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This video makes some claims that might have importance to understand: https://www.bing.com/videos/riverview/r … 23b4a504dc Quote:
SpaceX Starship: ABSURDLY Overpowered! 100 Tons to Mars WITHOUT Refueling
YouTube
Future Space
2 vi
I am pasting it here for further considerations.
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Isaac Arthur has some important information in: https://www.youtube.com/watch?v=y47MMNq … saacArthur Quote:
Moon: Industrial Complex
Isaac Arthur
811K subscribers
At "1.5 minutes inside the video", a description of the fuel needs Earth/Moon to lift a load off each world. The evaluation has to do with Hydrogen/Oxygen propulsions. 12/.7 is the ratio given, and may involve the Hydrogen in the evaluation.
So, I think that to get Oxygen to a Starship, the Moon may be the best deal. But that depends on things like labor sources, and where the Starship is located. If it is in LEO, then you have to bring the Oxygen from the Moons orbits to LEO. That is an additional effort and cost.
If you could get the Starship to a Lunar orbit, then perhaps the loading of Lunar Oxygen would be considered reasonable economically.
So, one way to do that would be to fill the Starship in a filling orbit of the Earth with only enough Oxygen to get to a Lunar Orbit, but with an abundance of Methane.
Another option might be to bring Methane to Lunar orbit using an Electric Rocket.
Methane or Carbon delivered to the Moons surface could be used with Solar Pyrolysis to extract Oxygen from Lunar ore.
I agree that water at the Lunar poles may be a massive prize, but depending on how much there is, and how hard it is to process, it may be wise to reserve it for use on the Moon.
But if you could land Carbon on the Moon, you might use Solar Pyrolysis at the Equator to extract Oxygen as CO2.
Then to extract the Oxygen from the CO2, and launch that to Orbit from the Equator which has an advantage to getting it from the poles.
You could either get Carbon or CO back out of the CO2 you produced and use that again to do Pyrolysis on more Moon regolith.
From Post #9, from post #6: Quote: (From post #6):
https://www.reddit.com/r/spaceflight/co … ?rdt=46570 Quote:
It has a 5-meter diameter, and a Vacuum Archimedes engine.
https://www.rocketlabusa.com/updates/ro … hitecture/
Quote:Designed as an expendable upper stage for now, Neutron’s second stage is a six-meter-long carbon composite structure with a single vacuum optimized Archimedes engine.
Image Quote:
Using something like Neutron's 2nd stage if you put Carbon landing legs on it, and if its engine method could be made suitable for a Lunar landing, then you have the remnants of the Methane Fuel, and also the Carbon of the tank and the Carbon of the landing legs to work with.
Some metal parts like engines would have value. So, if you could fill the tank with a maximum of Methane practical, and the just necessary amount of Oxygen to land with a margin, you might have a source of Methane to make water with, and a larger source of Carbon for the pyrolysis of Lunar Regolith.
If a version of Superheavy from SpaceX, could be modified to do the Neutron process, then very large sized versions of Neutron 2nd Stage could be launched to LEO, for similar reasons. To carry Methane and a minimum amount of Oxygen necessary to go to the Moon and land at the Equator. The tanks and landing legs to be cannibalized for the pyrolysis of regolith. As I have said, a remnant Methane delivered could be processed into water using Lunar Oxygen, and the Carbon of the Methane could be used in more Pyrolysis of Lunar Regolith.
What would be done with the metal parts is open for debate.
You would want a constant input of more Carbon to the Moon and a little Hydrogen, as the Pyrolysis process will not be able to recycle the Carbon with 100% efficiency.
Eventually if electric propulsion matures, it might be used to move the Carbon Tanks with Carbon legs and an engine(s), to Lunar orbit from LEO.
That might make it even more efficient fuel wise.
I would still suppose that efforts could be made to access the resources of the Lunar Poles, but this equator method might have it's own justification to exist.
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A subsurface spin gravity habitat might be possible to work in some various ways. Not guaranteed, rather I sense that it may be possible.
The ice caps of Mars are typically regarded as too cold for habitation. But then people will go ahead and suppose that humans will want to inhabit other very cold places, such as Ceres, Callisto, and Titan for instance.
It occurs to me that if you want the opposite of a lifting gas, CO2 cooled to near its condensation point should be a fluid that is perhaps able to allow floatation of a hollow object with a greater buoyancy in side. The Martian Ice Caps may provide that level of Cold for a reasonable price, I think. And of course the atmosphere of Mars being dominantly CO2, it is very available.
