Wasn\'t this impossible ?...

On 8/23/2020 7:40 PM, bitrex wrote:
On 8/23/2020 7:23 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 3:39:30 PM UTC-4, bitrex wrote:
On 8/23/2020 3:29 PM, bitrex wrote:
On 8/23/2020 3:25 PM, bitrex wrote:
On 8/23/2020 1:15 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 8:11:26 AM UTC-4, John S wrote:
On 8/21/2020 8:10 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 11:55:30 AM UTC-4, bitrex wrote:
On 8/21/2020 6:38 AM, Phil Allison wrote:

Hi,

Recently it has become normal for astronomers to directly
observe planets around nearby stars in an optical telescope.

Couple of months ago, they found two in circular orbit around a
very new star.

https://www.businessinsider.com.au/first-ever-photo-shows-2-planets-orbiting-sun-like-star-2020-7?r=US&IR=T



Seems there are in fact billions of the damn things.

Be \"...  an awful waste of space \" if Earth is the only one
with life forms.

Above quote from the SF movie \"Contact\".



.....  Phil



I\'m probably remembering the exact figures incorrectly but if
you could
push a space telescope out to about a tenth of a light-year from
Earth,
it could leverage gravitational lensing to make an equivalent
lens of
enormous size.

It could then search for evidence of life in a large volume of
space by
imaging planetary surfaces around other star systems directly,
it could
resolve stuff like oceans, plants, or structures.

But the time required to return those images would be...
astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first.
The farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand.  I\'m referring to the RF link analysis.  They
have a very hard time seeing anything other than stars because
other objects are too dim.  I haven\'t done the math, but the data
rate would have to be microscopic to successfully send and receive
a radio signal from such distances.  0.1 light year is 6324 AUs.
The Voyager probes are about 141 AU so about 40 times closer.  They
now are transmitting at 160 bps.  Doing the math I get about 3
years to transmit a MB of data.

? 10Mb/160bps = 62.5k seconds = 17.4 hours. What am I doing wrong?

Not as bad as I thought, but I suppose they would highly value any
image compression, but lossless of course.  With the image mostly
the star, I suppose they could do a fair bit of compression.
Still, they would want to transmit and awful lot of MB, so it will
take lots of time, still years.

Imagine what it would take to manage the cameras and other devices.
Over a month just to send any message no matter how short.


160 bps is what they have now, not from 0.1 light years away.  Apply
the -17 dB factor and recalculate...  I think the distance ratio is
actually 45.  Opps, I think I made a mistake.  It should be -33 dB,
no?  I used 10log instead of 20log.  So yeah, years.

I suppose they could just pop in a power source 2,000 times more
powerful.  How many kW would that be?  Or is it MW?  Not MW, they are
currently using 23 watt transmitters, so 45 kW instead, only slightly
less than WWVB.  Can we launch WWVB into space?


You\'d use a laser of some type, probably. One megawatt laser through
40 meter optics should be at least detectable by similar optics up to
20,000 light-years away:

https://iopscience.iop.org/article/10.3847/1538-4357/aae380

At a thousand AU you\'d need more than 25 watts, but likely not
megawatts. I don\'t think a radioisotope-thermal source would cut it
but small fission reactor might work.

Optical nuclear-electric battery seems like a plausible power source,
better power-to-weight than radioisotope thermal, less complexity than
something with circulating coolant

https://en.wikipedia.org/wiki/Optoelectric_nuclear_battery#:~:text=An%20opto%2Delectric%20nuclear%20battery,constituting%20a%20%22dust%20plasma%22.



Or you could just have the whole power-generation system on Earth for a
relatively (heh) short distance like that. A huge-ass 100 megawatt laser
beams power to the spacecraft\'s solar panels and uses the electric power
to run its ion drive to accelerate it up and slow it down, and at 1000
AU there\'s enough received power from the huge-ass laser on Earth to run
a downlink laser back. Flight time would be about 20 years

What speed could be achieved?  1000 AU is still 6 times closer than
0.1 light year.


When I first typed up my post I overstated the distance to get a
gravitational-lens effect off the Sun\'s own gravity well. 500-1000 AU
should be enough. Nuclear thermal rocket, specific impulse ~1000 seconds
could do 1000 AU with basically current technology well within a human
lifetime. Ion/plasma drive, specific impulse 50,000 seconds, cuts it
down to 10 years maybe.

To go faster than in reasonable time that you need something far beyond
near-future tech. Fusion ramjet cuts it down to 3 months or so I think,
but you might as well send it on to the nearest star at that speed.

The fusion ramjet has hardly left the garage at that point that is to
say, it isn\'t even up to cruise speed
 
On 8/23/2020 7:40 PM, bitrex wrote:
On 8/23/2020 7:23 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 3:39:30 PM UTC-4, bitrex wrote:
On 8/23/2020 3:29 PM, bitrex wrote:
On 8/23/2020 3:25 PM, bitrex wrote:
On 8/23/2020 1:15 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 8:11:26 AM UTC-4, John S wrote:
On 8/21/2020 8:10 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 11:55:30 AM UTC-4, bitrex wrote:
On 8/21/2020 6:38 AM, Phil Allison wrote:

Hi,

Recently it has become normal for astronomers to directly
observe planets around nearby stars in an optical telescope.

Couple of months ago, they found two in circular orbit around a
very new star.

https://www.businessinsider.com.au/first-ever-photo-shows-2-planets-orbiting-sun-like-star-2020-7?r=US&IR=T



Seems there are in fact billions of the damn things.

Be \"...  an awful waste of space \" if Earth is the only one
with life forms.

Above quote from the SF movie \"Contact\".



.....  Phil



I\'m probably remembering the exact figures incorrectly but if
you could
push a space telescope out to about a tenth of a light-year from
Earth,
it could leverage gravitational lensing to make an equivalent
lens of
enormous size.

It could then search for evidence of life in a large volume of
space by
imaging planetary surfaces around other star systems directly,
it could
resolve stuff like oceans, plants, or structures.

