4 futuristic space technologies — and when they might happen
Solar farms in orbit, nuclear power on the moon, space elevators and interstellar travel — which might we see happen first?
World Space Week this year, which runs between Oct. 4 and Oct. 10,is celebrating how space technology is aiding us in our fight against climate change on Earth — but sometimes it pays to also look outward at what technology can offer us as we expand into space to harness the energy and the worlds that lie out there.
Here we highlight four technologies, look at the challenges that they pose and give some indication of when they might come to fruition — if ever. The time estimates are not necessarily a prediction of when they might happen, but are intended to give a rough idea of how much work still needs to be done on them.
Related: Space-based solar power may be one step closer to reality, thanks to this key test
2040s-2050s: Space solar farms
Currently, solar power provides just over 5% of the world's total electricity supply, but we can do much better than that.
The best place to feel the sun’s energy is in space, without clouds to block the view or an atmosphere to absorb our star's rays. A huge array of solar panels would therefore have an unfettered view of the sun, but the tricky part of this idea concerns building such a space-based array in the first place. Plus, even if we manage that somehow, how would we get the harvested solar energy down to Earth?
Compared to most technologies on this list, power beaming from space is actually ahead of the curve. In January of 2023, the Caltech-built Space Solar Power Demonstrator launched into Earth orbit. On board was an instrument called MAPLE, the Microwave Array for Power-transfer Low-orbit Experiment. MAPLE successfully converted solar energy into microwaves and then beamed the microwaves down to a receiving station at Caltech, where it was converted into electricity. It was a pretty low amount of power — just milliwatts — but it was an exciting proof of concept.
Now, the Japanese Aerospace Agency, JAXA, working with commercial interests, are exploring their own program that the agency hopes to culminate in a solar farm capable of producing one gigawatt of energy and beaming it down to Earth. However, building a solar farm isn't easy.
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A solar panel in space, above the absorbing effects of the atmosphere, receives about a kilowatt of energy per square meter (10 square feet) of the sun. Solar panels are not 100% efficient, however; currently available commercial models have an efficiency of just 30%, meaning a solar panel in space can realistically produce just 300 watts per square meter. To scale this up to producing 1 gigawatt of energy, which would be the equivalent of a nuclear power station on Earth, would require an enormous array of solar panels, multiple kilometers in diameter, with a mass of 10,000 metric tons. Compare this to the International Space Station, which has a mass of 419 metric tons, and that shows just what a daunting engineering task this would be.
Supposing a solar farm could be built in space, it would be placed in geosynchronous orbit, 35,786 km (22,236 miles) above the Earth. The challenge would then be to keep the microwave beam narrow and on target — you wouldn't want the microwave beam to stray and fry something accidentally. Although lasers instead of microwaves would be easier to direct, laser energy can be absorbed by water vapor in the atmosphere or blocked by clouds, whereas microwaves pass freely through them.
Lasers, though, might be more suitable for space-to-space power transfer. This could extend the life of satellites, for example, but they would have to be built with some kind of receiver to accept the incoming laser power beam. We could also imagine a network of solar farms and relay satellites around the moon, beaming power via lasers to a lunar base on the surface.
Second half of the 21st century: Space elevators
This is an old science fiction concept, first conceived by Russian scientist Konstantin Tsiolkovsky — rather than blasting off in a rocket atop a dangerous column of flame, why not ride into space on an elevator car?
