Polymer solar cells look interesting, though they still have a way to go. Semiconducting polymers seem like they could also be useful as electrodes in electrolytic cells and fuel cells. If they could replace platinum, or at least drastically reduce the amount of platinum necessary, then that would be a big step forward for both technologies. I've found various articles about research into polymer electrodes for both technologies.
Superconductivity? There's a certain problem. Superconductivity requires supercold temperatures. Like liquid-helium temperatures for most practical applications of it. Helium boils at about 4 K -- that's 4 Centigrade degrees above absolute zero. 0 C, the melting point of water, is about 273.15 K. That's why superconductivity has mostly been used to make superstrong magnetic fields. One needs a liquid-helium refrigerator to make the effect happen, and it's easiest to afford one when it's for a big magnet.
Outer space? From the numbers I'd cited earlier, the cost to send a common solar panel into orbit is about 400 times its retail price, and that assumes a rocket that's fully loaded with that kind of panel.
I checked on that great fount of knowledge, Wikipedia, and I found several articles:
Launch service provider,
Comparison of orbital launch systems,
List of orbital launch systems,
List of private spaceflight companies,
List of government space agencies There are now several companies offering launch services, companies based in the US, Europe, Russia, China, and India.
The downside for rocket development comes from the nature of the beast: orbit-capable rockets are expensive and complicated, there aren't many individual ones used, they have to work right the first time, and that time is the only one that nearly all of them get used. Part of the expense comes from using liquid propellants, and often cryogenic ones, something that is a necessity for getting high exhaust velocities. One can get as much as 3 km/s from a solid rocket, but about 3.5 km/s for kerosene and liquid oxygen, and 4.6 km/s for liquid hydrogen and liquid oxygen (
Solid-fuel rocket - Wikipedia).
So it's not surprising that rocket design has tended to be rather conservative. The Russians have been using variants of the Soyuz design for about 50 years now. The ULA's Delta II rockets have been in use for some 26 years. Even SpaceX has been somewhat conservative, using its Merlin rocket engine in all its rockets. Its first one, Falcon 1, used 1 of them, and its current one, Falcon 9, uses 10 of them, 9 in its first stage and 1 in its second stage. Its upcoming Falcon Heavy rocket will be essentially a Falcon 9 with two strap-on boosters that are essentially two Falcon 9 first stages, thus giving a grand total of 28 Merlin engines.
So I don't see much prospect of lowering launch costs by a factor of 400 or so, what would be necessary to make orbiting solar power stations economically feasible.