But the time required to return those images would be...
astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first.
The farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand.  I\'m referring to the RF link analysis.  They
have a very hard time seeing anything other than stars because
other objects are too dim.  I haven\'t done the math, but the data
rate would have to be microscopic to successfully send and receive
a radio signal from such distances.  0.1 light year is 6324 AUs.
The Voyager probes are about 141 AU so about 40 times closer.  They
now are transmitting at 160 bps.  Doing the math I get about 3
years to transmit a MB of data.

? 10Mb/160bps = 62.5k seconds = 17.4 hours. What am I doing wrong?

Not as bad as I thought, but I suppose they would highly value any
image compression, but lossless of course.  With the image mostly
the star, I suppose they could do a fair bit of compression.
Still, they would want to transmit and awful lot of MB, so it will
take lots of time, still years.

Imagine what it would take to manage the cameras and other devices.
Over a month just to send any message no matter how short.


160 bps is what they have now, not from 0.1 light years away.  Apply
the -17 dB factor and recalculate...  I think the distance ratio is
actually 45.  Opps, I think I made a mistake.  It should be -33 dB,
no?  I used 10log instead of 20log.  So yeah, years.

I suppose they could just pop in a power source 2,000 times more
powerful.  How many kW would that be?  Or is it MW?  Not MW, they are
currently using 23 watt transmitters, so 45 kW instead, only slightly
less than WWVB.  Can we launch WWVB into space?


You\'d use a laser of some type, probably. One megawatt laser through
40 meter optics should be at least detectable by similar optics up to
20,000 light-years away:

https://iopscience.iop.org/article/10.3847/1538-4357/aae380

At a thousand AU you\'d need more than 25 watts, but likely not
megawatts. I don\'t think a radioisotope-thermal source would cut it
but small fission reactor might work.

Optical nuclear-electric battery seems like a plausible power source,
better power-to-weight than radioisotope thermal, less complexity than
something with circulating coolant

https://en.wikipedia.org/wiki/Optoelectric_nuclear_battery#:~:text=An%20opto%2Delectric%20nuclear%20battery,constituting%20a%20%22dust%20plasma%22.



Or you could just have the whole power-generation system on Earth for a
relatively (heh) short distance like that. A huge-ass 100 megawatt laser
beams power to the spacecraft\'s solar panels and uses the electric power
to run its ion drive to accelerate it up and slow it down, and at 1000
AU there\'s enough received power from the huge-ass laser on Earth to run
a downlink laser back. Flight time would be about 20 years

What speed could be achieved?  1000 AU is still 6 times closer than
0.1 light year.


When I first typed up my post I overstated the distance to get a
gravitational-lens effect off the Sun\'s own gravity well. 500-1000 AU
should be enough. Nuclear thermal rocket, specific impulse ~1000 seconds
could do 1000 AU with basically current technology well within a human
lifetime. Ion/plasma drive, specific impulse 50,000 seconds, cuts it
down to 10 years maybe.

To go faster than in reasonable time

Er that phrase doesn\'t make sense :) \"to go faster\" will do fine
 
On 8/23/2020 7:26 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 4:09:51 PM UTC-4, bitrex wrote:
On 8/22/2020 11:34 PM, Ricketty C wrote:
On Saturday, August 22, 2020 at 3:04:21 PM UTC-4, upsid...@downunder.com wrote:
On Sat, 22 Aug 2020 08:41:34 -0700 (PDT), Ricketty C
gnuarm.deletethisbit@gmail.com> wrote:

On Saturday, August 22, 2020 at 4:19:44 AM UTC-4, Martin Brown wrote:
On 22/08/2020 02:10, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:

But the time required to return those images would be...
astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first. The
farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand. I\'m referring to the RF link analysis. They have
a very hard time seeing anything other than stars because other
objects are too dim. I haven\'t done the math, but the data rate
would have to be microscopic to successfully send and receive a radio
signal from such distances. 0.1 light year is 6324 AUs. The Voyager
probes are about 141 AU so about 40 times closer. They now are
transmitting at 160 bps. Doing the math I get about 3 years to
transmit a MB of data.

It is slightly amazing that the Voyagers can be received at all now. The
transmitters on the probes are fixed 1970\'s space approved technology
with limited power and quite crude by modern communications standards.
The error correction was very sophisticated for the time though.

The base station receivers have improved so much since the probes were
launched that they can still follow Voyager out to the heliopause.

Data rates for a future deep space probe should be about the same order
of magnitude as the recent probe to Pluto managed but downgraded by the
increase in distance effects on signal to noise.

Yes, that is the problem. The distance hugely weakens the signals in both directions.

Only -6 dB for each doubling of the distance.

\"Only\" is a four letter word!

And how is the data rate impacted by a -17 dB adjustment to signal strength? You have to consider they are pushing the limit of what they can do working at 160 bps presently. We have done a lot to improve the ground stations, but they can\'t keep increasing their transmit power ad infinitum. As I said, it will take years, maybe decades to transmit a high resolution image from a space craft that far away. While larger antenna in general produce a more collimated beam, there are limits to what you can do given the precision of the antenna shape and the frequency you transmit on.


Cheapest bang-for-the-buck per-unit mission profile I think is keep the
power supply on Earth, a large laser, or array of lasers. Keep the
spacecraft as lightweight as possible. Fire it out into interstellar
space towards 1000 AU fast as it can go, using its instruments/optics to
take in all the data it can on the way, big sail of solar panels feeding
the ion/plasma drive or whatever from the laser beam.

Then at some point when received power is insufficient to run everything
flip it around and shut down everything but the downlink laser and use
the optics in reverse to beam the data back. Send as much as it can
before it goes out of range completely.

And how far would that be with this laser?

Beats me! Have to talk to some kind of NASA-person! ;) I\'m just enjoying
speculating beyond my depth in ways that are unlikely to get anyone
hurt, at least for the foreseeable future lol
 
On Sunday, August 23, 2020 at 7:29:25 PM UTC-4, bitrex wrote:
On 8/23/2020 7:19 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 3:25:11 PM UTC-4, bitrex wrote:
On 8/23/2020 1:15 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 8:11:26 AM UTC-4, John S wrote:
On 8/21/2020 8:10 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 11:55:30 AM UTC-4, bitrex wrote:
On 8/21/2020 6:38 AM, Phil Allison wrote:

Hi,

Recently it has become normal for astronomers to directly observe planets around nearby stars in an optical telescope.

