I remember someone asked about the risk of engine nozzle blowing up moon dust that may damage Lanyue lander's engine while referring Apollo's ascent module engine is protected by the dscent module.
Here is a comparison.
Apollo's dscent engine is about kneel high (0.5 metre) to the surface, it is also 47KN which is more than 6 times powerful than Lanyue's 7500N engine (X4), or 1.6 times of Lanyue's total thrust. So Apollo lander certainly blew up lots of dust (at thousands metres per second) that put the engine in risk. Dust blown up by Lanyue's 4 smaller engine will be less than single engine of same total thrust because the dust spreads out in a larger area because of its travel trojectory. The four engines are also mounted about 1.8 metres higher than apollo using the astronout as a reference. This is more than 2 metres from the surface, dust does not reach this hight according to a research paper on the dust flow of Chang'e 5 mission
"The nozzle plume erosion property on lunar dust in Chang’E-5 mission"
Another thing to remember is that Lanyue is very different from Apollo, it uses a dedicated deceleration module to do the main job just before some kilometre above the surface then discard it, the lander will use smaller engines to land and ascent as one piece. Apollo has the descent module (more than half of the weight to reach the surface) reach the surface. So Lanyue's crew space should be much bigger than Apollo (the ascent module).
Overall, China's moon landing is similar in weight class to Apollo program. China sends 26+26=52 tonnes to LLO, Apollo had 50 tonnes. China dumps the major mass of landing complex before reaching the surface while Apollo had bigger mass to reach the surface and half of it becamed dead weight. It is analog to rocket launching, China does an earlier staging, Apollo did a late staging, the difference is China has a higher useful payload to the surface while Apollo has higher weight on surface.