Mission to reach and operate at the focal region of the solar gravitational lens
arxiv.org
arxiv.org
Here's gmaps satellite view at ~10km/px
EDIT: fixed permalink https://www.google.com/maps/@41.4220797,-93.7912673,6877284m...
also: https://imgur.com/a/JwHmaIY
Wow.
And the reason we as a society aren't doing this already is what? This thing should be consuming a percent of two of US GDP until it's done.
Because you have to park it 900AU away from the sun (Voyager 1 is at 147AU after 40 years and not in a solar orbit) and it has to have a special kind of coronagraph that flies as a separate spacecraft from the telescope (hasn't been invented yet) and your telescope is limited to looking at objects directly opposite the star from the orbit of the spacecraft. At 900AU it would take decades to slew such a telescope to view a new object in the sky.
At the current time this is basically a science fiction project that promises that if we put a very special spacecraft in a very specific place then it is within our technological capability to image an exoplanet. That doesn't mean it's even a remotely practical idea. It's interesting to talk about but useless to get all worked up about why it's not getting funded.
This is one of the reasons for papers such as this one: exploring what meaningful solutions to these problems, and meaningful mission profiles, would actually look like in practice.
I'd hope less of a risk of micrometeorites (though it would have to look on its own for incoming projectiles and take evasive action). Then again, 900 AU is in the middle of the Oort Cloud so perhaps there's a lot of small junk out there too.
So just bring 50% more? I don't think the weight of the Pu-238 is a key limiting factor on this mission.
That kind of difference might be visible through one of these telescopes, especially if the border is long.
Though I've heard this is actually overstated.
[0] https://www.npr.org/sections/thetwo-way/2014/02/26/282909885...
https://www.businessinsider.com/divide-between-west-east-ber...
Such a line taken of Earth is likely to have nothing in it but ocean and clouds.
If you sent a swarm, each would get its own line of pixels, as many lines as spacecraft.
The idea was that at each moment of each day, the sun was in a different spot in the sky, and each day it shifted toward or away from the equator. So they stitched the samples together mathematically based on timestamp and a 3d projection of the earth. You could tell it was a backyard, but it was very gauzy, like that moment when you first wake after a nap.
The spacecraft would be taking one pixel, then awhile later another pixel, then another. It could get all kinds of dimensional details at each pixel, with full spectra, polarization, what have you, but just one at a time, unlike your scanner bed, which collects many thousands simultaneously, with as many separate optical sensor elements.
After it has collected the whole series, that would be the one, thin row of pixels sent home.
The next spacecraft over could collect another line and send that, watching a different bit of planet surface. Two thin line samples would not be very informative, but hundreds could be.
It is actually, potentially, a bit better: the planet would be rotating while the spacecraft moves between pixel points, and the spacecraft could continue sampling the entire time, getting at a series of adjacent bits of the planet, until the planet rotates to where the first was sampled, and you can sample the next spot over, looking from an infinitesimally different angle. So, possibly, it is scanning a line across the planet's surface, and then later another line nearby. But each line would cover almost the same line as last time.
Of course what it really would do is just watch the planet continuously for years, and send literally everything back, where the planet's presumed rotation could be puzzled out, and then everything could be stitched together afterward. Data from a single probe might suffice to yield an image.
In effect, the spacecraft moving is sweeping across one axis very, very slowly, and the planet's rotation is sweeping on another, albeit probably not one at 90 degrees, but at some angle to the first. (It would be very unlucky for the two to align, but wholly possible.)
Since all this would happen over days and years, the image would end up with an average of that many years' weather, so nothing like a snapshot. But if cloud cover ever breaks, any continents shores would anyway be sharp.
> The spacecraft would be taking one pixel, then awhile later another pixel, then another.
This is what each pixel in scanners CCD does. In his example, the swarm would be like the row of pixels.
> unlike your scanner bed, which collects many thousands simultaneously
The swarm would.
> watching a different bit of planet surface. Two thin line samples would not be very informative, but hundreds could be.
