You could probably use the data to figure out what fraction of the total drag the landing gear represents. I wouldn't be surprised if it was 1/3 the entire drag load of the airplane in level flight.
I wouldn't have been surprised either. Landing gear drag is less than I expected, however. I calculated landing gear drag energy, which is pretty easy if you can guess wheel c
d, particularly when Peter went to the effort to express his data in our quaint units, not to mention our language. Divide landing gear drag energy by prop and electrical efficiencies to get battery energy increment due to extended landing gear.
Peter gave us the real data, but I include the calculation for your amusement anyhow. Enter numbers in the yellow cells. I assumed Zürich airport elevation, 70 degrees F temperature, 50 degrees F dew point, baro set 29.97 inches Hg, to get air density and viscosity. Behold that this calculates extended-gear drag energy, but Peter measured extended-gear drag energy - retracted-gear drag energy. A retractable-gear airplane with gear retracted probably has more drag than a clean airplane.