The basic design of a space elevator sounds simple. A thick cable extends from a location within 10 degrees of the Earth's equator up into space. The forces acting on the cable would be fierce, with Earth's gravity trying to pull it down, and the centrifugal force on a mass at the end of the cable in Earth orbit pulling it the other way, keeping it taut. The stresses and tension of this cable would be so great that it would need to be made from a material 50 times stronger than steel, however. The only material strong enough are carbon nanotubes, which are "grown" from a process of chemical vapor deposition. The problem is, as the name suggests, carbon nanotubes are small, and the longest grown have been about 14 centimeters (5.5 inches) — that's a big difference to the 100,000-kilometer (62,000-mile) length of a space elevator
Suppose, though, a way is found to manufacture longer nanotubes and mass produce them. Once we have the materials, Stephen Cohen of Vanier College in Quebec, Canada, who is author of "Getting Physics: Nature's Laws as a Guide to Life" and an expert in space elevator design, thinks that the subsequent design phase would take five to 10 years, in parallel with the maturing of the cable material.
"The cable would be spooled down from geo orbit and eventually fastened to Earth port," Cohen told Space.com. "The ship that unspools it would use fuel to gain altitude and become the far-end anchor some 100,000 kilometers away. Alternatively, a separate ship transports the cable portion above geosynchronous orbit while the original vessel assumes the role of a geo port, which is the true ground central for long term operations. This deployment process could easily take a year."
While we're waiting on the carbon nanotubes, Zephyr Penotre of the University of Cambridge in the U.K. and Emily Sandford of Columbia University in New York think we could be setting about building a space elevator from the moon with current technology. Because of the moon's slower spin rate and lower gravity, they reason that the tension felt by a lunar elevator would not be as great as an elevator coming up from Earth and that carbon polymers such as Zylon would do the trick.
Penoyre and Sandford call their concept a "space-line." Whereas an elevator from Earth would be quite chunky, perhaps ferrying multiple elevator cars up and down simultaneously, the space-line would be a thin wire with a total mass of 40 metric tons. Anchored on the lunar surface, it would dangle toward Earth, stopping somewhere around geosynchronous orbit. So, it wouldn't actually touch Earth or subject it to the destructive tension that doing so would incur.
The idea is that a mission to the moon would launch to geosynchronous orbit, rendezvous with the space-line and ride it the rest of the way to the moon, or to a base at the Earthmoon Lagrange point where the gravity of the Earth and the moon balance out. It would cut the amount of fuel needed to get to the moon by a third; a mission would still have to launch out of Earth gravity well, but the space-line would be solar powered.
Penoyre and Sandford estimate that a prototype would cost billions of dollars, but in the long run it would save money if we are to permanently settle on the moon.
Cohen is looking even further afield, to Mars. "I think a first Mars venture with humans precedes space elevator construction but I would argue that no sustainable colonization of Mars is achievable without an infrastructure like the space elevator," he said. "And so, design and construction phases of the space elevator should probably coincide with the first humans on Mars."
Currently, there are no concrete plans for humans to travel to Mars. Much might depend upon how NASA's Artemis lunar program develops. If a lunar base can be built and crewed by the 2030s, astronauts can learn the skills they'll need to survive on the Red Planet, but first we need to learn how to live on the moon. And to do that, we'll need power, as we'll next discover.
2030s: Nuclear power on the Moon
The moon is tidally locked to the Earth, which means that we always see its same face, the familiar "Man in the Moon." Don't be fooled into thinking that the moon doesn't rotate, however — it does, at the same rate that it revolves around our Earth, which is how it always keeps the same face directed towards us. It takes a little over 27 days — about four weeks — to rotate once, which means (almost) everywhere on the moon sees two weeks of daylight and two weeks of night. The exception is some areas very near the poles, which can see 80% daylight. However, if a lunar base were to be solar powered, it would need 100% daylight, so an alternative power source is needed.
Nations and space agencies around the world are now racing to develop the first nuclear fission reactors for the moon. In February, NASA and the U.S. Department of Energy selected three design proposals for a fission reactor to fly on a future Artemis mission. The reactor has the design specification of producing 40 kilowatts for at least 10 years on the lunar surface.
Meanwhile, the Russians and the Chinese have announced that they are jointly planning an International Lunar Research Station with a nuclear reactor, to launch between 2033 and 2035. However, they admit they have not yet come up with a way of cooling the reactor.