You would want to do this simultaneously, like in a scanner, with some distance between the sensors, so they could sample different "thin lines" of the planet, which could be stitched together to make one image, just as in a scanner. No need to wait. Regardless, a rigid physical or temporal lock isn't really required here. The concept is the same. You could arrange the swarm as a line, diagonal, grid, whatever.
It would be bad luck to choose a Venus-analog to map.
I might have some fundamental misunderstanding, because I don't understand how this could be.
> stepping out until the probe has gone enough distance to be sampling a separate bit of surface.
Why not have a probe already at that distance, so it's gathering something of that surface?
My assumption here (knowing very little of gravitational lensing) is that the gravitational lens still has the concept of an "image surface", where a translation in that image surfaces can be mapped to some translation in the projection of the thing being viewed. Are you saying that if I put two probes up, with some appropriate spacing between, they can't collect different stripes of the same surface, at the same time?
But if the probes are recording continuously and sending it all back, you can probably identify points that are simultaneous on two tracks, after the fact.
But that gives you just a scattering of points on that day. The next pixel over, for each probe, will be for a different planetary day. Your image, stitched together from all the lines returned by all the probes, is an image smeared over at least as many days as pixels in each line.
In the Layers menu, set it to Satellite, Globe view, and turn off Labels. Then, zoom until the earth is ca. 1275 pixels wide
https://earthobservatory.nasa.gov/images/79800/city-lights-o...
I haven't read the paper yet, but this thing would have to have a fair amount of nuclear power, and comms would be a challenge as well. As the abstract mentions, though, while the project has a high degree of difficulty, there appear to be no complete technology showstoppers to actually doing this, so it's at least as doable (and considerably cheaper than) a von Braun-style centrifugal space station in Earth orbit.
It'll be interesting to see if the idea gets any traction...
I recommend clicking on the "solar system" toggle in the bottom middle of the view. It gives you a real sense of the planets, probes, asteroids etc that are flying around our solar system.
Also reminds me of looking at air traffic control maps and what that might look like once intra-solar system space travel becomes routine.
seems pretty good.
You'd need to carry a deployable/detachable mirror with you to reflect the laser back at the craft, but that mirror itself would also get accelerated further out, which means having to correct for that, etc., etc.
Which raises the other question: how would we slow this thing down so it just doesn't keep going past the 900AU mark?
Regardless, I guess we would be fine picking a slower speed that would get it there in a few years, which might be significantly easier to achieve.
It’s an ambitious project.
With all the various inefficiencies in power collection/generation, laser generation, momentum/power transfer, etc. we'd be talking probably somewhere around 5% end-to-end power transfer - if we were lucky. Which is still way better than the rocket equation (probably).
So to get the required 1.853 * 10^18 J at 5% efficiency, we'd need say 20x more power at earth to accelerate it (if 5% efficiency). So 3.706 * 10^19 J. Which starts get more concerning, at 8,840 gigatons of TNT.
Let's take the most efficient means we can imagine to produce energy, direct matter annihilation. Annihilating 1KG of mass (using 500g of Anti-matter, 500g of Matter) produces 8.986 * 10^16 J of energy. If we could somehow feed the resulting energy directly into the laser for accelerating the craft, and assume near 100% efficiency in doing so, before laser losses - we'd only need roughly 1000 KG of matter/anti-matter to do so.
Not bad!
But wait, our more likely end-to-end efficiency is at best 1%. Hmm. Which would require 100 times the input energy to spacecraft acceleration. 44 Gigatons of TNT or 1.853 * 10^20 J.
5KG of matter/antimatter.
Which is definitely not a significant fraction of earths mass, but yikes. I wouldn't want to pay that energy bill!
51,480,512,292,500 kWh (the 'wall plug equivalent') at my current rates would be $26 trillion dollars!
https://en.wikipedia.org/wiki/Project_Orion_(nuclear_propuls...
https://www.centauri-dreams.org/2022/07/26/getting-there-qui...
