Let's make a rough estimate: Concentrator solar cells and solar thermal towers can cool away ~1000 times the solar irradiation, or about 1 MW/m
2. Fission reactors have a bit more, for fusion people look at 10-25 MW/m
2 (
example 1,
example 2).
Let's be super optimistic and combine 50 MW/m
2 with LIGO-quality mirrors (1 photon out of 3.3 million is absorbed). They don't work at temperatures where you can cool this heat flow but this gives a conservative upper limit. That means we can provide 3.3 million times 50 MW per square meter, or 165 TW/m
2. To get the corresponding pressure divide it by the speed of light and multiply by 2 (arriving+leaving light). The result? 1.1 MPa, about 11 times the atmospheric pressure. That is in principle sufficient to launch a rocket.
Caveats: 165 TW (a single square meter in the calculation above) exceeds the global power consumption by a factor 10 and the electricity production by a factor 100. That is not really feasible. If you can dedicate a full large power plant block (1 GW) to the rocket launch and assume a super optimistic 50% laser efficiency, the force you get is only 1 GW/c = 3.4 N, not even sufficient to launch half a kg. With 10 power plant blocks you can launch two kilograms, still not reasonable as the mirror and other infrastructure will probably have a larger mass already.
What about storing the energy in advance?
Accelerating a payload of mass m to 8 km/s (roughly orbital speed, ignoring drag and gravity losses) at constant acceleration needs a force of mx over 8 km/s / x time. A force of mx needs mxc/2 laser power, or mxc electricity. Multiplied by the time we get an energy demand of 8 km/s * c = 2.4 TJ/kg. This energy doesn't depend on the acceleration profile, I just chose the easiest one here.
Superconducting coils are probably the cheapest technology that can store several TJ and deliver them back within minutes. A typical investment cost is about $100/kWh, so we need $100 millions per kg of lauch mass. A very small spacecraft of 100 kg would need $10 billion investment just for the energy storage. A one tonne payload would need $100 billions.
You could make a cavity with a stationary mirror and the rocket as other side. If we handwave away all focusing issues, that approach recycles the power efficiently, but unfortunately the moving rocket will shift the light frequency - and that means your mirrors get a much worse efficiency. Oh, and the focusing won't work.