I’m wondering: would a probe launched today instead employ a laser to communicate? This would seem to offer many orders of magnitude improvement in the directionality of the signal.
I’m wondering: would a probe launched today instead employ a laser to communicate? This would seem to offer many orders of magnitude improvement in the directionality of the signal.
However, due to the shape of the black body radiation curve, the sun gives out relatively less microwave radiation than it does visible light, which might outweigh the advantages of more directionality given by using a laser.
https://descanso.jpl.nasa.gov/monograph/series10/03_Reid_cha...
https://www.rfcafe.com/references/popular-electronics/amazin...
Not having thought this through before, I see now that while a transmit maser may have efficiency advantages, it may not improve directionality relative to a standard parabolic radio transmitter. All methods of producing microwaves will have basically the same diffraction-limited gain for a given “aperture” (dish) size. That darn uncertainty principle! (However, an optical laser would still give way better directionality.)
We want to download high resolution images/spectrographs whereas we only want to upload code/instructions.
https://www.jpl.nasa.gov/news/nasas-deep-space-optical-comm-...
https://en.m.wikipedia.org/wiki/Laser_Interferometer_Space_A...
Probably infeasible for several reasons (only useful when accelerating DIRECTLY away from Earth, incoming light to power spaceship is probably coming from the sun and therefore likely also in the directly of Earth, so net zero acceleration at best from firing the photons back towards the sun), but it'd be pretty neat.
My intuition would have been that you are better off using a fairly standard transceiver and spending your engineering budget either increasing power or getting a bigger dish (either by launching on a wider rocket or with a folding design).
Lasers might interesting for the downlink, but receiving a laser signal on the probe sounds difficult (earth is pretty bright).
We envision deployment in three sites at or near the longitudes of the existing DSN sites.
As an example, a potential initial phase could deploy 40 12-m elements at each complex to duplicate the X-band performance of a DSN 70-m antenna.
Second and third phase deployments may bring the number of 12-m antennas to 200, then perhaps 400 per complex.