Potential ozone depletion from satellite demise during atmospheric reentry
agupubs.onlinelibrary.wiley.com
agupubs.onlinelibrary.wiley.com
Their solution has been to develop satellites made mostly of wood, which will burn completely upon reentry.
The first such wooden satellite is planned to be launched in September. It is intended mainly for collecting data about the behavior of wood in the outer space, e.g. on wood expansion, contraction and degradation, along with internal temperature and electronic equipment performance.
An alternative to wood would be the use of synthetic polymers, but those are typically more sensitive to radiation, so more research would be needed for finding a suitable plastic and appropriate additives to decrease the radiation sensitivity.
Wood or plastic would not be suitable for ships hosting humans, because they are not hermetic, but they may be an acceptable choice for satellites with a short lifetime and with much more relaxed constraints for the composition and pressure of the internal atmosphere (which may not be needed at all, e.g. when the internally produced heat reaches the external radiant cooling surfaces through solid paths or through pipes with circulant liquid).
And a common place you find carbon fiber in the space industry is actually carbon fiber skinned aluminum honeycomb panels. Very light and very stiff.
https://www.rockwestcomposites.com/shop/plates-panels-angles...
"When finishing the surface of your wooden satellite you must, of course, use an orbital sander."[1]
[1]: https://www.metafilter.com/203958/Yes-they-wood-build-a-sate...
high mechanical strength, with a tensile modulus of approximately 150 GPa and a modulus of elasticity ranging from 18 to 50 GPa. CNCs also exhibit excellent thermal stability, undergoing gradual thermal transitions and decomposition between 150 °C and 600 °CI like how the Google image search for "japan wooden satellite" (https://www.google.com/search?q=japan+wooden+satellite&udm=2) is gummed up with garbage AI generated images of satellites with wooden solar panels. This wooden Borg cube with off-kilter panels is my favorite: https://indianspacetechnology.com/wooden-satellite-lignosat-.... This one is also great: https://www.universetoday.com/161473/building-a-satellite-ou.... I guess the satellite went back in time to the Cretaceous period, where North America had an inland sea?
The future is looking bright, guys!
Pretty soon the web's going to be one big Mikkelsen Twins ebook.
And here is an earlier rendering from 2021: https://www.japantimes.co.jp/news/2021/12/31/national/japan-...
And it only took a simple Google search to find, from a reputable news source.
If you are designing apps in an environment of scammers and shameless grifters, the options for the societies you can build are reduced.
Focusing on the core issue of "how can we stop people from destroying nice things" is critical for society-scale engineering, as it frees ethical engineers to create more magnificent tools.
Ignoring law / politics / etc, and solely focusing on "how can I design this given presence of grifters" is muted engineering.
No, that's a false equivalence. The artists' mockups wouldn't be this bad. They'd either have gotten a real photo or based their artwork on one.
Now Google Images is flooded with images generated in two minutes from half-assed prompts.
> because they have to put something at the top of the blog post or news article to catch viewer attention.
They do not. That's just a current-year web design tic, which "AI" will probably kill.
IIUC it's more that you do it to expand the page-inches on social media so that it's more likely readers will click through to your story, because social media displays the preview banner.
Maybe this is better because the vaporized wood would. not release any alumina. But you'd then have to look at the impact of wood's combustion products when introduced directly to the upper atmosphere. I'm not sure anyone has seriously studied that question.
We already know how the major byproducts interact, I think it would be a question of modeling what happens when we start adding them to the mesosphere. Models aren’t perfect, but it’s not like we have absolutely no idea how the components interact.
Unfortunately, just like green house gases, it requires the very people who benefit from ignoring these kind of problems to pay attention and well...
Unfortunately, the lack of a gradual set of limited changes is why the same process cannot be replicated for climate change remediation. Countries are trying to tackle the entire problem as an "impossible" monolith rather than breaking it up into separate industry and lifestyle practices to address incrementally.
