"silly idea" it may be but now i want a mega-maser as described for my own sporting purposes.
"silly idea" it may be but now i want a mega-maser as described for my own sporting purposes.
Anyways, the TL;DR is all those cables weigh a lot, so launching them in to space isn’t cheap.
What you're seeing with phones isn't microwave, but inductance, very different technology with very different benefits/drawbacks.
Yes, but they are because their power source is unbelievably large and free. If you look at their efficiency from the perspective of what the sun puts out, they're laughable.
Problem is, with the moon beams we don't have infinite and free source power to waste on inefficiency.
> And if you focus the beam instead of just using a glowing ball of hydrogen, go with a more efficient wavelength and remove all the atmospheric losses, it actually becomes quite efficient.
Focusing the beam is not that easy, you need to hit a moving spot of minimal size with an extremely powerful laser. Avoiding all atmospheric losses is probably not going to work, either. Lastly, you need to get those transmitters built on earth, which, as the OP points out, quite land intensive.
It is a theoretical option, but I would not call it efficient.
Power sources on earth are also plentiful and almost free, compared to building stuff on the moon (at least until we have a lot more infrastructure up there)
With the current capital cost of ~$50/W to beam power, its reasonable to think about for small endeavors, but for a base designed for 100k people making power lines onsite is better, as you will need that manufacturing capacity for other things anyway.
If you also switch to laser power beaming, they can illuminate the existing solar farm so a separate receiver is not needed.
That sounds weird. As per Wikipedia, Sun's apparent magnitude is around -26.7, full Moon's is -12.7, so the Sun is 400000 times brighter than the Moon under the best circumstances. Earth being larger can't correct this by three orders of magnitude.
Find a large symmetrical crater pointing directly at Earth. Silver its surface with very cheap to transport BoPET (Mylar). Once installed, there's no need to worry about the sheets flying off or dust blowing over since there is no wind. Place a solar / thermal collector at the crater's focal point. Reap power from earth-light.
If you choose a large crater, an MVP system can go live with just a small collector and small portion of the crater silvered. It can subsequently scale as your growing operations demand more power.
It can do double-duty in broadcast communications too.
You could use the same kit to radiate away some of that intense daytime heat too. Spread it across all of Earth.
Now as to solar PV, in principle it might be doable I guess. But I am not able to make the necessary calculations. How large would the crater need to be for 10MW say?
Even as a heat engine, you might get useful power out. If you could achieve say 150 - 200 celsius difference between your concentrator and night time temperature of the surrounding rocks. Which rocks serve as both the engine's heat-sink and a relatively comfy foundation for your habitat.
I'm pretty sure you are off by several orders of magnitude here as all sources I find list the sun as ~400,000 times brighter than the moon.
Or, better: In the same way every "daytime headlight" you see is outdoing the sun.
I doubt they'd want a very large band but in microwave work I dunno what counts as "large".
and i'm a little afraid to go look deeper into this because i'll wind up tearing up junkyard microwave ovens and building something i shouldn't.
But thats the thing: now i want to do a mad max maser on a truck with maybe dozens of magnetrons if i could tow a generator...
It fits with my "Orbital Slingshot" project so well, too.
It's a totally silly idea to built a big ass slingshot that throws things as high as possible. I figure calling it an "Orbital Slingshot" makes it at least as viable and investment worthy as some of the other efforts [1] and [2] forex.
If I can get my daughter to do some artwork I might fire up a web page for it finally.
[1] https://www.space.com/23015-slingatron-reusable-launch-syste...
[2] https://www.nextbigfuture.com/2018/02/spinlaunch-is-using-la...
basics:
solar constant: 1.36 kW / m^2
earth-to-moon range: 400 km
parameters from the article: frequency: 5 GHz -> wavelength: 6cm
earth antenna array linear dimension: 200 km
transmit power density: 100 W/m^2
Let's assume that the earth antenna array elements are 50m wide, and spaced out such that they cover 1% of the total 200km * 50m area, for a total antenna aperture of 1e5 square meters (10% of the SKA).
Combining the stated transmit power density of 100 W/m^2 with the antenna area, we get a total transmit power of 10 MW.Throw it at Friis:
power density at moon = transmit power * earth antenna area / (range^2 * wavelength^2)
= 10e6 watts * 1e5 m^2 / ( 400e3^2 m^2 * 0.06^2 m^2)
= 1.73 kW / m^2
Atmospheric attenuation at 5 GHz is pretty minimal. If we conservatively assume 20% loss, I think we still end up with a higher power density at a single frequency than from the sun across the entire spectrum.I don't think anything like this will ever be built, but I don't see why it is impossible. Where's the mistake?
Three zeros seem to be missing.