NASA has floated ideas to do sample return from Mars on a budget. One involves firing a very compact solid fueled multi-stage rocket, weighing only 25 kilograms or so, off from the surface of Mars with just a few grams of Martian dirt in a capsule. The capsule will then be captured in Martian orbit by an orbiting earth return stage, brought back to earth, inserted into small atmospheric reentry titanium sphere weighing only a few kilograms, and sent in for a landing.
Since the moon's surface gravity is only 1/3 that of Mars, this whole idea ought to be quite practical for lunar return as well, and doable for even less weight.
It was said the Chang'e 3 lander had a potential payload capacity of over 1000 Kgs, and only 120kg is used for the rover. There appears to be plenty of extra payload capacity for a small solid fueled ascent stage weiging some dozens of kilograms to hitch a ride, along with a Yutu 2 rover to look for interest dust to bring back. The Chang'e 2 bus had already demonstrated the capacity to escape from the moon again, so an modified Chang'e bus can be used to capture the moon dust capsule in lunar orbit, escape from the lunar gravity well and reenter earth's sphere of influence, zip by earth, and drop off a small reentry module housing the moon dust capsule.
The greatest challenge seem to be the lunar orbit rendevous needed for the lunar return craft to pick up the lunar dust capsule. Unmanned orbital rendevous so far from earth has, AFAIK, never been actually attempted.