Also, generally, what about increasing cloud cover in general? Wouldn't this reap a huge reward for cooling the planet? I know it doesn't remove gasses and prevent ocean acidification, however it may help with heat-related issues.
Also, generally, what about increasing cloud cover in general? Wouldn't this reap a huge reward for cooling the planet? I know it doesn't remove gasses and prevent ocean acidification, however it may help with heat-related issues.
I don't think people realize how a lot of these problems are solvable for only a few billion dollars... It's an engineering problem, mainly. Someone just spends the money and goes and fixes the problem.
You've shown a proposal, not a reality. (and the proposal didn't even mention a "shield" that I saw, but I may have skimmed past it). I didn't see a price tag, nor a timeline. Money can boost research speed, but not remove the need entirely.
Second, If the cross section of the earth is 1.2x10^14 m^2, one of these would...well, we don't know, because the link mentioned volumes and length (the 10k km is a potential "span length" and wasn't tied to being "one" of anything). I failed to find the cargo volume for a Falcon 9 or other rocket (everything is in mass) but I think it's safe to say that you're talking a lot of launches which clearly aren't trivial to do.
Third, and most importantly, you've just decreased the amount of energy coming to earth. You've not solved the problem, you've changed it.
I love tech, but I think it's worth noticing the ratio of times someone says "It's [just] an engineering problem" versus the number of issues that have been actually been solved in this way (seeing the problem, spending a boatload of money, seeing problem solved). Most of our industries are based on the fact that we KNOW they can grow into more, but figuring out how and the complications thereof are literally the work of countless lifetimes.
Probably the most important advantage sunshades have over other kinds of geoengineering megaprojects is that they can be trivially (compared to their construction costs, that is...) turned off. If they turn out to be very harmful in some previously unforeseen way, we can choose to not have them anymore.
That is not so for, for example, seeding lots of nutrients for algae over the continental shelf.
The sunshade approach to SRM looks like it may have been devised like other big speculative space projects: "start by assuming that big projects in space are the solution, then find a problem to motivate that solution." (See also: mining helium 3 from the Moon.)
Solar radiation management with reflective aerosols instead of space sunshades looks simpler and easier to me. Most importantly, SRM based on aerosols is incrementally scalable from small low initial investment/scope. The sunshade approach, like many envisioned large space projects, appears to require large "lumpy" investments before delivering any detectable benefit.
And, as mentioned, it's pretty easy to 'turn off' (fold or destroy) a sunshade. Not so easy to remove a bunch of aerosol in the stratosphere. I'd prefer more expensive but reversible action, personally.
On the other hand, a slow approach may negate that aspect, and just about anything is better than the nothing we've got now.
There's a lot of EM that neither chlorophyll nor existing PV can use. Hopefully a sunshade would be chosen that selectively works on those less-useful bands. I hope that someone is looking into aerogels for this purpose; they can cover a lot of area per unit mass and have tunable optical properties.
Really? This isn't just a matter of putting a big ball of tin foil out there letting it go. What about the station keeping? How is this big piece of tinfoil going to stay in place? At these sizes, solar pressure and the buildup of static charges become huge issues. It is going to drift. It will need engines, power and fuel. Ion thrust would seem an obvious answer, but electrical/static issues may make a web of ion drives difficult. It will need either new tech or, at least, extensive testing of current tech before any attempt. = a great many billions of dollars. I'd rather see that money spent on solar panels.
We do not have decades to develop a mature space-mining and construction industry.
Objects in space are generally also subject to less weather, and as such they don't materially degrade. You could make a shield out of opaque film that would tear to shreds at the slightest breeze (see JWST sun shield)
That said, I think the usual objection to the space mirror approach is that you can get the same result much cheaper by spreading a cloud of tiny reflective particles into the upper atmosphere. (I've heard of proposals that would just mandate some additive to the fuel used by large passenger aircraft.)
Making the sky 1% hazier is kind of uninspiring (especially when compared to giant orbital mirrors, which could also act as death-rays if aligned and focused properly), but if it's cheap and is likely to work, then maybe it's worth a try.
(Unfortunately none of these options is that they don't do anything about ocean acidification.)
