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this post was submitted on 17 Jun 2024
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SpaceX has been receptive to design changes to starlink in the past to minimize impact, like decreasing reflectivity and reflection angles for astronomers. They might be receptive to moving to different alloy for the body construction.
Magnesium comes to mind that would be light but expensive. Steel alloys might be cheap and heavy options for later when starship is operational. Would those have similar effects on ozone, or is it only the aluminum oxides?
Magnesium oxides can also serve as a catalyst for lots of reactions, but I'm not sure if it will have the same effect in this specific context, I'd guess it would.
That's why I added the link to the wooden satallites, that also reduces the metal debris somewhat and reduces other effects like radio interference.
Wood is interesting, but the article doesn't address off gassing at all, which is a huge problem for communication satellites. Is there a way to keep the wood from off gassing? For 3d prints in vacuum, they metal coat them to keep the gas inside. Or maybe you could resin soak them? With hopefully an extremely UV stable resin. But I didn't know what the weight trade looks like then, resin is heavy.
But if you're looking composites anyway, carbon fiber would be another great option. Lightweight but with a few manufacturing constraints. But should burn up to carbon dioxide on reentry.
I just read an interesting research article from NASA that shows that carbon fiber survives reentry better than our previous scientific consensus claimed.
Some carbon fiber will burn up into carbon dioxide, but a good chunk of it will surprisingly survive reentry conditions. I think you are very right that it should be a better material to use for starlink.
I feel like it shouldn't even have to be said out loud that gravity and weight correlate, but their orbit would be heavily impacted by replacing aluminium with five times as much steel for the same durability. You might be able to get away with slightly less if you consider the steel has more heat resistance, but idk.
Yeah you'd need to put up fewer sats per launch. But they might still have enough lift capacity on starship to do that.
Weight does not affect orbit. It affects the amount of fuel needed to reach orbit, and therefore cost, but not the orbit itself.
Exactly, it needs a higher angular momentum at the same altitude.
When there’s drag involved it’s different, but in vacuum there’s no relationship between weight and orbit.
Are you referring to the effects of upper atmospheric drag on the orbital maintenance requirements?