"The major issue is what to do with all that waste heat since there is no air on the Moon to convect it away," Simon Middleburgh of the Nuclear Futures Institute at Bangor University in Wales, told Space.com.
Middleburgh is working with the U.K. Space Agency and Rolls-Royce to develop a nuclear fission reactor that could fly to the moon on a future mission. Rolls-Royce have considerable experience working with nuclear reactors, since they outfit the U.K.'s nuclear submarines with them.
"The aim for the reactor energy output would be of the order of 100–300 kilowatts in combined heat and electrical power – both of which would be extremely useful up there [on the moon],” Middleburgh said. "This is an enormous amount of power compared to previous missions, and as the site [for a lunar base] grows, we may want to build a second or third system that will also provide assurance of energy supply. But we won't be building 100 megawatt systems any time soon."
2070s-2120s: Interstellar travel
It took nine years for the fastest ever space mission, NASA's New Horizons, to reach Pluto at a distance of 34 astronomical units (AU) from the sun. For context, an astronomical unit is the average distance between Earth and the sun. The closest star to the sun is Proxima Centauri. It's 268,779 AU (4.2 light-years) from the Sun. Having passed Pluto, New Horizons reached a velocity of 84,000 km per hour (52,000 mph) and it would take about 80,000 years to reach the distance of Proxima Centauri.
Clearly, we're going to need to find a faster way if we ever hope to travel between the stars, but there are people working on the problem. In the 1970s, members of the British Interplanetary Society developed Project Daedalus, which was plans for a two-stage nuclear-fusion powered but uncrewed starship that could ultimately reach 12% of the speed of light.
In 2016, the Breakthrough Foundation initiated Project Starshot, the concept of which is to drive a fleet of tiny spacecraft, called StarChips, attached to light sails that are pushed up to 20% of the speed of light by powerful laser. They would reach Proxima within decades rather than centuries. Just one problem though: the laser energy output must be up to 100 gigawatts — the equivalent of 100 nuclear power stations.
To solve this problem, we could combine futuristic technologies — the solar farms that could be built in orbit to harness solar energy could instead be used to power the lasers. It's all technology we have now, but on a scale far in advance of what we currently have. The stars are there waiting for us — but it seems they might have to wait a little while longer.
Right now, all we have is Earth.
This article is part of a special series by Space.com in honor of World Space Week 2024, which ran from Oct. 4 to Oct. 10 and explored how space technology can help fill the toolboxes of climate scientists.
Join our Space Forums to keep talking space on the latest missions, night sky and more! And if you have a news tip, correction or comment, let us know at: community@space.com.
Keith Cooper is a freelance science journalist and editor in the United Kingdom, and has a degree in physics and astrophysics from the University of Manchester. He's the author of "The Contact Paradox: Challenging Our Assumptions in the Search for Extraterrestrial Intelligence" (Bloomsbury Sigma, 2020) and has written articles on astronomy, space, physics and astrobiology for a multitude of magazines and websites.
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Unclear Engineer Of these 4 technology concepts, the nuclear reactor on the Moon seems like a sure bet, but the others seem more fanciful than realistically evaluated.Reply
Regarding the "space elevator" using a cable that is terminated on Earth and reaches past geosynchronous orbit, that just does not seem to have been thought through the dynamics properly. Even if we can eventually make a cable that can stand the load of tying the far end satellite to the Earth's surface, and assuming that a space "elevator" could "climb" that cable instead of being hauled up by another cable. there is still the issue of where the energy ultimately comes from to get the capsule to geosynchronous orbit.
Think about it this way: Assuming attachment of the bottom end at Earth's equator, it has a rotational speed to the east of 24,901 miles/24 hours = 1037.5 miles per hour. But, geosynchronous orbit is 6,876 mph. So, the capsule must be accelerated sideways by 5.838.5 mph.
