@Disposal of space junk
The ISS orbits at about 7km/second tightly round the Earth. Escape velocity at that altitude is around 11km/second.
So escaping Earth's orbit from ISS requires about 4km/second of velocity change. Now for some super simple math:
exhaust velocity * ln ( loadedWeight / emptyWeight ) = our capacity for velocity change i.e. delta-v
Let's assume a simple, bog standard, hypergolic hydrazine+nitro rocket cause it's cheap and simple. The exhaust velocity is about 2 km / second.
To reach escape velocity you would need about 7 times the fridge & rocket's weight in fuel.
Tank and all we're talking about a rocket far bigger than the fridge itself!
If you double that fuel you can get around 5.5km/second of capacity for velocity change, which is enough to leave earth orbit, into a solar orbit, then perform a second burn a half year later to change your orbit so it doesn't cross paths with Earth. Probably.
But you didn't want in space for a super long time, you want the Sun!
Earth orbits the Sun at about 29km/second. To de-orbit the sun you need to pretty much get rid of all of this speed. That's a velocity change of almost 29km/second. Maybe slightly less.
Those epic, giant launch vehicles? They can put out around 10km/second of delta-v.
There's absolutely no way a hypergolic rocket is sending you into the Sun. Even an efficient, cryogenic fuelled (lox-hydrogen) rocket won't do it for you.
To manage 29km/second you'll need a super efficient ion propulsion.
This basically amounts to installing a (probably expensive) engine, all the equipment for a satellite, and set of solar panels onto the fridge and programming it to set sail for fiery doom.
OR you could just fling it onto the Earth.