Couple of months ago, they found two in circular orbit around a very new star.

https://www.businessinsider.com.au/first-ever-photo-shows-2-planets-orbiting-sun-like-star-2020-7?r=US&IR=T

Seems there are in fact billions of the damn things.

Be \"... an awful waste of space \" if Earth is the only one with life forms.

Above quote from the SF movie \"Contact\".



..... Phil



I\'m probably remembering the exact figures incorrectly but if you could
push a space telescope out to about a tenth of a light-year from Earth,
it could leverage gravitational lensing to make an equivalent lens of
enormous size.

It could then search for evidence of life in a large volume of space by
imaging planetary surfaces around other star systems directly, it could
resolve stuff like oceans, plants, or structures.

But the time required to return those images would be... astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first.
The farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand. I\'m referring to the RF link analysis. They have a very hard time seeing anything other than stars because other objects are too dim. I haven\'t done the math, but the data rate would have to be microscopic to successfully send and receive a radio signal from such distances. 0.1 light year is 6324 AUs. The Voyager probes are about 141 AU so about 40 times closer. They now are transmitting at 160 bps. Doing the math I get about 3 years to transmit a MB of data.

? 10Mb/160bps = 62.5k seconds = 17.4 hours. What am I doing wrong?

Not as bad as I thought, but I suppose they would highly value any image compression, but lossless of course. With the image mostly the star, I suppose they could do a fair bit of compression. Still, they would want to transmit and awful lot of MB, so it will take lots of time, still years..

Imagine what it would take to manage the cameras and other devices. Over a month just to send any message no matter how short.


160 bps is what they have now, not from 0.1 light years away. Apply the -17 dB factor and recalculate... I think the distance ratio is actually 45. Opps, I think I made a mistake. It should be -33 dB, no? I used 10log instead of 20log. So yeah, years.

I suppose they could just pop in a power source 2,000 times more powerful. How many kW would that be? Or is it MW? Not MW, they are currently using 23 watt transmitters, so 45 kW instead, only slightly less than WWVB.. Can we launch WWVB into space?


You\'d use a laser of some type, probably. One megawatt laser through 40
meter optics should be at least detectable by similar optics up to
20,000 light-years away:

https://iopscience.iop.org/article/10.3847/1538-4357/aae380

At a thousand AU you\'d need more than 25 watts, but likely not
megawatts. I don\'t think a radioisotope-thermal source would cut it but
small fission reactor might work.

What exactly does it mean to use 40 meter optics on a laser beam? Are you suggesting the optics need to be far enough away from the laser that the inherent limitation of the coherence of the laser beam create a 40 meter wide beam? That would be a pretty big distance. One huge antenna array!

Perhaps I don\'t understand the meaning of 40 meter optics in this context?

I believe it means you use a lens or mirror of that scale to
focus/collimate the beam from your emitter. Like telescope but in reverse..

You aren\'t getting it. Why would you need a 40 meter lens or mirror to collimate a collimated laser beam that is so much tinier? Does the laser produce a beam 40 meters wide?


A MW is a bit more than 23 watts. A \"small\" fission reactor indeed. I realize they don\'t need to power it up until it is safely away from people, but the electronics need to operate in this environment. Can that be done in a weight that is practical to leave Earth orbit?


Yeah they\'ve flown fission reactors in space:

https://en.wikipedia.org/wiki/TOPAZ_nuclear_reactor

\"The first TOPAZ reactor operated for 1,300 hours and then was shut down
for detailed examination. It was capable of delivering 5 kW of power for
3–5 years from 12 kg (26 lb) of fuel. Reactor mass was ~ 320 kg (710 lb).\"

But you\'re going to need some more juice than that if you want to power
your ion/plasma drive that\'s going to take your probe out that far in
less than a human lifetime. Might as well power the communication laser
off the drive reactor or whatever power source if you\'re going to put
the propulsion energy source on board too.

It\'s still not clear to me you can communicate faster than some microscopic data rate. Just as laser beams are not perfectly collimated, it gets to be much, much harder to direct any energy beam is such a concentrated form.

--

Rick C.

-++ Get 1,000 miles of free Supercharging
-++ Tesla referral code - https://ts.la/richard11209
 
On Sunday, August 23, 2020 at 6:12:03 PM UTC-7, Ricketty C wrote:

> Why would you need a 40 meter lens or mirror to collimate a collimated laser beam that is so much tinier? Does the laser produce a beam 40 meters wide?

Lasers, like radio, have a wavelength, and diffraction limits their collimation.
A laser cavity 40 meters wide can do well over astronomical distances, was my
reading. A HeNe laser (6.3 E -7 m wavelength) at 20k lightyears (1.9 E 19 meter)
which starts at 40M, spreads by (6.3E-7/(2*pi*40)) = 2.5 E-9 radians
to make a spot-width of 4.7 E10 meters... ten times the \'orbit of Pluto\' solar
system size.

Maybe it\'s not as good throughput as you\'d want to transmit live-action SpongeBob
videos, but a weekly postcard isn\'t out of the question.

Or, gumdrops (about 1 gram of material) accelerated to 0.1c, having a wavelength of
 
On 8/23/2020 9:11 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 7:29:25 PM UTC-4, bitrex wrote:
On 8/23/2020 7:19 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 3:25:11 PM UTC-4, bitrex wrote:
On 8/23/2020 1:15 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 8:11:26 AM UTC-4, John S wrote:
On 8/21/2020 8:10 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 11:55:30 AM UTC-4, bitrex wrote:
On 8/21/2020 6:38 AM, Phil Allison wrote:

Hi,

Recently it has become normal for astronomers to directly observe planets around nearby stars in an optical telescope.

Couple of months ago, they found two in circular orbit around a very new star.

https://www.businessinsider.com.au/first-ever-photo-shows-2-planets-orbiting-sun-like-star-2020-7?r=US&IR=T

Seems there are in fact billions of the damn things.

Be \"... an awful waste of space \" if Earth is the only one with life forms.

