Well, I'm going to do a case study. Let's take Belgium(because I happen to live there) as an example.
...uhh, ok. What exactly is the problem? What you're doing is working, and you have a population density over TEN TIMES that of the US, and in 2010, Belgium was ranked as having in the top 10 best quality of life in the world.
If you want to keep using nuclear power, go right ahead. Radioactive materials aren't in particularly short supply. What's stopping Belgium from simply continuing to do what it's doing already?
Or were you just complaining about money?
Our nuclear reactors are falling apart(often quite litteraly), and most political parties want to stop using it all toghether. This will most likely lead to a massive increase in the use of fossil fuels, as happened in Germany. But the problem mostly lies with money shortages, as it does in quite a lot of countries.
Transmission frequencies aren't remotely a problem for microwave power transmission. We are talking about frequencies that AFAIK aren't even used for communication outside a few black ops military applications (maybe) and the benefits far, far outweigh what we are using them for now (if anything).
And the degradation is more then outweighed by the increase in efficiency from the space location. The increase in efficiency is as follows:
-x3 from constantly being at max output compared to earth applications which get 1/3rd max output over the day
-x1.5 from no weather conservatively
-x1.4 from no atmospheric interference even on a clear day
-x1.2 from reductions in the excess capacity needed as a safety factor
-x1.4 from reductions in power transmission losses
So that means that even after losing 17% of your capacity in the first 7 year you still are running 878% efficiency compared to earth. Btw, a 17% reduction in 7 years does not mean a reduction in lifetime by 10%, solar panels do not take 70 years to have a 17% reduction in output.
Add onto this the fact that you can send this power to anywhere on the surface of the earth that it's needed. So you can either chose to go the extravagant route and put that towards excess capacity so no one ever has a blackout ever again or you can bank the efficiencies and bump your economic efficiency up by another x1.5 or x2.0.
If you think that cluttering is a problem then you really, really, really, really, really have no sense of perspective about how big space is.
There's a serious garbage problem in space. One small impact might render your entire system useless.
Btw, you seem to understate several issues. Depending on the frequencies, the signal might be blocked by rain/clouds(Statements from the wiki), and you are certainly going to lose some power due to transmission inefficiencies, as well as needing enormous transmitters/recievers.
Complication with different frequencies will also be a problem. I'm going to do the math on cost some time later today, but I doubt it'll be viable.
Also it's not a lifetime reduction by 10% , but to 10%. (As in, from 30 to 3 years lifetime.)
Radioactive materials aren't in particularly short supply.
Peak Uranium will happen before 2100.
It isn't actually that common on Earth at all.
Thorium, MOX, and other new reactor types. The main problem with nuclear power is a huge PR issue, and the fact that most existing reactors are way to old.
Anyway, the calculations.
Power beaming from geostationary orbit by microwaves carries the difficulty that the required 'optical aperture' sizes are very large. For example, the 1978 NASA SPS study required a 1-km diameter transmitting antenna, and a 10 km diameter receiving rectenna, for a microwave beam at 2.45 GHz. These sizes can be somewhat decreased by using shorter wavelengths, although they have increased atmospheric absorption and even potential beam blockage by rain or water droplets. Because of the thinned array curse, it is not possible to make a narrower beam by combining the beams of several smaller satellites. The large size of the transmitting and receiving antennas means that the minimum practical power level for an SPS will necessarily be high; small SPS systems will be possible, but uneconomic.
To give an idea of the scale of the problem, assuming a solar panel mass of 20 kg per kilowatt (without considering the mass of the supporting structure, antenna, or any significant mass reduction of any focusing mirrors) a 4 GW power station would weigh about 80,000 metric tons, all of which would, in current circumstances, be launched from the Earth
Now, the wiki article plans to go to LEO first, and then use ion engines to get into GEO. Sadly there doesn't seem to be much progress on those, so we're forced to go the GEO in one trip.
The most likely candidate for the trip seems to be the
Delta IV-H, being the largest launch vessel in commision. This thing can carry 6,275 kg in one trip, for a cost 300 million dollars.
80 000/ 6.275 tonnes= 12749 flights
Now the amount of flights that this results in makes me pray I made a mistake, though I doubt it.
Now assuming we can use lightweight solar pannels
Very lightweight designs could likely achieve 1 kg/kW,[47] meaning 4,000 metric tons for the solar panels for the same 4 GW capacity station
This still means 638 flights at least, and that's just for the pannels, not counting the antennae or something.
Fake edit: Apparently the wiki comparison is incomplete, and the Ariana V can take a slightly larger payload into space. The Falcon Heavy (indevelopment) might also help, but both have a cargo capacity lower then 10.000 kg.
Note: One should take care not to confuse GTO (Geostationary transfer orbit), with GEO (Geostationary orbit.) There's a serious difference.