best plan?  That is not proven at all.  I did use the word laboratory, which implies testing.  It would have to pass quite a few tests, to displace other methods.

But keep in mind that my objective was to transfer an idea to other minds, and I have done that so, it really does not matter what further reply I get on this. 

I expect I will vacate this thread, at least for a while, and so keep the peace, even so, thank you for your time and input, and I really and truly hope that you outdo lasers  with your power beam concept.

#8993 Re: Interplanetary transportation » Beamed Propulsion Trajectory » 2013-11-15 11:23:00

Here is a reference to that GW:

http://en.wikipedia.org/wiki/Beam-power … ed_systems

http://upload.wikimedia.org/wikipedia/c … tcraft.jpg

I guess I will continue even though it is above my level

For a pulsed laser;
1) Have the rocket communicate it's position per gps on a continuing basis. Also send other information such as how atmospheric conditions (wind) are affecting the path and future predicted location of the rocket.
2) Analyze the atmosphere for twinkle per a low powered signal laser as is done for astronomy
3) Alternate pulses.  First a signal pulse to confirm pointing is good, followed by a power pulse, if the results are confirmed as good.

In the case of delivery to a non-chemical engine, it might be possible to fine tune the reciever with actuators, to displace it an inch or two.

By this method successful delivery of power pulses would be facilitated.  As it would be a chemical rocket intended to go to orbit if necessary without any successfully delivered power pulses, missing out on some would not be a problem.

Also, if the duration of a pulse were short, the actual delivery of a power pulse to a unintended part of the rocket might be survived, because actual damage might require a long set of power pulses being delivered to the wrong spot over a short period of time.

Of course the higher in the sky you got, the longer the communication time lag, which would make it harder, so for this reason (And others) there would be an altitude and distance limitation to it.

#8994 Re: Interplanetary transportation » Beamed Propulsion Trajectory » 2013-11-15 09:12:43

Void, you may not agree with me-- and that's fine!  I'd encourage you to state your disagreement if you don't agree, because I'm far from being right all the time.

OK, thats fine, it's better to find truth than to continue in ignorance.

However, if beamed power with lasers has any merit, then would it be possible to beam power to an attachment intended for that purpose, and not a rocket engine?  Then having the hybrid capability that way.  Of course the beamed power must be able to lift the attachment, and to make it worth anything it must provide a surplus of lift to add to that of the rocket.

If you are completely negitive to this then I would have to conclude that beamed power by laser is not a possibility.

Supposing that lifting a device with lasers is theoretically worth considering;
I will point out that if beamed power to a device without a chemical (Or altenative) lift has it's own problems.  Clouds for instance.

But yes any device which has not been produced yet has lots of unknowns, and I am sure that there was a time when many people thought that chemical rockets could never do what they do now.

#8995 Re: Interplanetary transportation » Beamed Propulsion Trajectory » 2013-11-14 15:06:18

Really no idea about the mass.  I was just hoping that existing engine designs could be evaluated on a testbed while firing, and that shining a modulated laser into them would reveal how they would have to be modified to tollerate it.  I am sure they are all tuned for a certain power limit before failing, so I would start by adding 1% extra power with a laser beam, and then move it up until the engine showed stress.  Then you would have to figure out how to redesign the engine to tollerate operating in both modes.  Chemical only or Chemical + Laser Boost.

Of course you would have to figure out if it actually gives more thrust.

I am not competent to give a added hardware weight evaluation.  Of course that has to be considered.

A Oxygen + Hydrogen flame is transparent I belive (To visible light), so I would suppose that you would need a wavelength which would be absorbed by very hot steam.

If it was a solid rocket then you would need something else.  I don't think I would persue it with solids though.

Also you would have to figure out your aiming.  I suppose that for a altitude of 0-10,000 feet, that might not be impossible, but then you have to consider what damage it might do to the rockets other parts, if the aim is wrong.

I Don't know if you would use solid state or chemical lasers.  Chemical Lasers can be pretty powerful, although as used in aircraft, they have issues, but they exist, and have been tested.  I am sure we don't want something so powerful that it can knock down a ICBM though.

As far as aiming it is favorable that the lasers and the rocket would be co-operating with each other, unlike using a laser to intercept a ICBM.

These would be ground based I would think.

#8996 Re: Terraformation » The Case for Titan » 2013-11-14 11:13:21

You have caused me to wonder if the following could be done:

Place a honeycombed floating shell in the mostly N2 atmosphere of Titan, so creating multiple zones, (1) the atmosphere above the honeycomb shell,
(2) the atmosphere below the honeycomb shell, (3) and of course a multitude of enclosed chambers incorported into the honeycomb shell.

If greenhouse gasses which will not consense could be pushed into zone 1, then below that could be kept as vaporized a significant amount of Methane,
as a further greenhouse gass.

