Airbus to build giant satellite network
bbc.co.uk
bbc.co.uk
If we assume the reporters got random factoids mixed up, 600 satellites? in 20 "planes" ? (lets assume they are somehow station keeping in the same orbital plane so 30 satellites each trying to stay 12 degrees away from the next satellite in the same plane, while trying to avoid the other 19 planes? One gets destroyed by space junk and you practically guarantee another 29 join it over the next 120 minutes or so? That is going to be quite the dance.
And what spectrum are they using for uplink/downlink? .5 Thz? Something they can get a license for all over the world presumably. That alone cost a billion dollars for Iridium.
I just can't imagine a scenario where this even works. Perhaps if they start with the old TeleDesic design or something.
"Only slightly more seriously, it would be very impressive
if they could pull it off, but having seen the deployment of
Iridium (66), GPS (32), GLONASS (24) , and Galileo (30) it
doesn't seem like we have a non-nation state that is up to
the challenge of putting 600(!) satellites into orbit all at
once."
It looks like these satellites will be a lot smaller than Iridium ones -- from the BBC article, about 150 kg each, vs. ~689 kg [0] for Iridiums. The total orbiting mass is only twice that of the Iridium constellation.600 * 150 kg = 90,000 kg
66 * 689 kg = 45,474 kg
Naively, they could lift everything in maybe five Ariane V (ECA) launches, for ~$1 billion at market pricing [1]. That'd mean packing over a hundred microsats in one payload fairing. I'm not sure how close this is to reality: I'd guess there'd need to be a lot of structure overhead too.
[0] https://en.wikipedia.org/wiki/Iridium_satellite_constellatio...
[1] http://www.spaceflight101.com/ariane-5-eca.html
($200 MM/launch, 21,000 kg payload to LEO)
Although there are other potential options (EDTs, etc, etc) that don't have as much difficulty with scaling.
That's not what they'll be using, though. They'll be using Hall Effect thrusters.
With satellites and chemical thrusters, it's pretty much "the lightest possible". Thrust to mass ratio is almost irrelevant. Almost any thruster will have the thrust required.
And I'm kind of surprised by the ion thrusters. I wouldn't assume that they had the thrust required to stationkeep in LEO - the drag in LEO being as high as it is.
At around ~800km, solar sails start to become practical because aerodynamic drag drops below photon pressure.
Ion thrusters and photovoltaics are COTS techs which are vastly more powerful than solar sails, which exist only at the prototype/demo stage.
Ion thrusters are practical to fight drag down to around ~200km given the right design, or are perfectly happy at 300-350 given a typical suboptimal design. GOCE managed it down to ~230km, after performing a multiyear mission at ~260km: http://www.spaceflight101.com/goce-re-entry.html
And interesting. Always nice to see hard numbers.
It might be bad for truly tiny sats, but we're talking about 150kg vs. 700kg. 1kg is perfectly fine for those.
They chose a very high section of LEO, though, 1200km, where debris lasts millennia. Further populating high orbits like this without a solid plan for deorbit is problematic - not for OneWeb, but for the rest of us who don't want to see a Kessler Syndrome cascade thirty years down the road.
"End of Life Disposal When a OneWeb satellite nears the end of its intended service life, it will de-orbit automatically, ensuring that the space around our planet remains free and clear for future generations."
So at least they've thought about that.
(It's very promotional though, not very technical)
They have set for themselves quite the challenge.
Operating in a single orbital plane is really not as hard as you're imagining it to be. We do it all the time. And there are tens of thousands of large objects in Earth orbit, but we only detect collisions every several years.
How they plan to accomplish that is not clear to me.
EDIT: Look for "Progressive Pitch" on the web page.
As for interference: They're planning on beaming signal to a wide swath of every plane for full-Earth coverage, not just at a narrow stretch near nadir. That means you'll have users acquiring a fix from a wide swath of sky; Let's say 45 degrees from zenith in various directions. That would make every user below 45 degrees latitude encounter fixes with OneWeb proximate to the geosynchronous belt on a regular basis.
If spectral separation alone was insufficient to prevent interference, it's not something that would affect communications when a satellite is near the equator at all, it's something that would affect all the satellites nearly all the time. A 1200km orbit is 30x closer to Earth than the geosynchronous belt.
http://spacenews.com/virgin-qualcomm-invest-in-global-satell...
(or on my earlier link or Wikipedia)
But it must not be thruster based.
I really doubt they're going to hit anything, at least in a way that hurts more than one sat.
This is one of the things where investing in a fast moving technology reminds me of deflationary economy - we are putting a lot of satellites up there and spending billions doing it when tech is accelerating at such a fast rate that in 10 years the electronics will be quite dated, so it might be worth a wait. There is no easy way to update electronics on these once they're up.
Suppose billionaires wants to have a legacy in space before their time on earth is done!
Personally can't wait until this is cheap enough for normal individuals/startups. Low orbit nanosats can be done for $20k-ish already - www.economist.com/news/technology-quarterly/21603240-small-satellites-taking-advantage-smartphones-and-other-consumer-technologies
Going to get crowded up there!
And arguably if you put a server on a satellite, governments will be the only entities capable of reaching it.
Maybe they don't even need to be profitable if they also serve some sort of propaganda/free speech function for regions of the world that the developed West wants to poke at.
People having a satellite dish pointed at a satellite there would be in the range of hundreds of millions alone in europe.
But the point is, that if some country decides the new internet via satellite to be illegal, it is _very_ easy for them to find people using it.
A dish leaks very little energy except in the direction of the satellite. It could be astronomically unlikely anyone could detect its use unless they were line-of-sight between the dish and the satellite. And pointed in the right direction.
If you want internet via satellite, they are transmitting, and while they are directional towards the satellite, there's enough signal going off in other direction sides making it not that hard to detect from the ground.
Ballistic missile defense is a very interesting field. It actually seems uncannily defensive given the rest of the "Defense" Industry, ignoring potentially destabilizing MAD. =P
Few unmanned spacecraft flown to date are in principle more complex than a Toyota. If you did 1-unit automotive production runs, and 1-unit production runs for most of the parts rather than using standardized templates, things would be expensive there too.
My main question is how fast is it going to be? Can I expect 10Mbps to each terminal / user?
If they're so british why don't they think they should pay tax like the rest of us?
Of course, it's still a tax dodge and the company should pay tax like the rest of most of the world!
This excludes many types of internet use cases.
That'll definitely be lower than that (at that kind of height, you wouldn't need hundreds of satellites for global coverage). Wiki page talks about 800km and 950km orbits.