"MYHRVOLD: So, climate change is a 1-percent effect. Now all we have to do is make the sun 1 percent dimmer. Now I don’t literally mean changing the sun. But there are a variety of things that bounce sunlight back into space. Clouds are one of those things: white clouds bounce white light back up into space. It turns out that volcanoes throw ash and particles, if it’s a big volcano, very high in the atmosphere. That reflects some of that light. And in fact this happened in 1991 when Mount Pinatubo went off. It cooled worldwide temperatures by a degree, degree-and-a-half-Fahrenheit for 12 to 18 months. Well, my company has come up with some very practical and cost-effective ways of deliberately putting particles into the upper atmosphere. And on paper, it works out that you could nullify all of global warming that way." [2]
[1] http://www.nathanmyhrvold.com/ [2] http://freakonomics.com/podcast/save-the-planet/
PS: Unfortunately, as a side effect you reduce the energy of all plant life by ~2% solar panels would also be effected. While this is probably no where near as bad as global warming it is something to look into.
That is to say it's clearly still possible, just not as cheap as people are assuming.
A better choice is something akin to a semi-sun-synchronous Molniya-style-orbit. That is, orbit that is somewhat highly elliptical (so a satellite on it spends most of it's time near apogee, and zips through the perigee relatively quickly), and which precesses so that the apogee is always between the earth and the sun.
A satellite on such an orbit can easily spend >70% of it's time between the earth and the sun, and you could send many satellites there for a similar cost to putting just one to Earth-Sun L1.
There are going to be real trade-offs to any orbit, but I think the minimum cost is going to be above X mass in L1 means X mass into LEO as you can't use less mass than that in any other orbit.
BFR could deploy a completely passive sail directly into such a sun-synchronous elliptical orbit, return to land, and launch again after a few hours.
The only reason ionic propulsion might be considered is the they are already going to be solar panels. If you make a large chunk of them from solar panels you then have crazy energy for space based industry and plenty of energy for ionic propulsion.
Also, with that much mass in orbit you are going to want some way do move dammaged segments.
I'd imagine that in the neighborhood of L1 you would try to find some equilibrium point a little closer in to the sun so that the force of the solar wind matches gravitational pull to the sun. If you start drifting in to the sun, you expose more surface area, and if you're drifting towards the Earth, you re-orient the sail to absorb less solar wind.
But, while not necessarily difficult it does prevent a lot of the more simple designs as you can't just toss out a bunch of reflective beach balls with very low pressure or other 'simple' means of blocking sunlight.
But, aim the sail off-center say 45 degrees from the sun and you can pick if that's adding or subtracting angular momentum from your orbit over time. Reduce angular momentum and gravity pulls you into a lower orbit and thus more orbits/year. Reverse that and your gain angular momentum and get fewer orbits per year. L1 is a special case as it's balanced between the sun and earth so you have the same number of orbits per year.
Now, rather than just orbiting the sun your also orbiting the earth. But, similar manovers work just fine.
PS: It's even more complected as you end up in elliptical orbits if you don't keep things balanced etc, but that's the basic idea.
The geometry works out more or less linearly with distance. So 1.5 / 0.384 = 1.065. Which means and object 1.065x as wide as the earth would also provide a total solar eclipse. Making sunshades more than 2x effective L1 vs LEO.
PS: Only 1/2 the time they are on the sun facing side, but they are not perpendicular with sunlight for that entire half. At a 45 degree angle a sunshade blocks ~70% as much sunlight vs a 0 degree angle.
Personally, I like the idea of Marine Cloud Brightening. Getting 1 or 2 thousand ships spraying seawater into the air seems tractable, if not trivial.
I suppose you could have a bunch of shades in a geosynchronous polar orbit, but I suspect they'd still be more effective over the equator, just because it gets more sunlight.
Don't think it works here though - if the pressure of reflected sunlight is counteracting gravity, then I don't see how the statite can be acting as a sunshade. If it were in position for that, the sunlight would be pushing it toward the Earth, no?
If anything this sounds more like the reflectors often proposed for Martian terraforming, which are designed to heat the planet rather than cool it.
But in practice, I think you're right. Forward wrote a short story about such a "pole sitter" ("Race to the Pole"), and had one of the characters say this:
The control problem of keeping the [statite] balanced over the pole is very tricky, especially during the summer season of that hemisphere when the polar axis is over on the sunlit side of the Earth. That’s why ‘pole-sitters’ have to be placed so far away from the Earth. If they get any closer than 250 Earth radii, they become unstable during the summer. [2]
[1] https://patents.google.com/patent/US5183225A/en
[2] https://www.centauri-dreams.org/2010/07/29/statites-hovering...