On Fri, 08 Sep 2023 06:18:35 GMT, Jan Panteltje <alien@comet.invalid>
wrote:
On a sunny day (Fri, 08 Sep 2023 00:06:59 +0200) it happened jeroen
<jeroen@nospam.please> wrote in <uddhi4$34vlh$1@dont-email.me>:
I've been trying to find something about the link budget. I had
one for the Voyager or Pioneer probes somewhere, but I can't seem
to find it again. IIRC, factors going into it were transmitter power,
antenna gains, path loss, receiver S/N and bandwidth. It shouldn't
be much different for IR EM waves, although receiver S/N would here
be limited by shot noise rather than Johnson (thermal) noise.
The 'antennas' here are telescopes, of course.
Maybe I am seeing his wrong,
but for a receive antenna to collect as much signal as possible,
a focussing dish surface catches a lot more light than a telescope aperture.
Aim a laser pointer at the wall. Then try the equivalent with RF.
So for the spacecraft some sort of dish (like James Webb has) or like used for RF (Voyagers have a dish) should
work better than a 'telescope' (with lenses).
For transmission a lens system is cool, although lasers already have a narrow beam by default?
Searching finds this:
https://www.jpl.nasa.gov/news/nasas-deep-space-communications-to-get-a-laser-boost#carousel-27fdb231-a68f-434e-ad7e-5e92f104b2f1-1
you can enlarge the photo inset, shows a small mirror.
I sure hope they get enough signal.
Very small compared to the radio dish.
Now one could argue about the IR wavelength being much shorter
so for waves per square surface area more for IR..
But with such a small mirror back in a long tube, pointing becomes critical. >> ?
Seems sort of 'tucked on'?
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