[HN Gopher] New Calculation Finds we are close to the Kessler Sy...
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       New Calculation Finds we are close to the Kessler Syndrome [video]
        
       Author : cratermoon
       Score  : 46 points
       Date   : 2024-11-20 20:33 UTC (2 hours ago)
        
 (HTM) web link (www.youtube.com)
 (TXT) w3m dump (www.youtube.com)
        
       | visviva wrote:
       | The paper in question is here:
       | https://link.springer.com/article/10.1007/s40295-024-00458-3
       | 
       | It adds to a pretty large body of literature around this subject,
       | the gist of which is "risk is going up, but we don't really have
       | a good way of estimating what that means in terms of actual
       | collision rates".
        
       | m3kw9 wrote:
       | I would think newer sats will have collision avoidance
       | capabilities and older ones will just crash. Maybe even clean up
       | sats will be developed to collection them
        
         | bell-cot wrote:
         | With currently deployed tech, most of the smaller orbital
         | debris is not (usefully) track-able.
         | 
         | At orbital velocities, you gotta know it's coming to be able to
         | avoid it.
         | 
         | And a orbital velocities, the untrack-able stuff can still kill
         | a satellite.
        
         | michaelmrose wrote:
         | Leo starts at 7.8 kilometers per second and speed plus
         | secondary and subsequent collisions with very small debris
         | makes it impractical. Also carrying fuel to react frequently
         | would dramatically change the entire mission.
         | 
         | If your non refuelable sat is good for 6 months it probably no
         | longer makes sense to launch it.
        
         | bagels wrote:
         | Satellites fail (lost control, or spontaneously explode). Very
         | small debris is everywhere and under 5-10 cm largely untracked,
         | but some are working to fix this gap.
         | 
         | There is no incentive large enough for cleanup (it's expensive,
         | nobody can/wants to pay, and there are a lot of objects)
        
       | benchmarkist wrote:
       | As long as it is militarily and commercially viable then the
       | number of satellites will continue increasing, regardless of what
       | academics have to say about collision rates. As per usual this is
       | a coordination problem and in case people have not noticed
       | nations are becoming less coordinated and more insular.
        
         | akira2501 wrote:
         | > in case people have not noticed nations are becoming less
         | coordinated and more insular.
         | 
         | And what is your yardstick for measuring this? As far as I can
         | tell this is the opposite of true. It's a popular national news
         | meme but I don't believe it's been measured in any reliable
         | way.
        
           | bragr wrote:
           | I don't know about whether it is more or less common, but
           | there has been international drama over conjunctions over the
           | last several years
           | 
           | https://spacewatch.global/2021/12/spacewatchgl-share-
           | chinese...
        
       | mapt wrote:
       | The current trajectory is that SpaceX proved the commercial and
       | military viability of an LEO megaconstellation, repeatedly
       | lowering their target altitudes and raising their satellite count
       | because of debris and cell size concerns...
       | 
       | And now the rest of the world is trying to catch up in a sort of
       | arms race, and not taking any care about debris concerns. The
       | most tempting orbits are the ones in upper LEO that permit them
       | to launch fewer satellites.
       | 
       | SpaceX are going to end up well under 500km (orbital lifespan: a
       | decade) before things are finished, and they switched to very low
       | orbit staging with SEP spiral out to reach final orbit a ways
       | back.
       | 
       | China's newest constellation Thousand Sails is at an altitude of
       | 800km (orbital lifespan: thousands of years), with a thousand
       | satellites in the works over the next year or so and 14,000
       | planned, and they're launching them using chemical upper stages
       | designed to explode into a thousand pieces at the target
       | altitude. This is sufficient for Kessler Syndrome all on its own,
       | without counting interactions with anything else up there. A
       | catastropic debris cascade at 800km percolates down to lower
       | altitudes over time and impacts.
       | 
       | We need viable treaties limiting development beyond 400 or 500km
       | and we need them ten years ago.
       | 
       | I don't know how to sell the urgency of this predicament. You can
       | have as many satellites as you want, a million uncoordinated
       | bodies, at 400km because direct collision potential scales with
       | (satellite count / orbital lifespan) ^2 . At 1000km, satellites
       | decay so slowly we are already too crowded; we have already
       | overused the space. We are speed-running the end of the space age
       | and we are doing it to save a small number of dollars and to
       | avoid a small amount of diplomacy.
       | 
       | This is not something we get a do-over on. There is no practical
       | way to collect ton-scale debris at present, no way to track
       | kilogram-scale debris, no practical way to shield pressure
       | vessels against gram-scale debris, and even milligram-scale
       | debris can hit with the force of a bullet. After collisions start
       | occurring at a rapid clip, the mass of potential impactors
       | quickly forms a long tailed lognormal distribution that denies us
       | space for centuries.
        