The impact of CFC's on the ozone layer was first proposed in a scientific paper in 1973; the authors testified before the US House of Representatives in 1974 and significant funding was provided to study the problem. The Montreal Protocol was then signed in 1987 despite industry protests that the research was uncertain and there was no crisis that demanded urgent action. This was only 14 years (!) after the effect was first hypothesized. The discoverers of the effect won the Nobel Prize for chemistry in 1995.
I don't expect to see anything even remotely as successful as the Montreal Protocol in my lifetime.
You might as well say people now think { vaccines are clot shots | earth is flat | 9/11 was an inside job } and use that as justification to do nothing about AGW.
People don't understand that those problems were peanuts though in comparison.
Any exercise in making numbers out of nothing is completely useless.
(Besides, is chlorine activation really a bottleneck in ozone depletion? AFAIK it gets activated by UV light quite quickly.)
More fundamentally, chemical catalysts by definition are not consumed by the reactions they catalyze.
Think: a cheese grater. It doesn't react with the cheese, so a few ounces of grater could make hundreds of pounds of grilled cheese.
A hypothetical 300 tons of catalyst is not limited stoichiometrically to how much substrate it would affect.
With a 5-year lifespan for an LEO sat, that's potentially 120,000 deorbits every 5 years...
That will add up quickly... I don't know the science of aluminum oxide increase to ozone depletion.. but this can certainly warrants more research and consideration
1: https://starwalk.space/en/news/spacex-starlink-satellites-ni...
Does the mass make a difference?
NOx is also has a global cooling effect, taking the edge off climate change.
NOx and VOCs from power plants and diesel vehicles produce ozone.
For example, consider that a car exhaust catalyst contains ~5 grams of platinum, and AFAIK, that doesn't really "wear out".
So the range of human impact is somewhere from 2 to 10 times the meteoritic material in Al. That's quite surprising, assuming that my math and research is correct.
Switching to steel should make the environmental impact negligible, considering that the Fe content of meteorites is quite high.
meteoritic material source: https://adsabs.harvard.edu/full/1994IAUS..160...45B
For example the 4 reaction control wheels for attitude adjustment where you actually want mass, were specifically moved to Al on starlink so that they _would_ burn up on reentry.
I don't know how you weigh the risk of environmental effects vs occasionally landing a sat on something, or someone. I guess an actuary somewhere has a table for that.
I still think it’s a political non-starter, though. People will be terrified of being randomly struck with a satellite, and it would be an enormous international crisis if an American satellite deorbited and took out a skyscraper in Beijing or vice versa. Heaven forbid one accidentally hits the Pentagon or similar, it would probably start world war 3.
1 - https://api.starlink.com/public-files/technology_v2mini_back...
More interestingly, the majority (perhaps not yet "vast majority" [0]) of active satellites right now are Starlink satellites. Those things actually maneuver all the time in the interest of collision avoidance, and the rate at which they maneuver is predicted to increases as the number of satellites increase for obvious reasons. [1]
[0] https://www.visualcapitalist.com/who-owns-the-most-satellite...
[1] https://www.space.com/starlink-satellite-conjunction-increas...
Assuming it's overall heavier, you have to carry more fuel, and then the rocket equation kicks in and you have to carry more fuel than that. That's all extra weight that makes your launch more expensive. But if your cost to launch is $30/lb instead of $1200/lb, you've got the budget for it.
More mass means you need larger reaction wheels (or CMGs) to control the attitude of the spacecraft, larger reaction wheels means you need more power to control those reaction wheels, more power means you need more solar arrays/batteries, more solar arrays means more mass and moment of inertia...which means you need larger reaction wheels and on and on and on.
Often people talk about the "tyranny of the rocket equation" but many other things on a satellite are the "tyranny of other non-linear systems"
You can end up seeing that in companies like K2 Space. Their goal is to take advantage of cheaper launch costs with large, cheap satellites. But if you read in the article [0] they had to do things like develop new reaction wheels in house because "there was not a suitable supply chain for spacecraft bus like Mega Class". Starting from scratch on mechanisms like that for space is not super cheap.
https://spacenews.com/k2-space-plans-first-launch-as-company...
I'm not claiming steel is the best option though. Other metals, or even non-metal materials as mentioned in other comments might be better.
