Earlier quoted context omitted.
The existing helicopter is extremely small and light, IIRC. less than one kg. So it definitely won't be picking up a 900kg rover, even if you tried to scale it up somehow. The atmosphere is just too thin to support anything but a minimal payload. But yeah having more helicopters might be feasible - for surveying the surface.
Is there a problem of scaling this up to say a 20kg payload? I’m not an aeronautical engineer, so I guess what I’m asking is if there is some problem scaling up flying machines in an extremely thin atmosphere?
https://ieeexplore.ieee.org/abstract/document/9843501
In short: 30kg heli, 5kg payloads. Other designs by collaborators are closer to 20kg. It's probably possible to transport a few of these on the existing lander technology, which would be awesome.
The scholar.google.com keywords you want are "Mars Science Helicopter" and a good touchpoint author is T. Tzanetos or S. Withrow-Maser
Ames and JPL were still collaborating on this when I worked there.