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I have made some changes. Again, I only think this might be close to possible, but in a test of reality may need more innovation: 
In order to have the desired Helium, it may be necessary to have fusion power plants. But such power plants would also be valuable for the power they would produce, not just the potential of Helium.
The Helium Oxygen mix would be breathable in an emergency, and would also be tolerated by robots. And of course where I have suggested, a cold CO2 gas for the "Rotor" to float in, the Helium would make the "Rotor" more buoyant.
I will admit that if the floatation CO2 gas is very cold, and the "Rotor" not too cold, then some type of lightweight insulation will be desired.
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So, we would not want the flotation gas to get cold enough to solidify from the gas phase:
https://en.wikipedia.org/wiki/Carbon_dioxide
Quote:
194.6855(30) K (−78.4645(30) °C) at 1 atm (0.101325 MPa)
So, the polar ice caps might supply something not quite that cold, I would hope.
https://en.wikipedia.org/wiki/Martian_polar_ice_caps
The North Ice Cap is said to be about 2km thick, the South Ice Cap is said to be about 3km thick.
As far as ice column pressure this should be 1/3 that of the Earth, for similar thicknesses.
Could we drill all the way down to the base of the ice, and have a cylinder? Could we have a substance with enough compressive strength to hold the ice from squeezing the hole shut?
(North=1.2427423845 miles), (South=1.8641135767 miles)
If one of these could be built in a way that works, then it should be possible to make many, many of them and to have passages to join them together.
The lids on theses could be domes covered in a synthetic pykrete, with enough weight to hold in the internal CO2 air pressure.
Enough for now.
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I am interested in playing some mind games for Mars. I have done some of this elsewhere elsewhen, but I have more of it now.
I have begun to wonder if we could think of spinning habitats that could be inside of enclosures on Mars. Japan has a concept of something like that for the Moon. Japan has a different imagination than in the USA, but that is a good thing:
https://space.innovationkyoto.org/2024/ … 4/?lang=en Quote:
Kyoto University and Kajima Corp. Joint Study on the Feasibility of an Artificial Gravity Residential Facilities on the Moon —A Step Towards Realizing Artificial Gravity Residential Facilities—
By space
So, that gives me a little permission to think of similar for Mars.
Dr. Zubrin and many others frown on the idea of "Building Worlds", and he sees Mars as the most practical major objective, I believe. However some others support "Islands in Space", and some others who I think regard working persons as servant class, who should only be concerned with worshiping their proclaimed brilliance.
It is not as though each viewpoint is entirely wrong. But what if we could do "Islands in Space", under the surface of Mars? I suggest that the air it floats in is not going to spin all at the same rate. The floating cylinder could be called the "Rotor", and we can call cylinder in which the air is compressed, in which the "Rotor" floats, the "Stator".
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Rock is very hard to hollow out, so I am going to suggest ice caves.
Here is an ice slab, that I have looked at before, there are others that are not so far away from the equator, but this one is plain to see. And anyway, if we are to see Mars inhabited, I expect that various nuclear power schemes will be employed. https://en.wikipedia.org/wiki/Korolev_(Martian_crater) Image Quote:
Quote:
Korolev crater is located on the Planum Boreum, the northern polar plain which surrounds the north polar ice cap, near the Olympia Undae dune field. The crater rim rises about 2 kilometres (1.2 mi) above the surrounding plains. The crater floor lies about 2 kilometres (1.2 mi) below the rim, and is covered by a 1.8 kilometres (1.1 mi) deep central mound of permanent water ice, up to 60 kilometres (37 mi) in diameter.[2]
Can we think to remove a 1.1 mi deep cylinder of ice, and put a roof over that? I don't really think we have to do that deep but this is an imaginary exercise.
By the same notion that we could float a habitat in the atmosphere of Venus, I propose this vision: 
Now, can we spin it? Yes, but what are the consequences?
I looked and got the notion that an O'Neill Cylinder at its perimeter might travel at 400 miles per hour.
https://en.wikipedia.org/wiki/O%27Neill_cylinder
I have information that says that a 747 might reach speeds of 600 to 660 mph.
So, not impossible to tolerate. I assume that a factor desired is not to break the sound barrier, or nasty stresses would be introduced that are not desirable.
But that speed would be in a thinner atmosphere, so maybe lets drop the air pressure down to 1/3 bar to approximate those conditions. We will have less buoyancy but also unlike as in a Venus Cloud habitat, you do not have to have all the heavy equipment for the economics on board of the "Rotor".
