Motors.
If you look up the motors used most have a voltage/prop chart that will give you the lift capacity at 50% - 100%.
Take the number of motors x the lift capacity at 50% throttle and that will give you the target lift capacity.
I have a QUAD that uses T-Motor U7 490KV motors and 18/6.1" props. On 6S battery power, each motor at 50% should be able to pull 2420 grams of thrust.
So 2420 x (4) motors = 9680 grams of total thrust at 50% throttle. That is 21.34lbs at 50% throttle. So i would want my rig's all up weight (rig, gimbal, cam and batts) to be no more than 21.34 lbs.
Hope that helps!
If you know your auw, you can reference the amp draw figures on the kde spec sheets for your prop size and voltage your using to predict hover time. take your auw in grams-to make it easy then divide by number of motors. this is the amount of thrust per motor you need to make your rig hover. reference the spec sheet for that thrust number per motor using the prop size and voltage your using and look at the amp draw. once you know how many amps per motor are being used to hover- multiply that number by the amount of motors on your rig to get overall total hover amp draw. Then convert your batt mah to amp hours then divide by total amp draw and multiply by 60. this will give you hover time ballpark wise if the auw numbers are correct and spec numbers provided by kde are correct. if the spec sheets are not exact for your auw just use closest figures for ballpark numbers.
here is a theoretical example since i cannot explain things well.lol ..
Say my 450 on 6s w/ 11inch props (auw) is 2760 grams. i divide 2760 by 4 to get minimum thrust per gram i need to lift my craft, ends up to be 690 grams of thrust. 2760/4= 690.
i reference the kde spec sheet chart for 6s with the 11X3.7 prop that i'm using and it tells me i can lift 690 grams at 50% throttle at a 2.9 amp draw-*see 515kv spec sheet w/ 6s and 11prop.
take 2.9amps and multiply by number of motors which is 4 on my quad and that equals 11.6 amps for hover for my rig. 2.9*4=11.6
I'm using a 6s 5000mah batt so i convert to amp hours 5000mah becomes 5.0ah then divide by the total amp draw figure which was 11.6 and then multiply by 60...
what it looks like----5.0ah/11.6amps X 60=25.86 ish min-hover time .
* this is using 100% of the battery so multiply the hover time by .8 to use only 80% of the total mah to keep lipo happy which will give you 20.6ish hover time. this is hover time not flight time, can't predict how heavy on the throttle your going to be during flight, altitude, wind etc these can effect numbers as well as components that also use some mah but this will give you ballpark numbers and has worked for me making predictions on builds and comparing motors. The kde's are great, the computer balancing is a biggie for me as i'm only interested in the end raw video result, jello for me is a no no and the added efficiency and build quality of these motors is icing on the cake.
you can also find your amp draw for your flight if you don't have osd with telemetry by using flight time and mah used. simply take mah used convert to amp hour divide by flight time and multiply by 60- thats your total amp draw for your flight.
ex- my 450 used 4000mah and flew for 20.6 minutes. so 4.0/20.6* 60= 11.6 amps---
the only problem with the 50% argument is that some of the flight controllers don't love hovering at 50% and actually do much better in the 60 to 70% range. This has been my experience with DJI controllers, for example.
IMHO.
I saw this on another thread I think the user was "Sk8brd" or something like that but he nailed it.. again all based off 50% thrust:
I wonder what my max payload would be then? X4 (8 motor config).
Motors are Torx Power Pro 3536
40A Maytech Esc’s
Props 13x6.5 Carbons
If you can get this kind of lift from a quad, why does anyone deal with the extra arms, extra weight, extra size and extra cost of an octo to fly large cameras? Is your quad not half-ish the price of a heavy-lifting octo? Your quad will lift my Scarlet no problem.