Enough to run an electrostatic propulsion system? Probably not.
You see, the generator is so massive in terms of kilograms per kilowatt generated, that by the time you scaled it up to the point it could feed an ion drive, the rocket's total mass would be such that the acceleration would be a microscopic fraction of a gravity. It would take several years to travel between Terra and Luna.
NASA looked into those things back in the days before nuclear energy. They used mercury instead of water, for efficiency. Such systems are generally useful for power needs between 20 kW and 100 kW. Below 20 kW a solar cell panel is better. Above 100 kW a nuclear fission reactor is better.
They typically have an alpha of 250 to 170, a collector size of 130 to 150 watts per square meter, and a radiator size of 140 to 200 watts per square meter.
(where "alpha" is how many kilograms of generator you need to produce one kilowatt)
By the way, you forget to include the heat radiator.
There is a design for an emergency maneuver drive called a "solar moth"
http://www.projectrho.com/public_html/rocket/enginelist.php#id--Beamed_Power--Solar_Moth
It is basically a half-silvered balloon used as a mirror to heat up propellant that is expelled from an exhaust nozzle.
The advantage is that it is so cheap and low mass that any ship can afford to have one as an emergency back-up.
The disadvantage is a single Solar Moth engine has a pathetic thrust of 4,000 Newtons. This means if the ship has a mass of 100 tons (not dtons), a Solar Moth engine could give it an acceleration of 0.04 meters per second, or about 0.004 g. Which is still better than the steam engine feeding an ion drive.