[HN Gopher] Are we ready to see satellites built on an assembly ...
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       Are we ready to see satellites built on an assembly line approach?
        
       Author : cosmosguru
       Score  : 39 points
       Date   : 2021-04-27 18:38 UTC (4 hours ago)
        
 (HTM) web link (blog.satsearch.co)
 (TXT) w3m dump (blog.satsearch.co)
        
       | walrus01 wrote:
       | This URL appears to be specific to 1U through 6U cubesats, which
       | are considerably smaller and less capable than a single starlink
       | satellite. Or Oneweb, the most recent other medium large volume
       | satellite manufacturing project.
       | 
       | Of course neither company is publishing any photos/schematics or
       | details whatsoever about their assembly line, because that's a
       | competitive advantage.
        
         | cosmosguru wrote:
         | These smaller satellites can support cameras, low data rate
         | communications like IOT via space, etc.
         | 
         | I guess if you consider space as the 'highway', the size of the
         | satellites can be motorcycles, small cars to big trucks!
        
         | portillo wrote:
         | There are multiple pictures of OneWeb's assembly line in their
         | website, https://onewebsatellites.com/factory/ , including
         | pseudo-blueprints: https://bit.ly/32QSDBS
         | 
         | Still far from what you would expect from a truly automated
         | production line, but it has dedicated stations that allows
         | workers to assemble multiple satellites in parallel.
        
       | kjrose wrote:
       | I think it is an interesting idea, but I fear that unless we find
       | a way to bring down the broken, disabled, etc. satellites we
       | have, this will lead to accelerating the possibility of a Kessler
       | Syndrome phenomena.
        
         | modeless wrote:
         | There is a simple and comprehensive solution to this problem
         | which SpaceX has already implemented for Starlink. Simply put
         | all of the satellites under 600 km altitude. Anything at that
         | altitude will fall out of orbit in a few years due to
         | atmospheric drag, unless it continuously boosts itself up. And
         | before you ask: no, collision debris is _not_ ejected into
         | orbits that decay significantly slower than the original
         | orbits, just due to how orbital mechanics work.
        
       | trothamel wrote:
       | With 1,300 Starlink satellites in orbit, and many thousands
       | scheduled to go up, I think we're already seeing the assembly
       | line approach to building satellites.
        
         | cosmosguru wrote:
         | There are favorites coming up in Europe, China, India and Japan
         | apart from the US.
         | 
         | It almost seems like taking a leaf out of the auto industry.
         | The question is, how many of these can survive eventually!
        
           | TrainedMonkey wrote:
           | Very few, capital cost to build and launch is quite
           | significant, cost to operate is significantly less, but still
           | substantial. You need a lot of subscribers to make this
           | worthwhile and this is likely will be winner take most tech
           | market. Left alone global LEO market would probably support
           | 1-2 constellations. Given geopolitical nature it is likely
           | that some constellations will be outlawed in certain areas.
           | SpaceX will likely capture a 75%+ portion of the market
           | everywhere it is not prohibited.
           | 
           | It is feasible to see project Kupier and One Web eventually
           | getting competitive with Starlink 1.0, but they are not
           | launching or innovating fast enough. By the time they are
           | ready to start offering V1 constellation SpaceX will be
           | launching V2 and testing V3. Long term the only real
           | competitor is China because they have a large protected
           | market and capable of subsidizing launch and scaling up
           | incredibly rapidly.
        
             | jupp0r wrote:
             | Sorry I can't resist but put my hacker hat on:
             | 
             | How would effective prohibition work? Beams are directed
             | enough to make them hard to find from a frequency
             | perspective. Payments will probably be possible in BitCoins
             | at some point given Teslas move in that direction.
             | Controlling the import of hardware seems like a way to do
             | it, but I bet it would still show up everywhere.
        
               | aurelianito wrote:
               | That's easy. If spacex does not respect the ban, China
               | will fire anti-satellite missiles to the spacex
               | constellation.
        
               | modeless wrote:
               | That's not easy. There will be tens of thousands of
               | satellites. It would be prohibitively expensive to hit
               | them all with missiles. Not to mention the debris cloud
               | which, while temporary, would cause real problems for
               | everyone in space for a few years.
               | 
               | More feasible attacks would be hacking the satellites or
               | ground systems, RF jamming, or just locating users on the
               | ground by their RF emissions and throwing them in the
               | gulag. Or how about holding the Shanghai Tesla factory
               | hostage? Less fancifully, China can put pressure on
               | SpaceX via the ITU. There are plenty of options for China
               | and there is zero chance SpaceX will try to break Chinese
               | law.
        