How is that sideways acceleration going to be provided? If it is provided by a vertical cable pushing the capsule to the side as it climbs the cable, that will tend to move the cable to the west, which will lower the upper end of the fixed length cable as it takes on a more spiral path from Earth's surface to the upper end satellite. But, that will destabilize the geosynchronicity of the orbit, causing the upper end of the cable to eventually fall out of orbit.
So, maybe that could be fixed by putting rocket motors on the capsule that fire sideways to keep the side pressure on the cable to zero.
But, we also need to consider the effect on the upper satellite caused by hauling the capsule upwards. That will also haul the upper satellite downwards, again taking it out of geosynchronous orbit.
So, again, we could put rocket engines on the capsule to push it upwards, instead of "climbing" the cable by pulling itself up mechanically (and simultaneously pulling the satellite downward).
So, to have a vertical cable, we would need rocket motors that pushed the capsule sideways and upward in the right amounts to reach geosynchronous orbit. But, wait a minute, isn't that like what we already do without the cable? Are we really saving rocket fuel that way? Nope.
So, how would we design a cable stretching past geosynchronous orbit that could be used to haul mass to geosynchronous orbit without using any rocket fuel?
We would need to have that cable spiral in a path that is effectively tugging on the Earth's rotational energy directly along the axis of the cable at all points between the Earth's surface and the upper satellite. I am not sure that such a path even exists, but think that at least most of the energy could come from slowing the Earth's rotation a tiny amount but probably still requiring some rocket thrust on the upper satellite end of the cable to keep things stable, there.
And, besides the effects of hauling mass to geosynchronous orbit, there are also gravitational effects from the Sun and the Moon that need to be worked out. Just like the surface of Earth's oceans get pulled towards the Moon and the Sun, the satellite(s) in geosynchronous orbit and the cable will get pulled on a daily basis by the Sun and Moon with the Moon's pull changing into and out of phase with the Sun's pull on monthly period.
So, to show how this would need to be designed to really work, somebody needs to figure out the Lagrangian equation for the cable spiral, solve it, and determine how long that cable would really need to be. And, they need to determine what amount of rocket fuel would need to be hauled up that cable to keep it stably in geosynchronous orbit while people hauled masses up the cable and the Sun and the Moon affect it.
My guess is that it would need to be a much longer cable than the proponents of this concept envision for a vertical cable. And, I suspect that even thousand-mile-long nanotubes are not going to have the strength to weight ratio needed. That is the issue for a cable from Earth to orbit.
I have not thought about the idea of one from the Moon to lunar orbit. For one thing, it could be pointed directly at Earth, and use that for stability. The cable would be tidally locked, just like the Moon. And, it would have far less distance and far lower forces to contend with. Still, the dynamic effects of hauling loads up and down with just the cable tension needs more thought than I have time to give it. Pulling a mass to the satellite in lunar synchronous orbit is still going to be pulling that satellite closer to the Moon. Even the Lagrange point between the Earth and the Moon is not stable for a free satellite. So, pulling on a satellite in that location to haul loads off the lunar surface is not going to leave the upper end satellite in-place for continued service without some sort of compensating force.
Maybe somebody can show me how the energy to lift the loads off the lunar surface can be "harvested" from the energies of lunar orbit or lunar rotation or Earth's rotation, but I am not envisioning a process for that, at the moment.
The important points to remember are:
1. the energy gained by the hoisted capsule must be taken from somewhere; and
2. it cannot come from the satellite orbit on the upper end of the cable without reducing the energy of that satellite's orbit, so that it goes lower to the body that it is orbiting. -
Stephen Cohen
The issue 'unclear engineer' appears to be raising is what to do about the Coriolis force acting on the cable by an ascending climber. I published a paper in 2008 in Acta Astronautical that explains how it causes the cable to sway, but the system is stable, and oscillates about a vertical equilibrium. The paper proposes several solutions to minimize and even undo such oscillations.Unclear Engineer said:Of these 4 technology concepts, the nuclear reactor on the Moon seems like a sure bet, but the others seem more fanciful than realistically evaluated.
