superconducting nanowire single-photon detectors
It would seem to me that launching a few receivers in LEO (above the clouds) where they could receive the data and then transmit it back either through integrating with Starlink's distribution system or directly to ground stations would be a reasonable investment, if laser communications is the future.
It's interesting that they went with liquid helium cooling for detection at 1550nm rather than more conventional telcom detectors based on ingaas at non-cryogenic temperatures. I suspect that long term they can probably improve the hardware enough that cryogenic cooling isn't needed.If you want to read more about RealTOR (the COTS Superconducting Nanowire Single-Photon Detectors (SNSPDs)), you can read it here.
https://www.nasa.gov/glenn/glenn-ex...tion/scan/real-time-optical-receiver-project/
Is this comparing the optical amplifier power to a modem + amplifier (s-band transmitter)? I don't think this is correct as an apples to apples comparison, typically optical systems are 10's to 100's of W for the full chain. The actual final gain amp may be on that order but its far from the only part you need to make the system work.For example, on Orion, the S-band transmitter required 5 to 20 watts of power, compared to the laser communications transmitter, which used just a single watt.
It's likely that SpaceX has built their kit to look for other objects in orbit rather than out into the general void. Though I'm sure they'd enjoy the cash if they were contracted to put stuff up to do it.There's probably a reason, but if space-to-space is feasible and SpaceX has already done it for satellites, why cant they do space-to-space optically then normal satellite-to-ground using whatever SpaceX/DirectTV use to send bandwidth to Earth?
All this also likely needs to be corrected to Mbps.Apollo returned data to Earth at about 50KB per second using radio frequencies. Similarly, Orion used S-band for a slightly higher communication rate most of the time, at 3MB to 5MB per second.
I didn't find hard data, but most likely this was the rated RF output power. The way it's phrased can make people think this was the power consumption of the transmission equipment — which in reality is about twice as much. I'm sure some engineers here can chime in.on Orion, the S-band transmitter required 5 to 20 watts of power, compared to the laser communications transmitter, which used just a single watt.
Eh? If they’re using an efficient codec like HEVC this is probably achievable at acceptable bit rates. 700 MB isn’t a huge output size for a 2h video in this regard, so about 25-30 seconds to transmit at 260 Mbps?"260 Mbps. At those speeds, the crew could have transmitted a full high-definition movie to Earth in seconds."
Really? Because either your figure is off by a few orders of magnitude or your math is just plain wrong...
My bad, you are probably right.Eh? If they’re using an efficient codec like HEVC this is probably achievable at acceptable bit rates. 700 MB isn’t a huge output size for a 2h video in this regard, so about 25-30 seconds to transmit at 260 Mbps?
Surely not -- there wasn't a single mention of reversing the polarity of anything!We are living in science fiction. That sounds like something a Star Trek crewman would suggest to solve the problem of the week.
Most likely it requires a decent telescope at the receiving end to achieve decent bandwidth. Nothing Hubble-grade, but on the order of a high-end hobbyist telescope -- 8-12" primary aperture, say. I'm basing that on some foggy memories of presentations at various conventions over the years from people working on interplanetary laser comms.There's probably a reason, but if space-to-space is feasible and SpaceX has already done it for satellites, why cant they do space-to-space optically then normal satellite-to-ground using whatever SpaceX/DirectTV use to send bandwidth to Earth?
Eh? If they’re using an efficient codec like HEVC this is probably achievable at acceptable bit rates. 700 MB isn’t a huge output size for a 2h video in this regard, so about 25-30 seconds to transmit at 260 Mbps?
Rather than a LEO constellation with all the associated issues of target tracking, my assumption would be some sort of low-count constellation in MEO or maybe GEO (slower orbit, less tracking hassle, handoffs less often), of lasercomm units pointed outwards, and using TDRSS/DSS for the "last mile" to Earth's surface. Starlink probably wouldn't work unmodified (pointing the wrong way, for one thing), but a future-gen Starlink or a Starshield variant optimized for NASA usage seems entirely possible. Not to mention the various Starlink competitors coming down the pipe.
I suppose I just gave Eric the benefit of the doubt on this one since it didn’t strike me as a major blunder.25 to 30 seconds is not what most people think of as seconds. If it had said in less than a minute that would be a lot more realistic. 260 Mbps is ~ 2GB per minute.
By and large, the Starlink inter-satellite laser links are focused on targets that don't move very much. Each bird has a link ahead of and behind it, to satellites in the same orbital plane, so they're effectively stationary to its own flight path, and a link to the satellites to the right and left of them, in different orbital planes. These move very slowly most of the time, but they do cross from right to left and left to right when the birds in question reach their maximum latitude.There's probably a reason, but if space-to-space is feasible and SpaceX has already done it for satellites, why cant they do space-to-space optically then normal satellite-to-ground using whatever SpaceX/DirectTV use to send bandwidth to Earth?
Sending signals is trivial. We aren't limited to a single watt for transmission. You can massively up the intensity of the signal and then you don't have to rely on nearly perfect superconducting photon sensors. One can also make larger focusing mirrors so that you can focus to a very tight spot where your orbiter is.Would it be feasible for at least some Starlink satellites to have a space-facing laser sensor?
If so, they cover all the globe and could be used as a kind of "last mile" relay, at least for reception.
Two way would be a different beast though.
We are living in science fiction. That sounds like something a Star Trek crewman would suggest to solve the problem of the week.
yeah, but maintenance and servicing and upgrade is a whole lot easier for 40 ground based 1 meter telescopes than 4 in GEO. As I recall, an off the shelf 1 meter telescope with all the positioning, etc. is less than $1M. $5M for the complete ground station is pretty easy to imagine, esp if we’re not doing fancy cryogenic receivers, so $200M for the whole network (which could be used for other things, too). And if one breaks, putting in a new station is easy.Sending signals is trivial. We aren't limited to a single watt for transmission. You can massively up the intensity of the signal and then you don't have to rely on nearly perfect superconducting photon sensors. One can also make larger focusing mirrors so that you can focus to a very tight spot where your orbiter is.
As to a distributed array, I don't know how much benefit that is for receiving. NASA says they need 40 ground-based, world-wide sensors to ensure cloudless access. I suspect the transmission beam isn't that large such that you could detect the emissions from opposite sides of the earth. Instead, the emitter aims at southern Australia (e.g.) or possibly even a tighter spot than that. As such, if you only had 3 or 4 satellites in polar orbit, you're pretty likely to have one in visual range that isn't being blinded by the sun.