               | justaguy88 wrote:
               | Hitting one satellite is a hell of a warning shot though.
               | Literally no one wants the debris clouds.
               | 
               | Every country, US included, would pressure SpaceX to stop
               | operating in countries that don't want it if it were to
               | result in any debris.
        
               | fennecfoxen wrote:
               | no
               | 
               | no no
               | 
               | no no no
               | 
               | please. if you want to make Starlink illegal what you do
               | is state Starlink is illegal and maybe make it illegal to
               | pay Starlink. that's a lot cheaper and doesn't piss off
               | the international community.
        
       | bernardlunn wrote:
       | Anybody know how dead ones are recycled or is it junkyard in
       | space?
        
         | volkk wrote:
         | random question for anybody that can answer:
         | 
         | for satellites that are scheduled to be "deprecated," can we
         | use a different rocket to gently nudge them out of orbit and
         | have them float off into space? even if you nudge them at
         | something super low velocity like 100MPH into a direction,
         | presumably it would continue floating endlessly at 100MPH until
         | it would hit something?
         | 
         | i'm guessing the building a separate "rocket that nudges dead
         | satellites out of earths orbit" is extremely expensive?
        
           | simonh wrote:
           | I seriously recommend investing in a copy of Kerbal Space
           | Program. There is no better way to gain an intuitive grasp of
           | orbital mechanics.
        
           | knowaveragejoe wrote:
           | You would deorbit the sat and let it burn up into the
           | atmosphere. In orbit, you can't really "drift off into" space
           | like you're saying here.
        
           | dmurray wrote:
           | It doesn't work like this. If you nudge something in a
           | circular orbit by 100MPH, in general it moves into a very
           | slightly higher, lower, or more elliptical orbit. For a
           | typical satellite in LEO, the size of the "nudge" you need to
           | get it to "drift away" is comparable to all the rocket fuel
           | that went into getting it there in the first place.
        
             | trothamel wrote:
             | That isn't right, since all you have to do is lower the
             | orbit until it hits the atmosphere, and let that do all the
             | work. A Space Shuttle deorbit burn was ~90 m/s, versus the
             | 7,600 m/s that the ISS moves at. (With even more lost to
             | drag, gravity, etc, getting there.)
        
               | maccam94 wrote:
               | The ISS is in a relatively low orbit at ~400km altitude,
               | geostationary satellites are up at 35,000km and have
               | basically zero drag.
        
           | GlenTheMachine wrote:
           | "I'm guessing the building a separate "rocket that nudges
           | dead satellites out of earths orbit" is extremely expensive?"
           | 
           | Yes, at least as expensive as launching the original
           | satellite, if not more (because it has to have the ability to
           | intercept).
           | 
           | Also, just adding a little nudge doesn't really help. It
           | changes the orbit slightly, but it isn't like an additional
           | 44 meters per second (which is what 100 mph is) of velocity
           | is going to make the derelict spacecraft achieve escape
           | velocity. You'll just change the shape of the orbit some. You
           | need to add an additional ~ 3300 m/sec (7400 mph!) in
           | velocity to get to escape velocity.
           | 
           |  _Decreasing_ the velocity, such that the derelict eventually
           | de-orbits and burns up in the atmosphere is typically much
           | less expensive. A few hundred m /sec would probably do it,
           | but it depends a lot on what orbit the derelict starts in.
        
           | cookingrobot wrote:
           | If you give a satellite a shove, it will end up on a slightly
           | higher or lower (or eccentric) orbit depending which way you
           | shove. It won't keep floating off endlessly into space unless
           | you shove it with enough energy to get to escape velocity.
        
         | distribot wrote:
         | Like any other externality that isn't constrained by
         | regulation, the problem is raging out of control.
         | 
         | https://www.bloomberg.com/opinion/articles/2021-04-17/space-...
        