Regarding the "space elevator" using a cable that is terminated on Earth and reaches past geosynchronous orbit, that just does not seem to have been thought through the dynamics properly. Even if we can eventually make a cable that can stand the load of tying the far end satellite to the Earth's surface, and assuming that a space "elevator" could "climb" that cable instead of being hauled up by another cable. there is still the issue of where the energy ultimately comes from to get the capsule to geosynchronous orbit.
Think about it this way: Assuming attachment of the bottom end at Earth's equator, it has a rotational speed to the east of 24,901 miles/24 hours = 1037.5 miles per hour. But, geosynchronous orbit is 6,876 mph. So, the capsule must be accelerated sideways by 5.838.5 mph.
How is that sideways acceleration going to be provided? If it is provided by a vertical cable pushing the capsule to the side as it climbs the cable, that will tend to move the cable to the west, which will lower the upper end of the fixed length cable as it takes on a more spiral path from Earth's surface to the upper end satellite. But, that will destabilize the geosynchronicity of the orbit, causing the upper end of the cable to eventually fall out of orbit.
So, maybe that could be fixed by putting rocket motors on the capsule that fire sideways to keep the side pressure on the cable to zero.
But, we also need to consider the effect on the upper satellite caused by hauling the capsule upwards. That will also haul the upper satellite downwards, again taking it out of geosynchronous orbit.
So, again, we could put rocket engines on the capsule to push it upwards, instead of "climbing" the cable by pulling itself up mechanically (and simultaneously pulling the satellite downward).
So, to have a vertical cable, we would need rocket motors that pushed the capsule sideways and upward in the right amounts to reach geosynchronous orbit. But, wait a minute, isn't that like what we already do without the cable? Are we really saving rocket fuel that way? Nope.
So, how would we design a cable stretching past geosynchronous orbit that could be used to haul mass to geosynchronous orbit without using any rocket fuel?
We would need to have that cable spiral in a path that is effectively tugging on the Earth's rotational energy directly along the axis of the cable at all points between the Earth's surface and the upper satellite. I am not sure that such a path even exists, but think that at least most of the energy could come from slowing the Earth's rotation a tiny amount but probably still requiring some rocket thrust on the upper satellite end of the cable to keep things stable, there.
And, besides the effects of hauling mass to geosynchronous orbit, there are also gravitational effects from the Sun and the Moon that need to be worked out. Just like the surface of Earth's oceans get pulled towards the Moon and the Sun, the satellite(s) in geosynchronous orbit and the cable will get pulled on a daily basis by the Sun and Moon with the Moon's pull changing into and out of phase with the Sun's pull on monthly period.
So, to show how this would need to be designed to really work, somebody needs to figure out the Lagrangian equation for the cable spiral, solve it, and determine how long that cable would really need to be. And, they need to determine what amount of rocket fuel would need to be hauled up that cable to keep it stably in geosynchronous orbit while people hauled masses up the cable and the Sun and the Moon affect it.
My guess is that it would need to be a much longer cable than the proponents of this concept envision for a vertical cable. And, I suspect that even thousand-mile-long nanotubes are not going to have the strength to weight ratio needed. That is the issue for a cable from Earth to orbit.
I have not thought about the idea of one from the Moon to lunar orbit. For one thing, it could be pointed directly at Earth, and use that for stability. The cable would be tidally locked, just like the Moon. And, it would have far less distance and far lower forces to contend with. Still, the dynamic effects of hauling loads up and down with just the cable tension needs more thought than I have time to give it. Pulling a mass to the satellite in lunar synchronous orbit is still going to be pulling that satellite closer to the Moon. Even the Lagrange point between the Earth and the Moon is not stable for a free satellite. So, pulling on a satellite in that location to haul loads off the lunar surface is not going to leave the upper end satellite in-place for continued service without some sort of compensating force.