Above quote from the SF movie \"Contact\".



..... Phil



I\'m probably remembering the exact figures incorrectly but if you could
push a space telescope out to about a tenth of a light-year from Earth,
it could leverage gravitational lensing to make an equivalent lens of
enormous size.

It could then search for evidence of life in a large volume of space by
imaging planetary surfaces around other star systems directly, it could
resolve stuff like oceans, plants, or structures.

But the time required to return those images would be... astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first.
The farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand. I\'m referring to the RF link analysis. They have a very hard time seeing anything other than stars because other objects are too dim. I haven\'t done the math, but the data rate would have to be microscopic to successfully send and receive a radio signal from such distances. 0.1 light year is 6324 AUs. The Voyager probes are about 141 AU so about 40 times closer. They now are transmitting at 160 bps. Doing the math I get about 3 years to transmit a MB of data.

? 10Mb/160bps = 62.5k seconds = 17.4 hours. What am I doing wrong?

Not as bad as I thought, but I suppose they would highly value any image compression, but lossless of course. With the image mostly the star, I suppose they could do a fair bit of compression. Still, they would want to transmit and awful lot of MB, so it will take lots of time, still years.

Imagine what it would take to manage the cameras and other devices. Over a month just to send any message no matter how short.


160 bps is what they have now, not from 0.1 light years away. Apply the -17 dB factor and recalculate... I think the distance ratio is actually 45. Opps, I think I made a mistake. It should be -33 dB, no? I used 10log instead of 20log. So yeah, years.

I suppose they could just pop in a power source 2,000 times more powerful. How many kW would that be? Or is it MW? Not MW, they are currently using 23 watt transmitters, so 45 kW instead, only slightly less than WWVB. Can we launch WWVB into space?


You\'d use a laser of some type, probably. One megawatt laser through 40
meter optics should be at least detectable by similar optics up to
20,000 light-years away:

https://iopscience.iop.org/article/10.3847/1538-4357/aae380

At a thousand AU you\'d need more than 25 watts, but likely not
megawatts. I don\'t think a radioisotope-thermal source would cut it but
small fission reactor might work.

What exactly does it mean to use 40 meter optics on a laser beam? Are you suggesting the optics need to be far enough away from the laser that the inherent limitation of the coherence of the laser beam create a 40 meter wide beam? That would be a pretty big distance. One huge antenna array!

Perhaps I don\'t understand the meaning of 40 meter optics in this context?

I believe it means you use a lens or mirror of that scale to
focus/collimate the beam from your emitter. Like telescope but in reverse.

You aren\'t getting it. Why would you need a 40 meter lens or mirror to collimate a collimated laser beam that is so much tinier? Does the laser produce a beam 40 meters wide?

There wouldn\'t be a single emitting device at those power levels. You\'d
use a phased-array, lenses, mirrors, some combination to build the beam
from array of sources. Raw laser diodes don\'t produce collimated beams
automatically AFAIK


A MW is a bit more than 23 watts. A \"small\" fission reactor indeed. I realize they don\'t need to power it up until it is safely away from people, but the electronics need to operate in this environment. Can that be done in a weight that is practical to leave Earth orbit?


Yeah they\'ve flown fission reactors in space:

https://en.wikipedia.org/wiki/TOPAZ_nuclear_reactor

\"The first TOPAZ reactor operated for 1,300 hours and then was shut down
for detailed examination. It was capable of delivering 5 kW of power for
3–5 years from 12 kg (26 lb) of fuel. Reactor mass was ~ 320 kg (710 lb).\"

But you\'re going to need some more juice than that if you want to power
your ion/plasma drive that\'s going to take your probe out that far in
less than a human lifetime. Might as well power the communication laser
off the drive reactor or whatever power source if you\'re going to put
the propulsion energy source on board too.

It\'s still not clear to me you can communicate faster than some microscopic data rate. Just as laser beams are not perfectly collimated, it gets to be much, much harder to direct any energy beam is such a concentrated form.
 
On 8/23/2020 7:19 PM, Ricketty C wrote:

What exactly does it mean to use 40 meter optics on a laser beam? Are you suggesting the optics need to be far enough away from the laser that the inherent limitation of the coherence of the laser beam create a 40 meter wide beam? That would be a pretty big distance. One huge antenna array!

Perhaps I don\'t understand the meaning of 40 meter optics in this context?

Basically a larger aperture makes the beam spread out less over
distance, not more
 
On Sun, 23 Aug 2020 16:09:43 -0400, bitrex <user@example.net> wrote:

On 8/22/2020 11:34 PM, Ricketty C wrote:
On Saturday, August 22, 2020 at 3:04:21 PM UTC-4, upsid...@downunder.com wrote:
On Sat, 22 Aug 2020 08:41:34 -0700 (PDT), Ricketty C
gnuarm.deletethisbit@gmail.com> wrote:

On Saturday, August 22, 2020 at 4:19:44 AM UTC-4, Martin Brown wrote:
On 22/08/2020 02:10, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:

But the time required to return those images would be...
astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first. The
farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand. I\'m referring to the RF link analysis. They have
a very hard time seeing anything other than stars because other
objects are too dim. I haven\'t done the math, but the data rate
would have to be microscopic to successfully send and receive a radio
signal from such distances. 0.1 light year is 6324 AUs. The Voyager
probes are about 141 AU so about 40 times closer. They now are
transmitting at 160 bps. Doing the math I get about 3 years to
transmit a MB of data.

It is slightly amazing that the Voyagers can be received at all now. The
transmitters on the probes are fixed 1970\'s space approved technology
with limited power and quite crude by modern communications standards.
The error correction was very sophisticated for the time though.

The base station receivers have improved so much since the probes were
launched that they can still follow Voyager out to the heliopause.

Data rates for a future deep space probe should be about the same order
of magnitude as the recent probe to Pluto managed but downgraded by the
increase in distance effects on signal to noise.

Yes, that is the problem. The distance hugely weakens the signals in both directions.

Only -6 dB for each doubling of the distance.

\"Only\" is a four letter word!

