Lots of hidden trades here. Many rocket nozzles have huge numbers of cooling passages in the bell. Both preheats the fuel for better performance and cools the nozzle to allow more heat flux from the rocket flame. This much simpler nozzle from SpaceX has forgone this route for something else. Maybe arranging excess oxidizer or fuel to flow along the inside of the nozzle for cooling. Or a thicker (heavier) nozzle wall to provide strength at higher temperature. Or something else altogether.
The Merlin 1D (as you can see below) is both regeneratively (top part) and a radiatively cooled super-thin nozzle extension--hence, the refractory materials (niobium alloy in this case). When you watch a launch, you'll see that skirt glowing pretty brightly. I had no idea how they'd go about making them, though. I suppose they'll still have to make nozzles/skirts like this, even though the SuperDraco and Raptor engines will have the chamber parts 3d printed?
On that note, thanks for that "spinning" video John Coloccia. Beefy tool post on that rig.