Maybe somebody can show me how the energy to lift the loads off the lunar surface can be "harvested" from the energies of lunar orbit or lunar rotation or Earth's rotation, but I am not envisioning a process for that, at the moment.
The important points to remember are:
1. the energy gained by the hoisted capsule must be taken from somewhere; and
2. it cannot come from the satellite orbit on the upper end of the cable without reducing the energy of that satellite's orbit, so that it goes lower to the body that it is orbiting.
Regarding energy required to lift the climber to GEO, the majority is provided by the climber's motor, but some is taken from Earth's rotation (the Earth will slow its rotation... Negligibly, of course). Ascent beyond GEO requires no input energy, as it 'falls' upward. -
Stephen Cohen The server will not let me post the link. Feel free to search 'The effect of climber transit on the space elevator dynamics'. It is easy to find.Reply -
Unclear Engineer OK, I found it. The first place I found it seemed to be some sort of condensation that stopped in the middle of sentences and went on to the next section. But, I did find a PDF that is 127 pages, so it is going to take me a while to read through it all.Reply
However, the first thing I saw is that the calculations were "simplified" by assuming that the cable is "rigid". That tends to make me discredit the rest of the study right there. A rigid structure that needs to be well over 22,000 miles long seems like a non-starter.
So, how about some simplified explanation here. Are you assuming that this "tether" goes in the vertical direction except for the sinusoidal oscillations in the horizontal direction? Or, do you let it assume some sort of spiral shape with altitude? -
Unclear Engineer This seems to be the crux of the issue, from the paper:Reply
"Therefore, the work per unit mass done by the motor to move the climber from the
surface of the Earth to the geosynchronous altitude is about 48.5 Ml/kg. An apparent
anomaly occurs when examining the change in the energy per unit mass of the climber
before and after transit, EH2' given by
(2.33) or
(2.34)
The increase in the total energy per unit of mass of the climber in moving from the
surface of the Earth to the geosynchronous altitude is about 57.7 Ml/kg. This result begs
the questions, "How did the climber gain more energy than the work the motor put into
it?" and "Where did this free energy come from?" Thefree energy came from the spin of
the Earth. For a transit to the altitude dj. the energy per unit mass extracted from the
Earth is given by .Q2
; for this particular case, it is .Q2 (R~ - R2 ). The
slowing of the spin of the Earth due to this energy extraction is negligible."
So, basically, the side force on the tether needed to impart 57.7 - 48.5 = 9.2 MI/kg to what is sent up the tether to the geosynchronous level. That is what challenges the assumption of effective rigidity.
Also, I note that trying to launch something off the tether at any other altitude will require rockets to match the vehicle velocity to the local orbital velocity. Otherwise, the ones launched from the tether below the geosynchronous orbit would not be going fast enough (for a circular orbit) and the ones launched from above geosynchronous altitude would be going too fast (for a circular orbit).
Getting back to that side force, that is what I want to see explained, beyond the assumption that the tether is "rigid". Side force cannot be exerted with a non-rigid tether unless the tether is deflected to the side to some degree, so that the spin of the Earth is pulling on the climber to accelerate it. And, the assumption that a tens of thousands miles long tether could actually be rigid is not something that I expect an engineer to be able to design, not with carbon nanotubes, or any other "unobtainium". -
Stephen Cohen Indeed this paper uses a simplified model. A rigid model indicates the basic behavior. My thesis published in 2006 also looked at an elastic cable model. Many papers since have done so as well. An ascending climber excites an elastic model primarily with the rigid body mode but it also induces sinusoidal lateral elastic mode shape participation. The most concerning mode would still be the rigid body one, because it is effectively undamped.Reply -
Unclear Engineer When you say others used an "elastic" model, was that only in the longitudinal direction of the cable, or could it deflect sideways in the two other dimensions.Reply
And, what is the assumption about the upper end mass? Is it assumed to be immobile, or can it move up and down and east and west and north and south?