And how is the data rate impacted by a -17 dB adjustment to signal strength? You have to consider they are pushing the limit of what they can do working at 160 bps presently. We have done a lot to improve the ground stations, but they can\'t keep increasing their transmit power ad infinitum. As I said, it will take years, maybe decades to transmit a high resolution image from a space craft that far away. While larger antenna in general produce a more collimated beam, there are limits to what you can do given the precision of the antenna shape and the frequency you transmit on.


Cheapest bang-for-the-buck per-unit mission profile I think is keep the
power supply on Earth, a large laser, or array of lasers. Keep the
spacecraft as lightweight as possible. Fire it out into interstellar
space towards 1000 AU fast as it can go, using its instruments/optics to
take in all the data it can on the way, big sail of solar panels feeding
the ion/plasma drive or whatever from the laser beam.

Shining a laser through current largest ground based telescopes you
might be able to get a 10 nanorad beam, unfortunately at 0.1 ly the
beam is more than 10000 km in diameter, so you would need a huge
receiver to extract power.
 
On 8/23/2020 11:49 PM, upsidedown@downunder.com wrote:
On Sun, 23 Aug 2020 16:09:43 -0400, bitrex <user@example.net> wrote:

On 8/22/2020 11:34 PM, Ricketty C wrote:
On Saturday, August 22, 2020 at 3:04:21 PM UTC-4, upsid...@downunder.com wrote:
On Sat, 22 Aug 2020 08:41:34 -0700 (PDT), Ricketty C
gnuarm.deletethisbit@gmail.com> wrote:

On Saturday, August 22, 2020 at 4:19:44 AM UTC-4, Martin Brown wrote:
On 22/08/2020 02:10, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:

But the time required to return those images would be...
astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first. The
farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand. I\'m referring to the RF link analysis. They have
a very hard time seeing anything other than stars because other
objects are too dim. I haven\'t done the math, but the data rate
would have to be microscopic to successfully send and receive a radio
signal from such distances. 0.1 light year is 6324 AUs. The Voyager
probes are about 141 AU so about 40 times closer. They now are
transmitting at 160 bps. Doing the math I get about 3 years to
transmit a MB of data.

It is slightly amazing that the Voyagers can be received at all now. The
transmitters on the probes are fixed 1970\'s space approved technology
with limited power and quite crude by modern communications standards.
The error correction was very sophisticated for the time though.

The base station receivers have improved so much since the probes were
launched that they can still follow Voyager out to the heliopause.

Data rates for a future deep space probe should be about the same order
of magnitude as the recent probe to Pluto managed but downgraded by the
increase in distance effects on signal to noise.

Yes, that is the problem. The distance hugely weakens the signals in both directions.

Only -6 dB for each doubling of the distance.

\"Only\" is a four letter word!

And how is the data rate impacted by a -17 dB adjustment to signal strength? You have to consider they are pushing the limit of what they can do working at 160 bps presently. We have done a lot to improve the ground stations, but they can\'t keep increasing their transmit power ad infinitum. As I said, it will take years, maybe decades to transmit a high resolution image from a space craft that far away. While larger antenna in general produce a more collimated beam, there are limits to what you can do given the precision of the antenna shape and the frequency you transmit on.


Cheapest bang-for-the-buck per-unit mission profile I think is keep the
power supply on Earth, a large laser, or array of lasers. Keep the
spacecraft as lightweight as possible. Fire it out into interstellar
space towards 1000 AU fast as it can go, using its instruments/optics to
take in all the data it can on the way, big sail of solar panels feeding
the ion/plasma drive or whatever from the laser beam.

Shining a laser through current largest ground based telescopes you
might be able to get a 10 nanorad beam, unfortunately at 0.1 ly the
beam is more than 10000 km in diameter, so you would need a huge
receiver to extract power.

My numbers were off anyway, you can be a lot closer than 0.1 LY to
leverage the Sun\'s gravitational lens. 500 AU minimum it looks like.
Voyager 2 is almost at 200 AU, \"only\" took 40 years using just chemical
rockets.

The idea in the white-paper I saw re: propulsion is you use a large
solar array, like a solar sail, tuned to the laser:

<https://www.nasa.gov/directorates/spacetech/niac/2017_Phase_I_Phase_II/Propulsion_Architecture_for_Interstellar_Precursor_Missions/>

\"A 10-km diameter, 100-MW laser array that beams power across the solar
system.

A 70% efficient photovoltaic array tuned to the laser frequency
producing power at 12 kV.

A 70-MW direct-drive, lithium (not xenon)-based ion propulsion system
with a specific impulse of 58,000 s.\"
 
On 8/24/2020 12:22 AM, bitrex wrote:
On 8/23/2020 11:49 PM, upsidedown@downunder.com wrote:
On Sun, 23 Aug 2020 16:09:43 -0400, bitrex <user@example.net> wrote:

On 8/22/2020 11:34 PM, Ricketty C wrote:
On Saturday, August 22, 2020 at 3:04:21 PM UTC-4,
upsid...@downunder.com wrote:
On Sat, 22 Aug 2020 08:41:34 -0700 (PDT), Ricketty C
gnuarm.deletethisbit@gmail.com> wrote:

On Saturday, August 22, 2020 at 4:19:44 AM UTC-4, Martin Brown wrote:
On 22/08/2020 02:10, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:

But the time required to return those images would be...
astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first.
The
farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand.  I\'m referring to the RF link analysis.  They
have
a very hard time seeing anything other than stars because other
objects are too dim.  I haven\'t done the math, but the data rate
would have to be microscopic to successfully send and receive a
radio
signal from such distances.  0.1 light year is 6324 AUs.  The
Voyager
probes are about 141 AU so about 40 times closer.  They now are
transmitting at 160 bps.  Doing the math I get about 3 years to
transmit a MB of data.

It is slightly amazing that the Voyagers can be received at all
now. The
transmitters on the probes are fixed 1970\'s space approved
technology
with limited power and quite crude by modern communications
standards.
The error correction was very sophisticated for the time though.

The base station receivers have improved so much since the probes
were
launched that they can still follow Voyager out to the heliopause.

