ToughSF posted a few avenues of research, early last weekend. Both definitively drawing-board. I'd have said something but I couldn't click the link to one of the actual papers then, so - you get my take on them, today.
One is laser-hits on a liquid propellant. It splashes. As far as ToughSF knows, nobody's solved this one. Then he went on to note how lasers sploot droplets. Next!
The University of Surrey is asking about magnesium rockets. I'd heard of burning aluminium (as Surrey spell it) in oxygen, or maybe some even stronger oxidant like ozone. Burning metals isn't for Earth or LEO, but it intrigues me for low-grav takeoffs like our Moon - once bermed. Magnesium is just as common over there. But again, this looks rife with Unsolved Problems. The link will be here (pdf).
Absent a pdf, we do get an illustration. It looks like AI and makes little sense to my mortal eyesight. I just see magnesium is not planned for surface-to-orbit roggets the way some were talking aluminum. They want mass drivers, to take this fuel into orbit which rockets burn it up there. Into that topic, PlanetaryEngSys has butted: that mass drivers should start small, such that the capsule then fire the engines on that (parabolic) trajectory, to bring it to orbit. Seems more reasonable than Surrey's proposal frankly. ESA should pay that grant to them.