https://spaceflightnow.com/2018/05/14/helicopter-to-accompan...
> She said the size of the rotors was restricted to 1.2 meters by the space available on the Mars 2020 rover’s belly pan. In turn, the 1.2-meter rotor diameter limits the mass of the helicopter to 4 pounds — 1.8 kilograms — based on the rarefied density of the Martian atmosphere.
> “The biggest thing is the atmospheric density at Mars is very thin,” Aung said in an interview Friday. “It’s 1 percent of that at Earth. It’s equivalent to about 100,000 feet in altitude here on Earth. The other difference is the gravity at Mars is lower. It’s about 40 percent. That plays into how much we can lift.”
> The rotors on the Mars Helicopter will spin between 2,400 and 2,900 rpm, about 10 times faster than a helicopter flying in Earth’s atmosphere.
Here it is running in test chamber at mars equivalent atmospheric density - https://www.youtube.com/watch?v=tMCJGfwj3rY
The thin atmosphere cuts both ways. It generates less lift. But it inflicts less drag.
Would they work in Mars' atmosphere?
This is basically a project that was "Let's try this, how much weight does the mission have to spare? Ouch, that's not a lot, let's see what we can do", that's my takeaway from this episode anyway https://www.planetary.org/multimedia/planetary-radio/show/20...
2) Yes, we've known for a while now that Mars has water ice. This is new science because they've built up a comprehensive map with the goal of identifying good landing sites for future missions to Mars, in particular missions focused on in-situ resource utilization of Martian water ice. The data is derived from current Mars probes, the Mars Reconnaisance Orbiter and Mars Odyssey Orbiter.
[1] https://www.nasa.gov/feature/jpl/nasas-treasure-map-for-wate...