I made a relatively small, 6 kg Quad VTOL. The setup and initial test flights went very well until I did a first endurance flight. With 40 18650 cells (2.1 kg, and AUW of 5.5 kg) the plane managed to fly 90 km, with one VTOL takeoff and one VTOL landing, with battery remaining capacity of about 10 %.
This was much less than I expected, although I did not do a preliminary calculation, because I was more worried about the VTOL setup and transition.
I started checking out the numbers, and discovered the following:
At 65 km/h it flies on 250 W electrical power, and at 95 km/h on 500 W. That should be around 170 W mechanical power for 65 km/h
I estimated the extra losses for the VTOL part as follows:
Motor and motor mounts: 18 W mechanical = 25 W electrical (=10 % of the total power)
Props which are not aligned with the wind: 44 W mech = 60 W electrical (during test flight both front props were perpendicular to the wind, and I do not know about the rear ones…) (= 22 %, up to of the total power, on average, around 14 .. 15 %).
There is also the issue of the forward motor prop which is here SK3-3548 1050 kV with 11 x 7 prop.
To improve overall efficiency, I will change the motor to Sunnysky 3520 560 kV with something like 14 x 8 prop, expecting about 10 % of improvement.
I also printed 3D cowlings for the motors, and I hope to get about 6 % improvement on these. (they add about 70 grams weight, around 1.5 % of the total weight, but they should more than halve the power lost now on drag on these items.














