If your numbers are correct, and I did the math correctly in my head, that's about five thousand pounds of thrust. A nuclear submarine might weigh ten thousand times that. Obviously a nuclear sub operates at much lower power level and obviously the hull doesn't have to be as thick for a spacecraft so I think it not a ridiculous comparison. Also you're spacecraft need not carry dozens of ICBMs, torpedoes, hundreds of sailors, etc.
Obviously the first engine ever exhaustively tested is usually not the highest performance achievable. A factor of a thousand seems possible although a hundred is more likely.
So for a very large nuclear plant, if the EM drive were weightless (LOL) then maybe 1/10th G applied to that nuclear sub is some kind of theoretical limit not entirely ridiculous but possible.
Now consider that to one sig fig a G of acceleration for a year is the speed of light. And if you're careful maybe you could run the plant for three decades.
So a round trip to the speed of light and back again is more or less back of the envelope possible to visit some distant star.
Relativity rears its ugly head and ten years of ship time around the speed of light is a lot further than 10 lightyears and time passing on earth is a lot longer than ten years.
Of course at the speed of light you're going to need a rather substantial hull, an active radar that can avoid interstellar crud, etc. If you can detect "stuff" at a day out, at a tenth of a G accelerating for an entire day you can be quite far away indeed by the time you pass it.
I can't run the numbers in my head like above, but even 1/100th G slices a very substantial amount of time off a Mars mission. Some unverified google results imply 1/100th G means Mars in a month not a year and a half.
At least as a back of the envelope calculation its quite a useful vehicle.