Now, what if we put wings on our rotor to produce additional lift?
We also may have the option of magnetic levitation, should that be desired to employ.
Now since we are on Mars, ~1/3 of the gravity is already supplied. So we only have to provide a maximum of ~2/3 of a g force, so we can slow our "Rotor" down somewhat.
Energy consumption and heat accumulations will be a concern. However, this "Rotor" essentially is riding on an air bearing, so the heat of friction should not be as bad as might be feared.
https://wp.optics.arizona.edu/optomech/ … ichard.pdf
Quote:
Air bearings can provide effectively zero friction, do not require lubricants, and do not wear. They provide high stiffness and higher damping, while allowing higher speeds with smooth and practically silent operation.
The above might be somewhat true, we can hope.
As for heat accumulation, a heat pump can extract heat from the "Stator" air and dump it into the "Rotor" air, and from the "Rotor" the heat might be radiated outside.
Or the heat from the Stator, heat might be disposed of to the outside by various means.
In the case where the rotor shell should rupture, then Oxygen masks would be wanted. Or the ability to move to more protected areas. The pressure in the interior of the "Rotor" might be 2/3 bar of N2/O2, so that the poisonous atmosphere of the "Stator" will not enter.
The interior of the devices should be rather well protected from radiation concerns. And the "Rotor" might achieve a maximum real + simulated gravity of 1 g.
So, possibly not a bad deal, and maybe much better than building orbital habitats, although I would opt for a few of those as well orbiting Mars.
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A video about Rocket Lab and Neutron, as it happens: https://www.bing.com/videos/riverview/r … cb0c9c120f
Quote:
ROCKET LAB Makes Major Breakthrough That Shocks the Industry! Spacex Blue Orgin Reacts
YouTube
NR Studio
So, I also think that they have some potential going into the future.
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I realize that it is a long shot, but if landers could be made of 2nd stages of Neutron, then perhaps an opportunity would exist to incorporate something like a modified Dragon, or maybe even an Orion capsule, to make a method to land on the Moon and ascend. I would feel more comfortable if this were supported by a Starship in orbit of the Moon.
But either capsule then might be able to do the return to Earth from Lunar orbit.
I will claim that this would align just a bit more to what Dr. Zubrin has recently suggested. It is not a Starboat, but maybe a poor mans method to get something done by reusing existing or soon to exist hardware.
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I am reading of impressive progress on the SpaceX Stainless Steel Structure methods, but I am also developing an interest in the Rocket Lab Carbon build method.
I would not for any reason argue to pick one and put down the other. These together could go a long way towards space capabilities.
https://3dprintingindustry.com/news/3d- … er-233751/ Quote:
Aerospace
3D printing ‘World’s Largest’ carbon composite rocket on Rocket Lab’s 90-ton 3D printer
Alex Tyrer-Jones October 21st 2024 - 4:58pm 0 0
Quote:
According to Rocket Lab, while it takes several weeks to build a stage 2 dome using conventional, manual methods, the AFP machine can produce one in just 24 hours. The company anticipates it will save over 150,000 hours when constructing rocket structures with AFP technology.
Quote: (From post #6):
https://www.reddit.com/r/spaceflight/co … ?rdt=46570 Quote:
It has a 5-meter diameter, and a Vacuum Archimedes engine.
https://www.rocketlabusa.com/updates/ro … hitecture/
Quote:Designed as an expendable upper stage for now, Neutron’s second stage is a six-meter-long carbon composite structure with a single vacuum optimized Archimedes engine.
Image Quote:
The Stainless Steel, has its advantages, but I would be very interested in Carbon build for Lunar activities.
So, I am thinking that for a Lunar Lander, these might have merit. A crash or onetime use to land on the Moon would leave behind useful materials like Carbon to be recycled on the Moon.
It might even be worthwhile to lift them to orbit using Starship.
I don't have the specs for these things so I cannot be certain, but I would guess you could build landers with 1, 3, 5 or maybe more of these 2nd stage units incorporated. A 2nd Stage unit in a centered position, might be gimbaled in order to assist in landing capabilities.
Such landers might be supported by a Starship in orbit of the Moon. Perhaps refilled in Lunar Orbits or not. Maybe the landers would see a one time landing of some hardware or consumables.
Just a capability that may be of use.
