It seems to me any need to deliver solar energy around the clock using space installations would be much cheaper to meet if the principle is to simply to use large thin film reflectors in orbit to reflect sunlight down to pre-existing ground based solar farms in remote areas, then to build orbital PV facilities that would generate power in situ and then transmit it down to earth and requiring additional ground based receiving antenna of the required scale.
A square kilometer of .4 mil commercially available aluminized mirror finish film weigh about 8 tons. Even if we assume we can do no better, and the supporting and positioning structure required to maintain mirror shape, counter solar photo pressure and maintain position and orientation would weight 5 times as much, a single LM9 launch can still lift 3 square km of such reflectors.
current solar PV technology allows about 40 MW of solar peak output per sq km.
So a 3 sq km reflector in space could roughly double the output of about 120MW of ground based solar generating capacity.
Current cost of solar PV is roughly $2 per Watt of capacity, installed.
So if LM9 class rocket can launch 120 tons into space for $240 million or less, or any rocket for launch at $2 million per ton, then mylar mirror in space might be a economically viable solution to allow solar farms to generate cover night using just existing solar PV technology without any need to beam microwave from space.
I think the primary draw of space based solar is that weather/day night cycle will be less of a factor. The greatest hurdle for solar energy today is that energy generation is not stable, which causes problems when integrating with the grid.