The moon's mean orbital speed is just over 1 km/s. You need to get rid of most of that to have the moon collide with the Earth. Not all of it, but most of it.
With technology that we have today, and with anything we could reasonably expect to get, changing the orbit of the moon would require some sort of reaction mass. There is, of course, very probably lots of interesting physics we are unaware of. But we are unaware of it. So we need to use reaction mass.
This question claims that electric propulsion could achieve 20 km/s for the nozzle velocity of a rocket. So, if you could construct an electric propulsion rocket that achieved this, you would need to throw away about one 20th of the mass of the moon to slow the rest by 1 km/s. The moon's escape velocity is about 2.68 km/s, and the solar system after that is about 16.6 km/s, so the stuff being ejected goes out of the solar system.
So you would need to construct a huge-honking electric propulsion rocket and fire one 20th of the mass of the moon "forward" so as to slow it's orbit. The exhaust would escape the solar system, so not be a concern. (Unless it happened to hit another planet.) You might need to adjust things to keep the jet aimed correctly and prevent the moon rotating out from under you. The time this takes depends on how big you make the rocket. If it was exceptionally large such that it produced one millionth of one g, then it would take 3.17 years. This would require $3.67 \times 10^{13}$ kg/s in the exhaust. And would require an energy input of $7.34 \times 10^{19}$ Watts, assuming 100% efficiency. That is about 2.5 million times the electrical power of the entire Earth.
Now it is probably possible to do some "jim-jam" with orbits and get a collision with less change of velocity. But your question specified a "spiral." So the analysis here is in the ballpark.