And then perhaps as a joint project perhaps SpaceX and Rocket Lab could make a much larger version of the 2nd Stage, that could ride up on the Superheavy, and perhaps that Superheavy might be modified to have the Hungry Hippo method of Fairings, like Rocket Lab's Neutron.
Some rather interesting landers for the Moon might be fabricated from that setup, I think.
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So, I like to imagine a future of good progress.
I think that both concepts of durable Stainless Steel and then also lightweight options such as Carbon structure are going to be good, and maybe even better in combinations.
But even then there are many wild cards which may shift the path of the future from what we may expect to other things. Ideally to better things.
I can name Dream Chaser, and advance robotics as being some of the emerging wild cards.
The Dream Chaser can provide a special service that neither SpaceX or Rocket Lab can provide at this time.
While we may imagine a growing population on Mars and some other worlds, for the moment I think the best path for animated structures in orbit and the Moon favor an expansion into robotics. But of course even on Earth we are going to wan to have greater amounts of low-cost robotic labor.
And many other things may show up.
We have chances of a great deal of a great deal.
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I guess I am doing wish lists. Things I might hope could appear.
I think that SpaceX and Rocket Lab could collaborate on some things, a frenemies more or less.
In the previous post I suggested reuse of Neutron 2nd Stages.
There is something, that I think that SpaceX might eventually do, if they have large enough sea platforms. But I think that Rocket Lab, using Neutron 1st stage, might do it much sooner and work out the kinks.
Rocket Lab now intends to catch Neutron 1st stage on barges. It has been my notion that rather than bringing the barge back in the thing to do would be to refill the Neutron 1st stage and fly it retrograde back to the original launch site. So, the barge it landed on would need means to refill the Neutron 1st stage. Methane and Oxygen, I believe.
The Neutron 1st stage retains it's "Hungry Hippo Fairings", so it would be streamlined to make that flight, but without a payload, it would not need a full refilling to do it.
I have to wonder if eventually Starship Superheavy could have a version that would have "Hungry Hippo Fairings" as well, and that a Carbon Starship could be fitted inside, as a 2nd stage. It would not be intended for atmospheric entry, but might work very well for the Moon, and maybe asteroids.
Superheavy, being Stainless Steel, apparently does not need much for heat shielding. And making a Carbon type Starship to send to orbit and not to land could have benefits.
Obviously, it would have less inertia.
It is worth mentioning that Carbon is a substance that will work with the Neumann Drive, if that ever gets sized up.
So, technically a Starship converted to a sort of Neutron Ship method, might be able to feed an electric rocket propulsion device. I am guessing that Carbon might be easier to convert to propellants for a Neumann Drive than would be Stainless Steel.
And I am not putting either company down. Each has come up with impressive technology that I fell might work together in some cases, to produce a significant benefit.
If it were to be air braked to Earth Orbit a "Overshield" of Lunar Materials might protect it. Otherwise the Carbon being of less inertia than Stainless Steel the inertia will be less. Indeed, if Neumann Drive were sized up, then such Carbon Ships could be brought back to Lower Earth Orbits by using electric rocket drive. And then to refill from a depot and perhaps lift significant cargo to a higher orbit or to the Moon.
This is "Food for Thought", I feel. If Carbon can be used for propulsion then the ships could eventually after a full service life end up being salvaged to make propellants for other Carbon Ships.
Of course the Raptors and other parts could be recycled.
Neumann Drive: https://neumannspace.com/
A Carbon Starship of the type I suggest would not have heat shield, or Flaps or Motors, which should drop it's price.
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I have been thinking about NEUTRON, 2ND STAGE.
They cannot return to the surface of Earth on their own. However, do they have further potential for value?
I suppose that Starship could bring them down, or they could be refilled to a new purpose in orbit.
Easy to say, but to repurpose them, I anticipate that an efficient way to move them to a centralized position in orbit may have value. I suspect that the use of an electric rocket tug would perhaps be justified for that purpose.
https://www.reddit.com/r/spaceflight/co … ?rdt=46570 Quote: 
It has a 5-meter diameter, and a Vacuum Archimedes engine.
https://www.rocketlabusa.com/updates/ro … hitecture/
Quote:
Designed as an expendable upper stage for now, Neutron’s second stage is a six-meter-long carbon composite structure with a single vacuum optimized Archimedes engine.
Image Quote:
The device is light weight and the engine is supposed to be durable.
After it has done it's work, it may not be in a convenient orbit. However, I think quite often the practice is to dump such a stage into the atmosphere to burn up.
The hope is that Starship could support an electric rocket tug to retrieve some of these to a reuse situation.