         | autoexecbat wrote:
         | > upper stages designed to explode into a thousand pieces at
         | the target altitude
         | 
         | By this do you mean at the 800km altitude?
        
           | mapt wrote:
           | Yes. In a lot of historical spaceflight programs, the stage
           | used in the upper atmosphere stayed with you to the final
           | orbit, and was detached at low speed there. This saved you
           | from having to design your satellite with significant onboard
           | propulsion. Some of the upper stages were able to vent
           | remaining propellants or pressurants, some were allowed to
           | heat up until the pressure vessel exploded.
           | 
           | Suffice it to say this is not sustainable for
           | megaconstellations in thousand years orbits. The responsible
           | thing to do with that kind of scale involves reliable,
           | redundant, prompt de-orbit of upper stages, and ideally for
           | high-thrust, high-mass, high-engineering-margin-of-error
           | atmospheric upper stages never to make it that far into the
           | mission.
        
         | bamboozled wrote:
         | One way is for the the US to be more politically stable again
         | (some how). Every country with an army will want its own star
         | link now for trust reasons.
        
           | mapt wrote:
           | For how long?
           | 
           | Because this thing is happening right now, it's happening
           | fast, and it's happening without any effort to fight against
           | the trend.
           | 
           | If your answer is "let's revisit this in 2050", then it isn't
           | an answer.
        
             | bamboozled wrote:
             | Yeah well it means a lot of satellites are going to end up
             | in space then.
        
         | leptons wrote:
         | >I don't know how to sell the urgency of this predicament. You
         | can have as many satellites as you want, a million
         | uncoordinated bodies, at 400km because direct collision
         | potential scales with (satellite count / orbital lifespan) ^2 .
         | At 1000km, satellites decay so slowly we are already too
         | crowded; we have already overused the space. We are speed-
         | running the end of the space age and we are doing it to save a
         | small number of dollars and to avoid a small amount of
         | diplomacy.
         | 
         | This sounds like the most first-world-problem ever. It
         | realistically affects practically nobody alive, nor would it
         | ever. Most people will live and die on the planet's surface and
         | never visit space, nor do they need to. There aren't too many
         | space-based services that are really necessary to life on
         | earth. Nobody really _needs_ internet in the middle of nowhere.
         | Sure, it 's nice to have, but that's a first world problem that
         | few people have.
        
           | nwiswell wrote:
           | > It realistically affects practically nobody alive
           | 
           | Do people in the Global South not use GPS or consume weather
           | forecasts?
        
       | Oarch wrote:
       | There might be a cool storyline where we have to use enormous
       | ground based lasers to clean up and start again.
       | 
       | Could even look a bit like the iconic Gibraltar WW2 search lights
       | photographs.
        
         | jcgrillo wrote:
         | What would zapping a satellite with a laser achieve? I suppose
         | if you get it hot enough to melt everything, without anything
         | flying off, then it would turn into a spherical drop of molten
         | scrap... but then what?
        
           | ZYbCRq22HbJ2y7 wrote:
           | I assume the poster means to change its trajectory.
        
             | sfink wrote:
             | By adding energy (and momentum)? That seems unlikely to
             | work. I guess you could try to shoot at things headed
             | towards you over the horizon, to slow things down?
             | 
             | I was assuming it was to vaporize things to make the re-
             | condensed remnants small and dispersed enough to be less of
             | a problem. Though that seems like a tough problem if you
             | have to stay trained on an orbiting bolt for any length of
             | time, as the atmosphere wobbles your laser around.
        
           | aeternum wrote:
           | You ablate part of it on the prograde side to create a small
           | retrograde thrust which will deorbit it.
           | 
           | I think the right move is to merge this approach with goo
           | blobs. We launch a large goo blobs or nets into a few
           | strategic geostationary orbits and now you only have to
           | ablate objects so they hit the goo then deorbit the goo once
           | it is full (or just leave it there) as they would be large
           | known orbits.
        
       | 0xbadc0de5 wrote:
       | My understanding was always that LEO is much less of a Kessler
       | risk due to atmospheric friction - ie: in the absence of active
       | control and regular correction, LEO objects will gradually de-
       | orbit themselves. It's the the higher geostationary orbits that
       | pose the problem.
        
       | resters wrote:
       | Positioning a large, armored satellite in low or mid-Earth orbit
       | significantly enhances its strategic value for both offensive and
       | defensive anti-satellite operations. Such a platform could serve
       | as a pivotal asset in maintaining orbital dominance, offering
       | rapid response capabilities to neutralize threats and protect
       | critical infrastructure.
       | 
       | In other words, welcome various "death stars" to keep order
       | against malicious Kessler style attacks, etc.
        
       | donaldihunter wrote:
       | I love Sabine Hossenfelder's videos but the audio effects on the
       | transitions are killing me.
        
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