Not only will a climber have to pull on that upper end, the moon going by is going to pull on it too. Just assuming that it is immobile is a fatal flaw in the analysis. It needs to be SHOWN to not move significantly BY the analysis. -
Stephen Cohen No study I am aware of has assumed the counterweight to be immobile. My studies and others have allowed longitudinal and transverse mode shapes that respect all boundary conditions.Reply -
Unclear Engineer Here is a more succinct explanation of the space elevator concept: https://en.wikipedia.org/wiki/Space_elevatorReply
It includes the following:
"As a payload is lifted up a space elevator, it would gain not only altitude, but horizontal speed (angular momentum) as well. The angular momentum is taken from the Earth's rotation. As the climber ascends, it is initially moving slower than each successive part of cable it is moving on to. This is the Coriolis force: the climber "drags" (westward) on the cable, as it climbs, and slightly decreases the Earth's rotation speed. The opposite process would occur for descending payloads: the cable is tilted eastward, thus slightly increasing Earth's rotation speed.
"The overall effect of the centrifugal force acting on the cable would cause it to constantly try to return to the energetically favorable vertical orientation, so after an object has been lifted on the cable, the counterweight would swing back toward the vertical, a bit like a pendulum. Space elevators and their loads would be designed so that the center of mass is always well-enough above the level of geostationary orbit to hold up the whole system. Lift and descent operations would need to be carefully planned so as to keep the pendulum-like motion of the counterweight around the tether point under control.
"Climber speed would be limited by the Coriolis force, available power, and by the need to ensure the climber's accelerating force does not break the cable."
So, my issue is addressed by the cable deflecting to the west while the climber goes up. Yes, it would deflect to the east as a climber comes down. But, the net effect would depend on the net transfer of mass up or down. Launching spacecraft would get at tiny fraction of Earth's rotational energy, while importing asteroid ores would add a tiny bit to the Earth's rotational energy.
The actual energy/momentum transfer between the Earth and the climbers is accomplished both by the sideways deflection of the tether + climber mass and the sideways return of the tether mass to the vertical orientation once the climber has stopped moving. There has been more analysis of that than I was aware of when I made my first post, here.
So, the issue becomes the necessary strength of the materials needed, and it requires consideration of these side forces as well as the force along the cable between the Earth and the top mass of the elevator.
So far, despite earlier projections that are presented in the Wiki link, we do not have demonstrated material properties that come close to the necessary parameters for both strength and fabricated length. The Liftport company that, in 2005, projected accomplishing that with a factory and launching a space elevator by 2010, actually never even built the factory. Actually being able to create an operational tether still seems to be the major hang-up.
But, I am also wondering about other issues that I do not see even being mentioned. For example, there is some discussion of avoiding lightning strikes by placing the surface end on a barge in the middle of the equatorial Pacific Ocean. And there is some discussion about the electrical conductivity of the tether material being able to provide electric power from Earth to move the climbers on the cable. But, has anybody thought about what electrical effects will occur when we put a conducting cable through both of the radiation belts that surround Earth that are presently directing incoming solar plasma toward the poles? Would the tether make a "lightning rod" ground for those radiation belts down to the Earth's surface? And cables extending from orbiting satellites have been proposed as propulsion devices for maneuvering the satellites, so it also seems prudent to ask what forces the magnetic field of the Earth and coronal mass ejections from the Sun would have on an electrically conductive tether that is tens of thousands of miles long.
I am not trying to argue that a space elevator is impossible. But, my opinion that one is not close to deployment isn't getting changed by what I am learning as I look into it more. It doesn't seem to be as far into the fantasy thinking realm as "interstellar travel", but does seem to share the over-optimistic thinking with "space based solar power". At least we think that the physics may be possible, even if the engineering eludes us for the present, and the economics are highly dependent on the engineering "solutions" eventually developed.