Starship could probably refill a modified version.
Granted it might be more complex than desired, but these things might be ganged together and refilled to use to send a payload somewhere, I think. Serial, or Parallel, or Wheel.
This would be a two rocket propulsion wheel: 
So, many more could be attached. During a mission 2nd stages could be expelled or held. They would be lost if expended, but if it were desired to reuse them then they might be retained, and the whole assembly would go back to a refurbishment point.
So, I do not guarantee that this is a wise plan, but at least I took the time to review the potential.
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The idea that humans are Carnivore, is surprising. The medical community does not prescribe that today.
https://www.bing.com/videos/riverview/r … &FORM=VIRE Quote:
Humans Are Carnivores. But One Fatal Mistake Changed Everything.
YouTube
Max German
6.7K views
2 days ago
The idea that brain size has become smaller due to farming is something to ponder. This could suggest that humans have been experiencing brain starvation since the end of the ice ages.
I have not viewed this one yet:
https://www.bing.com/videos/riverview/r … &FORM=VIRE
Quote:
Humans Are Carnivores. Here's Why
YouTube
Max German33.7K views
If there is truth in this we may want to find a way to get the nutrition of animals, without having to kill animals. I would like to get away from killing animals, but am not against eating meat.
There could be a pathway in lab grown meat, but maybe somehow some form of Precision Fermentation could give us food without the problems that come from plants.
I am still confused as to why the meat eating humans were healthier and had bigger brains than the agricultural humans.
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A very unproven theory from me is that plants may have some methods to get nutrients from animals.
A fairly direct way would be for a tree to take a form that birds might like to perch in. My notion is that bird droppings would be useful to some trees. So, a stationary or "Planted", life form would solicit assistance from an animated life form such as a bird, or perhaps a bat. The distribution of seeds from fruits and such also could figure into this.
We are familiar with carnivorous plants as they are so unusual, but animals also distribute nutrients "Upstream" though Feces and Urine. In the case of the birds, those are combined. Usually, nutrients wash downstream. But of course, the wind as well could carry some nutrients upstream.
It is less clear to me how things work with land Herbivores and Carnivores, as relates to land plants.
So, plants are ambivalent about animals perhaps. The want to discourage being eaten for the most part, but fruits and flowers are attractants, for pollination, seed distribution, and possibly receiving Urine and Feces.
Another distribution of nutrients could be from dead things, blood, and perhaps vomit. But my speculation is hesitant on how that would be encouraged by plants. Perhaps in some cases perhaps not.
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Referring to the previous post, not a bad plan, but I think that covered canals such as have been mentioned where Hydrogen would be injected to dissolve in the water, would also absorb CO2 and O2 and N2, from the atmosphere, and along with other nutrients should allow the production of large amounts of biomass.
In some cases, perhaps food from air and energy.
And some setups may be able to extract water from the air at the same time.
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I will work on this later. Thanks British! https://www.msn.com/en-us/weather/topst … r-AA1DaZo3 Quote:
4 billion tons yearly: UK starts sucking carbon from sea with floating solar power
Story by Prabhat Ranjan Mishra • 9h •
2 min read
Obviously this is going to be useful in the canals that I have suggested.
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A little bit of swearing in the very beginning, from the guy in the red coat. So you can silence that if you like.
https://www.bing.com/videos/riverview/r … &FORM=VIRE Quote:
Utube, Anthrofuturism, Lunar Transportation Infrastructure (Sintered Regolith Roads & Nuclear Power
40:12Lunar Transportation Infrastructure (Sintered Regolith Roads & Nuclear Powered Trains)
YouTube
AnthroFuturism
6.1K views
Some hope of delivering Oxygen to Low Earth Orbit from the Moon, so interesting.
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I think that this might involve solar panels being more of a structural material themselves.
There is no telling how much natural light is needed to signal plants to grow appropriately.
I am hoping for something like 5% maybe. So, although the dome or continuing archway, might be a little bit like a greenhouse, it would be more of a solar power collector.
We can hope that plants will be bioengineered, to work more with Acetate as their energy source.
Of course, if desired, some artificial lighting could also be included instead of windows, so that the plants can be convinced that the season is different than what it is. Again, you might hope that this would be a tiny minority of the energy needed by the plants.
And then this may lead to a question of if it is good to have classical greenhouses on Mars, or to do some alternative such as suggested in this post.
Acetate is supposed to be more efficient than photosynthesis. But plants are not yet adapted as well as needed to use Acetate.