Earths atmosphere and weather affects this sort of telescope IIRC and will filter out some lightwaves but seems like a much easier win
(aside from the obvious impossibility, would it work? I'm sorta assuming that heavier mass => more distortion => closer focal point. Is that correct?).
Light from far enough away is focussed by any mass, and will appear as a 'ring' around the mass. But if the mass isn't heavy enough the 'ring' that you see might be behind the object itself.
2109: Aliens receive a reply, which includes a map of their own world, including where their largest cities are located.
I'm just saying, this is totally a possibility! We can creep on the neighbours!
I think we'd interpret this as a threat, maybe, like a target map. They might too.
Probably best to reply with something more innocuous, like the Fibonacci sequence.
"We hear you, and just letting you know, we know where you live and have started targeting solutions. Just so you know, we're all armed down here!"
Way to make friends !
https://exoplanets.nasa.gov/resources/1015/flower-power-nasa...
"The "petals" of the "sunflower" shape of the starshade are designed to eliminate the diffraction that is the central feature of an Aragoscope."
"The starshade is a spacecraft designed by Webster Cash, an astrophysicist at the University of Colorado at Boulder's Center for Astrophysics and Space Astronomy. The proposed spacecraft was designed to work in tandem with space telescopes like the James Webb Space Telescope, which did not use it, or a new 4-meter telescope."
the article[1] says "For light grazing the surface of the sun, the approximate angular deflection is roughly 1.75 arcseconds." So, what, we take the arcsin of 1.75 arcseconds to get the apparent divergence ratio, and multiply that by distance to stars? As long as that value is larger than the aperture of your camera, then you don't get competing light? Or maybe you'd need something like the TESS satellite, where you have a screen specially created to only allow certain beam transits into your detector.
I've worked with a nearest 10k stars database (https://celestiary.github.io/, zoom way out) and the edge of that is about 2k light years away. So very roughly, let's say there's 1/8th of those in a certain direction... so you get.. what? some 2k sample points towards some distant object? But really most of them wouldn't deflect that object's light towards Earth, but usually over or undershoot.
Don't really know how to put these together quickly, but is giving me some good food for thought!
I wonder if the star around which the exoplanet orbits can be used to sound the channel? The light from the star would contain information in the form of its spectra. Maybe this can be used to get the channel response? Perhaps the spectra can be treated as a form of modulation?
Maybe related, depending on how close the light from the far target is to tangent near the lensing star, there is also an atmosphere around the star that is emissive. I was thinking that's mostly noise, but maybe it's accelerated enough to shift its spectrum and serve some purpose in measuring the lensing strength? But either way, would need to characterize it enough to remove it from signal.
I've created a project under Celestiary since I think we can use the code there to do the search on the Celestia star database and also do simulations.
https://github.com/celestiary/mglt
I hope that's interesting and that we can work together!
Cheers, Pablo
I think this one: https://www.goodreads.com/book/show/13039884-existence
Radio wavelengths are ~9 orders of magnitude larger than optical, meaning the detector would need to be placed roughly 30 light years from earth. A bit out of our reach.
(assuming I did my back of the envelope math right)
[EDIT]: the formula on page 4 of the book below does not seem to have a frequency parameter ...
Also, they seem to consider that objects worth looking at are at infinity, which is why there is a well-defined focal distance from the sun.
What seems to involve frequency is that the gain of the lens varies (same book, page 9).
http://erewhon.superkuh.com/library/Space/Spacecraft/Deep%20...
Yes.
And "aiming" your observatory involves moving it on that sphere. Given the distances involved that is pretty much either impossible or time prohibitive.
The region starts at 548 AU from the Sun. So 548 times the average Sun-Earth distance.
In an ideal world you would teleport your camera to this location instantaneously, take a picture and then teleport to the next location to look at something else.
We don't know how to do that. The distances are immense.
So instead we pick a target, and send out a satellite or satellites on the opposite vector from it to take a peek. There is a single point where the target will be in perfect focus, but in practice (as the paper shows) the target is "in-focus" enough in a larger region that your satellites can take a picture while they fly through the region around the ideal point.