Data rates for a future deep space probe should be about the same
order
of magnitude as the recent probe to Pluto managed but downgraded
by the
increase in distance effects on signal to noise.

Yes, that is the problem.  The distance hugely weakens the signals
in both directions.

Only -6 dB for each doubling of the distance.

\"Only\" is a four letter word!

And how is the data rate impacted by a -17 dB adjustment to signal
strength?  You have to consider they are pushing the limit of what
they can do working at 160 bps presently.  We have done a lot to
improve the ground stations, but they can\'t keep increasing their
transmit power ad infinitum.  As I said, it will take years, maybe
decades to transmit a high resolution image from a space craft that
far away.  While larger antenna in general produce a more collimated
beam, there are limits to what you can do given the precision of the
antenna shape and the frequency you transmit on.


Cheapest bang-for-the-buck per-unit mission profile I think is keep the
power supply on Earth, a large laser, or array of lasers. Keep the
spacecraft as lightweight as possible. Fire it out into interstellar
space towards 1000 AU fast as it can go, using its instruments/optics to
take in all the data it can on the way, big sail of solar panels feeding
the ion/plasma drive or whatever from the laser beam.

Shining a laser through  current largest ground based  telescopes you
might be able to get a 10 nanorad beam, unfortunately at 0.1 ly the
beam is more than 10000 km in diameter, so you would need a huge
receiver to extract power.


My numbers were off anyway, you can be a lot closer than 0.1 LY to
leverage the Sun\'s gravitational lens. 500 AU minimum it looks like.
Voyager 2 is almost at 200 AU, \"only\" took 40 years using just chemical
rockets.

The idea in the white-paper I saw re: propulsion is you use a large
solar array, like a solar sail, tuned to the laser:

https://www.nasa.gov/directorates/spacetech/niac/2017_Phase_I_Phase_II/Propulsion_Architecture_for_Interstellar_Precursor_Missions/


\"A 10-km diameter, 100-MW laser array that beams power across the solar
system.

Do not fly into beam with remaining aircraft
 
On Sunday, August 23, 2020 at 11:20:01 PM UTC-4, bitrex wrote:
On 8/23/2020 7:19 PM, Ricketty C wrote:

What exactly does it mean to use 40 meter optics on a laser beam? Are you suggesting the optics need to be far enough away from the laser that the inherent limitation of the coherence of the laser beam create a 40 meter wide beam? That would be a pretty big distance. One huge antenna array!

Perhaps I don\'t understand the meaning of 40 meter optics in this context?

Basically a larger aperture makes the beam spread out less over
distance, not more

You really don\'t even understand the question. How are you going to construct a laser with a 40 meter aperture?

--

Rick C.

+-- Get 1,000 miles of free Supercharging
+-- Tesla referral code - https://ts.la/richard11209
 
On 8/24/2020 1:15 AM, Ricketty C wrote:
On Sunday, August 23, 2020 at 11:20:01 PM UTC-4, bitrex wrote:
On 8/23/2020 7:19 PM, Ricketty C wrote:

What exactly does it mean to use 40 meter optics on a laser beam? Are you suggesting the optics need to be far enough away from the laser that the inherent limitation of the coherence of the laser beam create a 40 meter wide beam? That would be a pretty big distance. One huge antenna array!

Perhaps I don\'t understand the meaning of 40 meter optics in this context?

Basically a larger aperture makes the beam spread out less over
distance, not more

You really don\'t even understand the question. How are you going to construct a laser with a 40 meter aperture?

Like this? I guess?

<https://imgur.com/a/6bk21dO>
 
On Sun, 23 Aug 2020 22:15:30 -0700 (PDT), Ricketty C
<gnuarm.deletethisbit@gmail.com> wrote:

On Sunday, August 23, 2020 at 11:20:01 PM UTC-4, bitrex wrote:
On 8/23/2020 7:19 PM, Ricketty C wrote:

What exactly does it mean to use 40 meter optics on a laser beam? Are you suggesting the optics need to be far enough away from the laser that the inherent limitation of the coherence of the laser beam create a 40 meter wide beam? That would be a pretty big distance. One huge antenna array!

Perhaps I don\'t understand the meaning of 40 meter optics in this context?

Basically a larger aperture makes the beam spread out less over
distance, not more

You really don\'t even understand the question. How are you going to construct a laser with a 40 meter aperture?

You simply use a 40 m telescope :).

Big telescopes have now 10 m primary mirrors and up to 30 m mirrors
are studied, so a 40 m mirror is not too far in the future.

The idea is that the signal source (horn antenna, laser etc.) evenly
illuminates the parabolic reflector which then generates a planar
wavefront which has the same diameter as the mirror aperture.

The beam diameter remains constant only in the \"near field\", but in
the \"far field\" it spreads out as wavelength / aperture [radians]. The
transition between near and far field can be quite a distance from the
mirror. A decent microwave antenna handbook will have formulas for
calculating the distance from a parabolic reflector until the beam
starts to spread.

It should be noted that the distance to the Moon is measured by
sending a laser beam trough a 1 m diameter telescope, which is
reflected back from the Apollo era reflectors and collected a few
photons from the reflected light with an other telescope.
 
On 8/24/2020 2:15 AM, upsidedown@downunder.com wrote:
On Sun, 23 Aug 2020 22:15:30 -0700 (PDT), Ricketty C
gnuarm.deletethisbit@gmail.com> wrote:

On Sunday, August 23, 2020 at 11:20:01 PM UTC-4, bitrex wrote:
On 8/23/2020 7:19 PM, Ricketty C wrote:

What exactly does it mean to use 40 meter optics on a laser beam? Are you suggesting the optics need to be far enough away from the laser that the inherent limitation of the coherence of the laser beam create a 40 meter wide beam? That would be a pretty big distance. One huge antenna array!

Perhaps I don\'t understand the meaning of 40 meter optics in this context?

Basically a larger aperture makes the beam spread out less over
distance, not more

You really don\'t even understand the question. How are you going to construct a laser with a 40 meter aperture?

You simply use a 40 m telescope :).

Big telescopes have now 10 m primary mirrors and up to 30 m mirrors
are studied, so a 40 m mirror is not too far in the future.