Presumably the (3) honeycomb shell chambers could be partially filled with Helium for flotation, and if they were warmer inside that would also aid flotation.

Heat directed into zone (2) would eventually melt everything to an ocean, and also likely release a huge amount of hydrocarbons, which would have to be
mechanically moved to zone (1).  In zone (1), those hydrocarbons could be exported from the world, and hopefully sold to a buyer.  This would eventually allow a N2 atmosphere in zone (1) and a N2/O2 atmosphere in zone (2), but you would want to make sure that the amount of combustable gasses in zone (1) was kept below the flamable limt, in case zone (1) and zone (2) atmospheres got mixed.

Eventually when the ocean of Zone (2) existed, a very large amount of hollow floats made of plastic could be dropped into the ocean.  They would have
anchors for plants to root onto, and would likely collect into rafts.  Bog plants modified could cause them to become floating islands.  Of course
zone (2) would need artificial lighting for bog plants to grow, but then as much of the ocean as was desired could be covered in this manner.  I believe
that normal plastic objects can persist for quite a long time.  A method would be required however to keep them from becomming waterlogged over a long
period of time.

If zone 2 were to have a temperature near freezing in the areas of bog, then it could be a floating permafrost bog.  Otherwise at elivated temperatures
where trees grow on the floating bog, it still might be able to support the weight of a person, especially under a .1 g (Approximately) situation.

It might be possible to have one hemisphere as tropical, one as arctic, and a transition band of temperate between them.  For the arctic hemisphere,
then it would be required that the honeycomb shell above that area would not be heated on average above freezing.  To allow ice to form, the lights would
be turned off periodically.

Minerals could be extracted from the water, although the core is likely surrounded by several types of pressurized ice I speculate without proof,
minerals from the core may travel to the water ocean if cyro-volcanism occurs in that pressurized ice.

#8997 Re: Interplanetary transportation » Beamed Propulsion Trajectory » 2013-11-13 11:19:39

OK, I am going to presume that you are correct on the condensation thing, and give it up.

But as an ending I will suggest that a hybrid propulsion method as suggested previously "Might" be useful.

What I am speculating on is that the chemical rocket would be fully capable of orbit without the assist from the laser, but if assisted by the laser might achive orbit with fuel and oxydizer left over.  Supposing that that leftover could be handled in some manner to be stored, then it would be an orbital resource.

So, if the laser system failed during launch, from technical or atmospheric issues the rocket and payload would not necessarily be lost.  But if a laser assist was successful, then leftovers for orbital activities.

#8998 Re: Interplanetary transportation » Beamed Propulsion Trajectory » 2013-11-13 09:00:52

The de-condensation process could stop at the point where the fueling apparatus was disconnected, so it would not be that bad of a problem since any increased venting could be topped off.  I also think that the heating would be more of a zap type of a pulsed thing, scanning across the tanks to inhibit buildup.  Some wavelengths are particular to ice, but conduction would put some heat in.  But it is not a priorty, just an option to inventigate.

I actually only think of using the laser to engine coupling for the first 5000 to 10,000 feet, just to see if any good could come from it.

Of course long before committing to such a thing you would do an experiment with a small engine on a testbed, to see how this works, the problems it creats, does it give a benefit?  Also in fact what are the additional costs in modifying the engine, and in the laser system itself.  Of course it has to pay it's way.

#8999 Re: Interplanetary transportation » Beamed Propulsion Trajectory » 2013-11-12 07:02:03

Well thank you for responding, I did request it.

I do not want to interfere with the path that you want to take with this thread, but I will at least argue for a short time on some of this.

I consider your arguments to be valid from a point of view, but also see another angle or two.

As for removing condensate, I think that could be accomplished with a certain wavelength of light, pulsed lasers, which would not heat the cryrogenic fluids very much at all, during the time the rocket is not in flight.  The value is debatable.

As for the notion of actually heating the tanks intentionally during flight with a laser, for a rocket constructed with that intention, it could be beneficial, since during flight fluids are being directed to an engine where they are intended to become very hot.  It would simply be needed not to overpressurize the tanks to a failure.  It would be a laser powered steam engine effect more or less.

The updraft thing is very weak, and likely is not worth the persuit, but is interesting to think about.

As for shining laser beams into the inside of a running rocket engine, it would likely produce a greater push, with the same amount of mass, but could damage engines intended not to operate that way.

As for the argument against combining two powerful technologies, I will say that their was a transition between sailing ships and steam ships where both technologies were used, and that may have made it possible to develop steam engines for ships in the first place.

If any hybrid method could deliver extra amounts of payload to orbit for a reasonable added cost, then I think it can be a continuing consideration.

Cost would be the test.

#9000 Re: Space Policy » Newt Gingrich » 2013-11-11 14:05:38

See the movie "Cloud Atlas" perhaps.

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

Board footer

Powered by FluxBB