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I hope I will not annoy you Calliban.
Can you speak to any method to turn an Orion propulsion system into a reactor?
I have some notions which may have a small chance.
For instance, it is obvious that if you had an ice body which you did not mind contaminating, you could periodically set off
nuclear bombs, to store heat into water. There could be places on Mars for such. Korolev Crater for instance.
But that is not what I want to ask about, it just indicates that a pulsing nuclear reactor based on actual bombs might be possible.
What I have in mind is a metal shell, with a thick inner liner of Carbon. Vacuum within.
Upon setting off a bomb, it would be more like setting one off in space. Heat and Magnetics I presume. Not so much of a pressure wave. So, I anticipate some of the Carbon vaporizing immediately before the blast wave hit, so that would cushion it as the Carbon Vapors would be pushing towards the center of the sphere, and the blast wave would be pushing outward from the center.
Carbon is hard to come by near orbits of the Moon, so maybe Silicon would work?
The Vaporization for both is at a very high temperature.
The infrared from the explosion should mirror back to the center early in the explosion as the shell would act like a mirror.
It is possible that the sphere would need to be wrapped in space elevator worthy cables of some kind.
Obviously the bigger the shell, the more it could tolerate a nuclear explosion of this sort.
As I have said, in the starting circumstances before the explosion there would be a fairly substantial vacuum inside of the sphere.
Methods to tap the supposed stored heat, and then to get back in to put another bomb in will need some creative thinking.
Thanks for your tolerance, in advance,
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Returning for a bit, I am wondering about solar power orientations. We have somewhat horizontal to face the sun, we have vertical, and we have sun following.
Here are some simple representations: 
As it happens the Dome or Arch is actually like the Bifacial, but with a hollow inside. It is also like the sun orientation as, part of it is pointed to the sun as well.
This may be like a combination of types and may round out the power production more around the day. Bifacials are better in Morning and Afternoon. Semi-horizontal are best at noon time, I believe. Also, some orientations may be better for light bouncing off of clouds on a cloudy day.
If solar panels were put on all surfaces of a Dome or Arch, then the North side, in the North Hemisphere, would only get light bounced off the clouds or the ground. The exception would be, if you involved heliostats to purposely convey more photons to an area of a Dome or Arch.
Solar panels at this time provide some protection for animals, more in the case of non-vertical ones. They all, may reduce evaporation from the ground.
But a Dome or Arch, may do similar but even better. You could use such as animal shelters or perhaps grow things inside. I have suggested Precision Fermentation before, but if it becomes practical to grow plants in the dark with Acetate, then this also might be tried. The Dome or Arch may extend the growing season.
But you could have some windows, or transparent solar panels to allow a little light to get in. That could be important for many plants, to get their seasonal signals from.
But of course such a structure may be vulnerable to burrowing animals on Earth at least.
The idea that a roofed over volume can be incorporated into a solar power system has some value, we already do it with houses. But the variable orientations of the panels, would reduce the energy storage needs, I expect.
Depending on cost of solar equipment, you might have 2, 3, 5 times as much solar panels as you need for peak power. That would be if you go along with Tony Seba's "Superpower" notions.
If you could use excess Superpower to make Acetate, then that would be one route to take.
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The direction SpaceX expresses at this time seems to be towards robots as the first inhabitants of Mars, just as now, but I will presume that a modification(s) of Optimus would be at the heart of that. In support of that I will assume many Starships will land on Mars with hardware and those will stay on Mars for the most part.
This then supposes that the first human arrivals will not be required to set everything up. At the very least there could be a supply of water for life support if not for fuel.
Also ships that have landed could be set up to cook tanks with Oxygen and CO, perhaps in gas state. That would require a power supply, and of course the ability to process CO2 into O2 and O2.
It is possible that if these materials were available, then some sort of precision fermentation could be achieved, where, some sort of basic food stuffs could be accumulated.
Before the humans arrived, perhaps this much could be done.
Small scall mining of ice would have been demonstrated, and the potential to increase the mining assessed.
So, this might be a minimum startup situation, where some Oxygen and CO as fuel is stored, and some potable water is available, and maybe some bulk food is ready for use.
So, if a dual ship method was used, I have one particular version to consider in this post.
OK, this may contain some practicality issues: 
So, if two ships could be linked and put under spin. One would have its main propellant tanks to be habitable.
That one would have the highest synthetic gravity at the furthest extension in a tank, from the Barycenter of spin.
