Our European agencies (EASA) and the national one, AESA have kinetic impact assignment tables, according to a specific model (when you register your aircraft to operate in a specific category).
That makes far more sense than using only mass as the determining factor. Velocity is an important contributing factor.
Kinetic Energy K.E. = 1/2 Mass x Velocity squared.
kilograms-meters squared per second squared (Joules) = 1/2m (kg) x V(m/sec)^2
But it significantly complicates the regulations. It's so much easier to just pick weight as the determining factor, even if it makes no sense.
If you need to take velocity into account, as described in DJI's response, then you need to know either the maximum vertical velocity of the drone falling at terrminal velocity out of the sky, or it will be the horizontal velocity at the drone's maximum speed capability, or a combination of the two. That's starting to get complicated...
Generalizing, only aircraft with a MTOW greater than 800 gr. exceed those 80 Joules of kinetic impact, which implies that you must use mitigations such as a parachute.
But here again we have the grossly over simplified 80 Joules number. Kinetic energy alone isn't enough to determine what sort of injury may result. Given a known mass and a known velocity, you can calculate the Kinetic Energy. But surely the
shape of an object will significantly affect what sorts of damage will be delivered by that energy.
A sharply pointed dart or arrowhead will produce a totally
different type of injury, compared to a golf ball, compared to a basketball, compared to a piece of sharp metal shrapnel, compared to a styrofoam model plane, compared to a plastic multirotor drone, even if each of them were
equally carrying 80 Joules of kinetic energy.
It's ridiculous to claim you have the exact same 30% chance of fatality if struck in the head in each of the above cases.
Although parachutes are required by law with aircraft with MTOW greater than 250 gr when flying in an urban setting (specific cat.)
And yet those parachutes are required only for
unmanned aircraft weighing more than 250 grams, not for
all aircraft (i,e, manned aircraft). Curious, isn't it? A lot of effort has gone into imposing regulations to address problems that don't seem to exist.