Satellite guided to assisted crash in Atlantic in world first
theguardian.com
theguardian.com
https://www.esa.int/Applications/Observing_the_Earth/FutureE...
Along with a video of how it was performed:
https://dlmultimedia.esa.int/download/public/videos/2023/07/...
Controlled deorbits have been a thing for a while, and if we're talking about deorbits designed to minimize risk of debris impact, IIRC Starlink satellites were designed to maximize the amount of the satellite that is vaporized by reentry.
Edit: Ah, the "world's first" is that they were able to choose where any parts that aren't vaporized would crash. The esa article is clearer on that.
I guess if I were to be unnecessarily pedantic, most crewed capsules and reusable ISS resupply vehicles have also technically done that.
Aeolus, a satellite that has provided data to weather centers across Europe since 2018, was successfully helped to its final resting place by mission controllers at the European Space Agency.
[0] https://en.wikipedia.org/wiki/Car_Allowance_Rebate_System
> it was so sad seeing a car being deliberately killed.
like this
The amount of debris in space is going to be a problem that's going to be both costly to solve and very detrimental to future space systems if we continue to not do enough about it.
This is also a safety consideration in satellite design - see, for instance: https://spectrum.ieee.org/spacex-claims-to-have-redesigned-i...
If the whole thing comes apart into tiny pieces, you have no chance that anyone/anything on the ground will be injured/damaged by falling debris..
All that's really needed is a convention for those satellites than can, to use the last remaining propellant to perform a de-orbit maneuver.
An ICBM warhead reaches space but at suborbital speeds. It never reaches orbital velocity and will reenter no matter what; it has a heat shield so that the warhead remains intact when descending through the atmosphere.
For satellite disposal, the satellite starts off at orbital velocity and needs to be decelerated above the atmosphere to drop the low point in the orbit far enough that the atmosphere will decelerate it below orbital velocity.
https://what-if.xkcd.com/58/ has a good overview of the difference between suborbital and orbital velocity.
I had naively expected at least something like 10 years, even in LEO.
Imagine if every ship to ever sail was still afloat and never sank. We’d have thousands of unmanned, uncontrollable vessels ping-ponging around the ocean.
Then if you start counting every single piece of debris a satellite can run into, you're looking at millions of objects. Unlike ships, the debris (and even many satellites) doesn't have anyone "on watch" and there's no way to steer out of the way at the last minute. Because of how orbits work you can't really organize traffic into "shipping lanes".
If you want to do the math yourself, NORAD publishes satellite orbital parameters, which can be used to look for potential conjunctions. You can also sign up for an account at https://www.space-track.org to see the Space Force's data, or CelesTrak for something similar that isn't login-walled (https://celestrak.org/SOCRATES/). The tl;dr is that it's not rare for 2 satellites (or a satellite+debris) to have a 1 in 10,000 chance of crashing into each other. As more and more satellites go up and more and more "1 in 10,000" events happen on a daily basis, more conjunctions will occur. Each conjunction can create thousands of pieces of debris, which exacerbates the problem- nowadays I think ~30% of all debris in LEO comes from China's 2007 ASAT test.
NAVAREA VII 229 OF 2023: (24 JUL 23) 1. INDIAN OCEAN – SW SECTOR – AND SOUTH ATLANTIC OCEN – SE SECTOR 2. CHART SAN 1 3. AREAS TEMPORARILY DANGEROUS TO NAVIGATION DUE TO ROCKET CARRIER ELEMENTS ATMOSPHERIC RE-ENTRY FROM 0009 – 0712 UTC 27 JUL TO 02 AUG 2023 DAILY. A. 08 - 52S 092 - 27E B. 07 - 45S 089 - 27E C. 30 - 12S 061 - 09E D. 40 - 45S 002 - 20w E. 42 - 56S 002 - 23w F. 32 - 15S 063 - 10E 4. ALL VESSELS REQUESTED TO KEEP CLEAR POTENTIAL DANGER SHOULD VESSELS ENTER RANGE 5. CANCEL THIS MESSAGE 020730 UTC AUG 2023
i think it will be fine.