In one possible case the Lander would have the heat shield and flaps, to be able to land on Mars, but the Orbiter, might not have those and will need large enough header tanks to get into orbit of Mars.
This would allow simultaneous habitation of Mars itself and perhaps setting up some orbital structures.
Granted this is going to be a load on propellants, to get such a mass into orbit without aerobraking.
But if two ships could be supposed to host a total of 200 humans, the "Population" could be spread out into the tanks of the Orbital Ship, during passage, and to land then the Lander Ship then needs facilities for 200 people to be landed, and then offloaded to a base on the surface capable of giving them life support.
Maybe a few would go with the Orbiter, maybe there can be an attempt to develop Deimos and Phobos.
Some of this stuff could be swapped around, where the lander might be the one converted to have humans in the propellant tanks. And then you would have a working Starship in orbit. Of course then you have to get propellants to it, somehow for it to be of further use.
Just some stuff to consider.
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Just to complete the notions a bit more.
I already said that this scheme might be done with two full sized Starships.
One would be converted in route to Mars, the other would not be.
I think that once a ship was converted to inhabit its propellant tanks, it would be very hard to return it to its original character. Even so, if such a Starship did have the Header Tanks, it might be able to land on Mars, and I think then stay there.
Since SpaceX and Elon Musk, don't seem interested in Starboat, it may be that two Starships flying in linked pairs, may be useful.
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Very good and thank you (th).
I need to correct something in the post #1: 
With a Starship and Starboat linked in rotation, the Barycenter of the rotation would be in the nose of the Starship, so, the Synthetic Gravity in the Starboat would be normal as of the orientation of the Starboat on the surface of a world with significant gravity.
And I agree with you (th), it may be that several of these assemblies could travel near to each other for reason of mutual assistance, in the case of some types of trouble.
Upon launch from Earth orbit to Mars, the passengers/crew would be in the Starboat and rather cramped. As the propellants of the Starship were consumed, then the next mode is to purge the tanks on the Starship of vapors, and to then open methods to bring supplies into the tanks from outside. Perhaps with robots.
This then requires some sort of airlock that will be compatible with the propellant tanks having propellants in them at first.
Then with the exterior supplies brought into the Starship, the passengers/crew could spread out into extra space.
Upon arrival to Mars, presuming a base that was prepared to receive them and take care of them the passengers/crew would get into the Starboat for a small time period and land on Mars.
The fate of the Starship has many possibilities that I have mentioned in post #1.
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I request this topic but will without negative feelings comply with alterations such as removal or combining to another topic.
I am thinking at the moment of a Starboat connected to a Starship. But other methods might evolve.
We already think that robotic Starships can land on Mars ahead of time an compile a collection of materials for a life support for humans and their robots.
So, a Starboat might be all that you need to land people on arrival to Mars.
But it would be small, so in order to accommodate more passengers/crew, I suggest that a special sort of Starship could be linked nose to nose with the Starboat, but would not land on Mars.
The Starship might have its engines reduced once in Earth Orbit.
While it would have main Oxygen and Methane tanks filled for launch to Mars, in Earth orbit, then when those tanks were empty they would be purged, and special hardware would all humans to enter the tanks, with equipment to make them reasonably habitable.
In order to be able to spin the nose to nose assembly more than an airlock is needed to allow the connection to be safe, so some cables of some sort.
The Starboat would be upside down in gravity once you did the spin, but a furnishings for the Starship would be appropriate to the artificial gravity.
And from this point there are choices.
1) Upon Arrival to Mars, the Starship is disposed of with the passengers and crew landing in the Starboat, at a well built base. Prior to landing the nose area must be safe for heat shield purposes.
Or....
2) Some method of recovery of the Starship.
-Of course, the Starship might land on Mars separately if method and motive exist for that.
-Or the Starship might go into orbit of Mars, separately if method and motive exist for that.
-Or the Starship might take a 2 year free return to Earth and have some sort of capture to Earth or it's orbits, if means and desire for that exist. In an emergency then the Starboat might remain coupled to the Starship to also do that free return.
The Starship might have means to navigate to Earth, such as electric, or even header tanks.
It may or may not have heatshield and flaps to land on Earth.
Or perhaps some sort of ballistic capture to orbit may be possible.
In the event of a need to have passengers and crew ride free return to Earth, the assembly would have some artificial gravity which would make it more likely that people would survive the event.
***You could to the above with two full sized Starships. But by purging the Oxygen and Methane tanks of one, then you could make more habitation space, and render the artificial gravity more substantial.