The idea is that the signal source (horn antenna, laser etc.) evenly
illuminates the parabolic reflector which then generates a planar
wavefront which has the same diameter as the mirror aperture.

The beam diameter remains constant only in the \"near field\", but in
the \"far field\" it spreads out as wavelength / aperture [radians]. The
transition between near and far field can be quite a distance from the
mirror. A decent microwave antenna handbook will have formulas for
calculating the distance from a parabolic reflector until the beam
starts to spread.

It should be noted that the distance to the Moon is measured by
sending a laser beam trough a 1 m diameter telescope, which is
reflected back from the Apollo era reflectors and collected a few
photons from the reflected light with an other telescope.

\"Luke Campbell (who? - ed) uses this rule of thumb:

The smallest possible spot size to which a beam can be focused can be
calculated; if the initial beam width is D, the wavelength of the light
is L, and the distance to the target is R, the smallest spot size (S) is
given by S = 1.2 R L / D.” Notice that if D is very large, the focusing
distance can be very far, especially for short wavelengths.\"

<https://www.centauri-dreams.org/2013/12/30/laser-communications-for-deep-space/>
 
On 2020-08-24, Ricketty C <gnuarm.deletethisbit@gmail.com> wrote:
On Sunday, August 23, 2020 at 7:29:25 PM UTC-4, bitrex wrote:
On 8/23/2020 7:19 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 3:25:11 PM UTC-4, bitrex wrote:
On 8/23/2020 1:15 PM, Ricketty C wrote:
On Sunday, August 23, 2020 at 8:11:26 AM UTC-4, John S wrote:
On 8/21/2020 8:10 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 3:49:41 PM UTC-4, Pimpom wrote:
On 8/21/2020 10:54 PM, Ricketty C wrote:
On Friday, August 21, 2020 at 11:55:30 AM UTC-4, bitrex wrote:
On 8/21/2020 6:38 AM, Phil Allison wrote:

Hi,

Recently it has become normal for astronomers to directly observe planets around nearby stars in an optical telescope.

Couple of months ago, they found two in circular orbit around a very new star.

https://www.businessinsider.com.au/first-ever-photo-shows-2-planets-orbiting-sun-like-star-2020-7?r=US&IR=T

Seems there are in fact billions of the damn things.

Be \"... an awful waste of space \" if Earth is the only one with life forms.

Above quote from the SF movie \"Contact\".



..... Phil



I\'m probably remembering the exact figures incorrectly but if you could
push a space telescope out to about a tenth of a light-year from Earth,
it could leverage gravitational lensing to make an equivalent lens of
enormous size.

It could then search for evidence of life in a large volume of space by
imaging planetary surfaces around other star systems directly, it could
resolve stuff like oceans, plants, or structures.

But the time required to return those images would be... astronomical.

Sending back digital images over a distance of a tenth of a light
year by radio wave would take, well, just one-tenth of a year, or
about five weeks. No problem.

The big problem is to reach that 0.1 light year distance first.
The farthest man-made objects are now travelling at ~15 km/s
(Wikipedia). At that speed, it would take over 2000 years. :-(

You misunderstand. I\'m referring to the RF link analysis. They have a very hard time seeing anything other than stars because other objects are too dim. I haven\'t done the math, but the data rate would have to be microscopic to successfully send and receive a radio signal from such distances. 0.1 light year is 6324 AUs. The Voyager probes are about 141 AU so about 40 times closer. They now are transmitting at 160 bps. Doing the math I get about 3 years to transmit a MB of data.

? 10Mb/160bps = 62.5k seconds = 17.4 hours. What am I doing wrong?

Not as bad as I thought, but I suppose they would highly value any image compression, but lossless of course. With the image mostly the star, I suppose they could do a fair bit of compression. Still, they would want to transmit and awful lot of MB, so it will take lots of time, still years.

Imagine what it would take to manage the cameras and other devices. Over a month just to send any message no matter how short.


160 bps is what they have now, not from 0.1 light years away. Apply the -17 dB factor and recalculate... I think the distance ratio is actually 45. Opps, I think I made a mistake. It should be -33 dB, no? I used 10log instead of 20log. So yeah, years.

I suppose they could just pop in a power source 2,000 times more powerful. How many kW would that be? Or is it MW? Not MW, they are currently using 23 watt transmitters, so 45 kW instead, only slightly less than WWVB. Can we launch WWVB into space?


You\'d use a laser of some type, probably. One megawatt laser through 40
meter optics should be at least detectable by similar optics up to
20,000 light-years away:

https://iopscience.iop.org/article/10.3847/1538-4357/aae380

At a thousand AU you\'d need more than 25 watts, but likely not
megawatts. I don\'t think a radioisotope-thermal source would cut it but
small fission reactor might work.

What exactly does it mean to use 40 meter optics on a laser beam? Are you suggesting the optics need to be far enough away from the laser that the inherent limitation of the coherence of the laser beam create a 40 meter wide beam? That would be a pretty big distance. One huge antenna array!

Perhaps I don\'t understand the meaning of 40 meter optics in this context?

I believe it means you use a lens or mirror of that scale to
focus/collimate the beam from your emitter. Like telescope but in reverse.

You aren\'t getting it. Why would you need a 40 meter lens or mirror to collimate a collimated laser beam that is so much tinier? Does the laser produce a beam 40 meters wide?

etendue

--
Jasen.
 
On 2020-08-24, Ricketty C <gnuarm.deletethisbit@gmail.com> wrote:
On Sunday, August 23, 2020 at 7:29:25 PM UTC-4, bitrex wrote:

I believe it means you use a lens or mirror of that scale to
focus/collimate the beam from your emitter. Like telescope but in reverse.

You aren\'t getting it. Why would you need a 40 meter lens or mirror to collimate a collimated laser beam that is so much tinier? Does the laser produce a beam 40 meters wide?

etendue

this is basically basically entropy for light beams.
you can make them straigter but in the process you make them wider.

--
Jasen.
 