         | cosmosguru wrote:
         | There is a junkyard for GEO i.e 360000km orbit. But there are
         | now concepts and companies coming up to solve the junk problems
         | for the 500-2000km orbits - https://www.bbc.com/news/science-
         | environment-56420047
        
         | GlenTheMachine wrote:
         | "Recycled"? None.
         | 
         | Deorbited: quite a few. Depends on orbital altitude. Low-earth
         | orbit satellites generally deorbit by themselves eventually,
         | but at the upper range of low-earth orbit that can take a few
         | thousand years unless they are intentionally deorbited.
         | 
         | In geosynchronous orbit, nothing is ever deorbited, it's too
         | costly in terms of fuel. They are instead raised in altitude a
         | few hundred klicks to get them out of the way.
        
       | legulere wrote:
       | Are we ready to just see satellites and no stars anymore?
        
         | milesvp wrote:
         | I see a double edged sword here. We already have enough light
         | pollution that stars are hard to see in most cities. That
         | amount of pollution grows yearly as cost per lumen drops. The
         | problem ground based astronomers are having is the pollution
         | these low earth sats are having. This is the down side. What
         | makes me hopeful is how much better orbital optics can be.
         | Couple this with signal processing and scores of telescopes in
         | orbit, and you could create a virtual lens many times larger
         | and clearer than anything planet side.
         | 
         | As the price for getting satellites into orbit drops I imagine
         | astronomy having some pretty major breakthroughs.
         | 
         | That's at least my hope. Most of what I've been watching is low
         | orbit satellites but I don't know how high an orbit you'd want
         | for the kinds of things I'm imagining.
        
         | cosmosguru wrote:
         | Something that many in the astronomy community are asking
         | https://www.cnbc.com/2020/04/29/elon-musks-spacex-reducing-s...
        
           | bpodgursky wrote:
           | The opacity desires of astronomy are different than human
           | eyes. Painting satellites black (ongoing w/ Starlink) is
           | enough to make them dark to the human eye.
        
       | turbinerneiter wrote:
       | I wonder if it will make sense to go back to multi sensor
       | platforms. We could have a fleet of platforms in different
       | altitudes, combining different sensors and comm tech. Might be
       | better than to have a fleet for every specific wavelength (for
       | observation) and radio band.
        
         | cosmosguru wrote:
         | The problem is how do you do that when 20 companies are flying
         | the same type of satellites and are fighting for customers with
         | almost similar capabilities. If it was a question of science or
         | governmental cooperation, such agreements may be easier.
        
       | ratsmack wrote:
       | With the number of satellites slated to go up, there will be
       | enough shade to cool the earth and save us from climate change.
        
         | dmd wrote:
         | I know you're not being serious, but I like estimating stuff
         | like this.
         | 
         | The biggest solar panel array in space right now, AFAIK, is the
         | ISS at 2500 m^2.
         | 
         | There are currently ~6000 satellites in (any) orbit. Starlink
         | has 12000 more planned. Let's go nuts and say there's gonna be
         | 50000 total satellites.
         | 
         | Let's say ALL of them are as big as the ISS's, ridiculous as
         | that is. And let's say they cast a 1:1 shadow, even though
         | that's also patently ridiculous. I'm just making all of these
         | number as big as possible so nobody can possibly say "no, it's
         | bigger".
         | 
         | 2500 m^2 * 50000 = 125 square kilometers.
         | 
         | So with _many_ times the number of satellites planned, with
         | each one being anywhere between 50 and 100 times as big as it
         | really is, with each one casting a shadow as big as it is... we
         | shade - out of the entire planet - an area about 1.5 the size
         | of Manhattan.
        
           | Kye wrote:
           | You don't need to cover the whole planet, just the parts
           | under the sun. I'm not an orbital machinist, but maybe we
           | could park just enough blockers in an orbit that's always
           | between the sun and Earth to halt the warming. How much of
           | the sun would need to be blocked to bend the curve down?
           | Everything necessary on the ground to stop putting CO2 in the
           | air is already underway. All we need is more time.
        
             | edrxty wrote:
             | This is something that's been considered, particularly for
             | doing things like terraforming Venus. There are these areas
             | called Lagrange points[1] that provide a location where one
             | can park a satellite where it'll remain stationary relative
             | to the two-body system of interest. The point directly
             | between the sun and earth is the L1 point and allows you to
             | place a sunshade such that it'll always be directly between
             | the sun and earth. It should be noted, however, that these
             | points are generally not stable and so require some degree
             | of station-keeping to remain viable long term.
             | 
             | [1] https://en.wikipedia.org/wiki/Lagrange_point
        
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