However, we are using the mental model of a camera lens to reach that conclusion, and I'm not certain it applies:
1) even if we use the mental model of a camera lens, given the distances involved, you can probably consider most of the interesting the targets to be "at infinity"
2) I'm not certain that a gravitational lens works like a camera lens.But as an actual scientific investment, in my opinion, it belongs pretty near the bottom of pile of things we should spend our astronomy / cosomology / astrophysics budget on. The cost per unit of new information is just way too large, and the risk of mission failure too high, to justify making it a priority.
My opinion wasn't about the feasibility of this, but rather that of a tax-paying citizen who expects to get value for money spent. I don't see it in this, and I don't really expect the authors imagined they would be describing something that was likely to get any funding attention - the project is too big, and too far out there from an engineering perspective, given the little we'd get from it. So, yeah, I think their writing a long feasibility study is just published paper padding.
And not only is it good for planetary sciences, it's good for cosmology too since it enables looking at the truly small scale structure of the cosmic microwave background. A mission to the gravitational focal line opposite some star should be one of the highest priorities.
http://erewhon.superkuh.com/library/Space/Spacecraft/Diffrac...
http://erewhon.superkuh.com/library/Space/Spacecraft/Direct%...
http://erewhon.superkuh.com/library/Space/Spacecraft/Image%2...
http://erewhon.superkuh.com/library/Space/Spacecraft/Mission...
http://erewhon.superkuh.com/library/Space/Spacecraft/Photome...
http://erewhon.superkuh.com/library/Space/Spacecraft/Resolve...
If you don't have an active propulsion system for station keeping then you cannot pick targets. Who wants that? Nobody.
This concept is 50 years off at minimum.
Actual station keeping +- a few meters once out on the gravitational focal line opposite the target system (which itself is moving) would require some cold gas thrusters that would limit the duration of the mission. But the forces and accelerations required are very small when you're 600 AU out from the sun and even the photon pressure isn't throwing things off anymore.
Yes, getting out there with enough mass for station keeping would be hard and it'd require new methods. Either electrostatic solar sails, or a more traditional H-reversal oberth burn close to the sun.
[1]. https://www.seti.org/book/communications-extraterrestrial-in...
If so, where on that sphere would we place the scope?
Or would it sorta glide on that sphere to be able to look at a specific points in the universe?
But the focal point of this lens is about 500 times the distance of the earth to the sun, so difficult to get to.
Am I alone in thinking this is somewhat pointless to discuss before the prerequisite technology is developed? It's a bit like "how to keep your sentient sexbot from deciding to murder you". Like if we could do those things in the first place there would be a thousand applications with a better return on investment than this.
Probably not. Most people have trouble thinking long term.
> this is somewhat pointless to discuss before the prerequisite technology is developed?
People wouldn't develop said prerequisite technologies if there are no applications for it. This paper shows that if we would have those technologies we could get this neat thing.
> there would be a thousand applications with a better return on investment than this.
Name them.
From the article "The study reveals elements of such a challenging mission, but it is nevertheless found to be feasible with technologies that are either extant or in active development." (emph. mine)
It's pointless to discuss the application of technologies in active development?
> there would be a thousand applications with a better return on investment than this
You veered into a baffling non-sequitur, there. ROI in a unique science mission to image an exoplanet 100 l.y. distant to a resolution of 10s km for potential human habitation? The successful ROI is incalculable.
That said, we are indeed researching ever more advanced propulsion technologies!
We've made great strides in electric propulsion, which is far more efficient for long voyages than chemical rockets. This tech is already in wide use today in satellites and probes of all kinds.
We're ramping up research in nuclear rocket propulsion again. There are several branches here: nuclear electric, nuclear thermal and nuclear pulse. Of these, the last one is the least developed since it basically means using nuclear explosions to boost you, but it has the most promise for futuristic spaceship drives.
There's also the possibility of using antimater pulse drives but that's a hairy can of worms. Very hard to produce the fuel in enough quantities.