On 24/08/2020 00:19, Ricketty C wrote:
On Sunday, August 23, 2020 at 3:25:11 PM UTC-4, bitrex wrote:

You\'d use a laser of some type, probably. One megawatt laser
through 40 meter optics should be at least detectable by similar
optics up to 20,000 light-years away:

https://iopscience.iop.org/article/10.3847/1538-4357/aae380

At a thousand AU you\'d need more than 25 watts, but likely not
megawatts. I don\'t think a radioisotope-thermal source would cut it
but small fission reactor might work.

What exactly does it mean to use 40 meter optics on a laser beam?
Are you suggesting the optics need to be far enough away from the
laser that the inherent limitation of the coherence of the laser beam
create a 40 meter wide beam? That would be a pretty big distance.
One huge antenna array!

It is fairly routine at least up to 1m class optics used for Lidar
atmospheric surveys and lunar ranging. You pass the nominally parallel
laser through a diverging lens at the focus of the main mirror.

It makes the beam power density low enough that isn\'t dangerous to
anything nearby that gets illuminated by accident. The raw beam from the
high power laser is seriously nasty. ISTR on lunar retro reflector
ranging they typically only get a handful of photons back.

Perhaps I don\'t understand the meaning of 40 meter optics in this
context?

Dirty big mirror.

Arecibo can do this sort of trick with pulse or chirp radar to get
details TDR images of passing asteroids with impressive detail.

The trick is to exploit the largest possible ground based kit with the
most sensitive receivers and signal processing and keep the remote end
low power, lightweight and small.

A MW is a bit more than 23 watts. A \"small\" fission reactor indeed.
I realize they don\'t need to power it up until it is safely away from
people, but the electronics need to operate in this environment. Can
that be done in a weight that is practical to leave Earth orbit?

Possibly but it would have the greens up in arms.

--
Regards,
Martin Brown
 
On 2020-08-24 04:55, Jasen Betts wrote:
On 2020-08-24, Ricketty C <gnuarm.deletethisbit@gmail.com> wrote:
On Sunday, August 23, 2020 at 7:29:25 PM UTC-4, bitrex wrote:

I believe it means you use a lens or mirror of that scale to
focus/collimate the beam from your emitter. Like telescope but in reverse.

You aren\'t getting it. Why would you need a 40 meter lens or mirror to collimate a collimated laser beam that is so much tinier? Does the laser produce a beam 40 meters wide?

etendue

this is basically basically entropy for light beams.
you can make them straigter but in the process you make them wider.

It\'s just diffraction--the 1:1 tradeoff between beam diameter and
diffraction angular spread. Distance and angle are conjugate variables
in a Fourier integral, like time and frequency. Specifically, sin theta
is conjugate to xNA/lambda.

Etendue is something else, namely the product of area times projected
solid angle. A single diffraction-limited beam of whatever diameter has
an etendue of lambda**2/2, so etendue is proportional to the number of
optical modes that can contribute.

Cheers

Phil Hobbs

--
Dr Philip C D Hobbs
Principal Consultant
ElectroOptical Innovations LLC / Hobbs ElectroOptics
Optics, Electro-optics, Photonics, Analog Electronics
Briarcliff Manor NY 10510

http://electrooptical.net
http://hobbs-eo.com
 
On 24/08/2020 00:17, bitrex wrote:
At infrared or optical wavelengths it\'s hard to keep the light coherent
between members of the array separated by large distances, aperture
synthesis is a lot easier with radio astronomy I think

Although aperture synthesis is much easier with radio waves it has been
done in the optical and near infra red with remarkable results.

Prototype was COAST at MRAO (aka the telescope that sings).

http://adsabs.harvard.edu/full/1992ESOC...39..921B

Optical beamsplitters and path compensation is a nightmare though.

Limitation is that it only really works on bright stars that get fairly
high in the sky.

Full scale implementation at Mount Wilson and else where using radio
astronomy techniques in the near infrared.

https://www.researchgate.net/publication/231152988_First_results_from_the_CHARA_Array_II_A_description_of_the_instrument

--
Regards,
Martin Brown
 
On 8/24/2020 6:40 AM, Martin Brown wrote:
On 24/08/2020 00:19, Ricketty C wrote:
On Sunday, August 23, 2020 at 3:25:11 PM UTC-4, bitrex wrote:

You\'d use a laser of some type, probably. One megawatt laser
through 40 meter optics should be at least detectable by similar
optics up to 20,000 light-years away:

https://iopscience.iop.org/article/10.3847/1538-4357/aae380

At a thousand AU you\'d need more than 25 watts, but likely not
megawatts. I don\'t think a radioisotope-thermal source would cut it
but small fission reactor might work.

What exactly does it mean to use 40 meter optics on a laser beam?
Are you suggesting the optics need to be far enough away from the
laser that the inherent limitation of the coherence of the laser beam
create a 40 meter wide beam?  That would be a pretty big distance.
One huge antenna array!

It is fairly routine at least up to 1m class optics used for Lidar
atmospheric surveys and lunar ranging. You pass the nominally parallel
laser through a diverging lens at the focus of the main mirror.

It makes the beam power density low enough that isn\'t dangerous to
anything nearby that gets illuminated by accident. The raw beam from the
high power laser is seriously nasty. ISTR on lunar retro reflector
ranging they typically only get a handful of photons back.

Perhaps I don\'t understand the meaning of 40 meter optics in this
context?

Dirty big mirror.

Arecibo can do this sort of trick with pulse or chirp radar to get
details TDR images of passing asteroids with impressive detail.

The trick is to exploit the largest possible ground based kit with the
most sensitive receivers and signal processing and keep the remote end
low power, lightweight and small.

A MW is a bit more than 23 watts.  A \"small\" fission reactor indeed.
I realize they don\'t need to power it up until it is safely away from
people, but the electronics need to operate in this environment.  Can
that be done in a weight that is practical to leave Earth orbit?

Possibly but it would have the greens up in arms.

The sheeple do tend to have a better intuitive grasp of the nuclear
industry\'s actual safety and reliability capabilities than the nuclear
industry\'s management, on average.

Same goes for a number of industries. Show the average man-on-the-street
a Space Shuttle launch then tell him the reliability figures NASA
management were spewing for the system at the time and he\'d say \"That\'s
nuts\" and he\'d be dead right.
 

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