***During Earth Orbit Launch to Mars, extra hardware and water/food could be lashed to the outside of the assembly and be brought inside while in deep space. This might be things like chairs, beds, protective materials and such.
Where Dr. Johnson has indicated that one Starship spinning end over end might achieve .5 g synthetic gravity, two starships joined nose to nose, where one of them has its propellant tanks converted to living space could likely do more.

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I would say not puppet, neither is the UK a poodle as I have heard said.
Alignment was possible but becomes less so now. We were thinking of getting the UK into NAFTA, but I think they are not interested. More they may want the commonwealth and to diddle, Europe and North America.
But time will tell, if it allows us to be here to see what will be.
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Here is some more: https://www.youtube.com/watch?v=mWuGb_R … eanUpdates
I know that there is a great discomfort here with the seeming Anti-British tilt in this material.
I will say from the start that America is more "Native" to North America, than Canada or the British, or the French.
As become native to North America, we are not just Latin or African or South Germanic (English), in nature. We are also Slovick, East Asian/ Pseudo Siberian, and North Germanic in nature.
So, in my opinion we are more capable of operating in all the worlds, but allergic to Old World methods.
The British have been useful to us, as to better handle the things that we are more allergic to. But London, cannot operate well in Slovick, East Asian/Pseudo Siberian, and North Germanic worlds. London only wants to clash, with these people many of us here in America are the result of genetic and cultural cross breeding.
The idea of an upper class that is worthy to impose eugenics, on a presumed lower class(s), is barely tolerated by us, and less so now. The idea that the Dominant Man is worthy to exterminate and replace the Capable Man, is offensive.
And we know that we can never be of the ruling class of the Dominant Man, except criminal types who are in our country, and have not evolved to be American or not enough.
At this time at least, it is apparent that the deletion of "Inferior" genes, can do little to improve the capabilities of our people.
But it is apparent that whoever is running Britan and Europe, has little regard for the existence of a Free Capable People. Rather, it seems they are on a backsliding path towards the old world, which much of the commonwealth is embedded in.
So, no surprise that these two pathways are incompatible. And we cannot be murdered into compliance with the wishes of the Zombie peoples of the world.
I think that most of you should not say anything in agreement with me here as, I don't want you to get into trouble and I cannot protect you.
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In the previous post I mentioned heliostats to assist solar panels.
I do not think they have to be very powerful as solar concentrators. Perhaps they can have a active flex mirror, that can go slightly convex or concave.
I also think that since they would be robots, they may have the ability to protect themselves from bad weather, such as wind, Hail, or Dust.
With humanoid robots nearing stronger utility this is not as silly as it may seem.
It is also not completely wrong to think that solar panels might have some form of active protective animation.
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I wanted to leave you alone during your vacation.
Thinking about bulk raw materials on Mars.
I would mention the enormous amount of clay that apparently is on Mars.
If brine from a well could be accessed, here is another interesting possibility: https://www.msn.com/en-us/money/other/s … r-AA1D0FE9 Quote:
Scientists debut innovative technology to transform seawater into next-gen building materials: 'We can fully control their properties'
Story by Leslie Sattler • 10h •
2 min read
And then there is sandstone, such as Mt. Sharp: https://en.wikipedia.org/wiki/Mount_Sharp
And things like Asphalt, Ice, Pykrete, and even water.
And then of course Lava Tubes.
So, bulk materials, some of which might be useful in your construction plans.
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So, looking at this again:
Far better though, perhaps would be to work with fresh water on a humid seacoast.
OK, this would be a round canal as a collector:
I am imagining that if you were putting slush of water ice into the canal under the Shade Balls, you might be able to push the slush and Shade Balls around the circle to help distribution of the Slush.
I have been thinking of the potential value of this structure on Mars.
I could serve as an air generator, and distillation, and Precision Fermentation device.
In the process of distilling water, the waste heat could go into the canal along with Hydrogen.
Oxygen could be handled separately.
A circular structure is not mandated. It could be of a polygon. Perhaps a Square, or Serpentine.
In the age of animated machines, complex heliostats would be able tilt light to appropriate spots on the covering roof for the solar cells. The roof could be "Smart", and say that it wants more, or less.
Solar Panels will not want to be overheated, but kept cool, but may handle more light if not abused with too much heat.
Robots that work as Heliostat directors during daylight might be able to do other tasks at night.
This should have value on Earth, Mars, and maybe other worlds.
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