I don't think needing new components is really a downside except in the very short term. With much cheaper launch at much higher volume, we're going to be doing a lot of that anyway. We're going to have all sorts of new applications that weren't economically feasible before.
The mass consideration has certainly changed things in general. One of the things we have seen is a shift from aluminum honeycomb panels to just machined aluminum plates which weigh more for the same stiffness but are easier and faster to manufacture.
Steel might also drive more spacecraft to have to do a controlled re-entry (something the Starlink satellites are not currently designed for) as with the higher melting point and more mass it is more likely to survive re-entry. Although it does have a lower specific heat capacity than aluminum so I'm not quite sure on that one but usually the things I have seen that we expect to survive re-entry are titanium tanks and large glass mirrors. They also have the benefit of being in the center so there is a bit of an ablative shield.
On the scale of the planet, that's incredibly tiny. 17 metric tons of aluminum oxide can be made by oxidizing a cube of aluminum about 1 meter on a side. The catalytic action must be incredibly potent!
Wolfram helpfully tells me that the mass of the mesosphere is on the order of 10^12 tons, so that's on the order of parts per trillion.
More is bad that's the bottom line.
Single-use heat shields for smallish things like satellites are quite easy I believe, although fold-out items like solar panels would need to be designed to fold-in again.
Why doesn't every messy industry like this have to pre-pay massive insurance fees ahead of time for known and unknown damages?
Note X isn't the only one with thousands of satellites, there are several startups that are launching their own thousands. Soon we'll have debris and burnup of dozens a day, that will add up.
I can't see the cat going back into the bag (or reengineered) unless there have been proven negative results like the ozone hole directly linked to CFCs.
> One option is to make the satellite survive re-entry rather than burn up. Then just re-enter over a desert like australia or the sahara so you can go find and collect the junk.
So be careful what you wish for!
Global military industrial complex: Now that you mention it...
You don't need a science paper to end up with "letting satellites burn up in the atmosphere results in burned satellite dust in atmosphere", do you?
- Natural Al estimated at 141.1 metric tons / year not varying.
- Human-made: 2016: 5.36 tons, 2022: 41.7 tons, "future" could be 912 tons, i.e. more than 6x natural.
I think the last figure is based on many planned large satellite constellations being deployed.
People will also be upset about the environmental damage, real or imagined.
This is not true, most satellites do not perform controlled re-entry. In order to perform controlled re-entry, you need to have enough thrust to perform the final de-orbit maneuver in a short amount of time before you get so low that you start to lose attitude control of the spacecraft and wouldn't be able to guarantee you are firing your thrusters in the correct direction. To do this in a short amount of time means you need a high thrust system, in other words a chemical propulsion system and not electric propulsion.
All of the Starlink satellites use electric propulsion to do their de-orbit so they are performing uncontrolled re-entry. NASA's Orbital Debris Mitigation Standard Practices (ODMSP) say that you can perform uncontrolled re-entry if the probably of casualties on the ground is less than 1 in 10,000. There are NASA analysis tools that are used to do that assessment of what kind of debris would survive re-entry. This is likely getting updated in the near future to be more conservative though as there was recently a piece of an old ISS battery they thought would burn up hit someone's house in Florida:
https://spacenews.com/uncontrolled-reentry-of-space-debris-p...
I thought I recently read about a law requiring a de-orbit plan for anything launched. I would assume if most of the mass doesn't burn up (Starlinks mostly burn up), it would require them to hit the South Pacific patch or similar.
People tolerate when natural processes kill very few people.
But they get very upset when human activity kill very few people.
https://iopscience.iop.org/article/10.1088/1748-9326/aae98d/...
The good news, since an internet forum's commentariat opinion isn't relevant to whether it happens or not, is that humanity is a couple of teratonnes into a 200-year experiment of many kinds of atmospheric modification and nothing critically non-linear has happened yet. Though we certainly don't have many sigmas of confidence that it isn't going to go non linear (but in the "hot" direction) at some point!
We're even doing a cute little cross-over trial specifically on atmospheric sulphur dioxide injection (just entered the second placebo phase)