Here is the data I collected from the last round of 12S testing. Thanks to the bunch of you that help out in this process... Enterprise for two motors and a hand full of props, TimmyC and Liberty10 for some data off motors and props I don't have, and Tom K. for helping with the thrust measurements.
This test was to accommodate the 70-74 wingspan class planes, as well as the new 84 inch MXS using the DM5335-195Kv as the power option with 22x10 props. Going to a bigger prop is possible, but more power means more Amps and less flight time, and more than 2-to-1 thrust to weight seems to be enough power for even the power hog like me.
In the charts, you will see the motor listing, along with the labeled Kv, the unloaded Kv (ULKv), the prop information including the weight in grams (Pwt), and then a list of volts per cell (V/S).
I calculated the power values at each of these voltage levels, then highlighted in green the average voltage of the individual tests over a ten second blast at WOT with that specific prop. As a comparison, I also included the measured thrust off the Rapala during the ten second episode. With Tom's help and a new stationary scale mount, I think I have some very accurate and relative values. N/A is not available because I did not test the setup myself and don't have a Rapala reading for it. But I did do the calculations, which are highly accurate.
There is also a calculated RPMs per voltage level, and the RPMs in the green row are the statistical equivalent of the log data representation.
You will also see Amp readings. All values less than 73A are in blue and all values greater than 72.99 are in red. You can interpret this any way you want, but the red is simply an alert that with the 12S setups, this is where I began to see more heat than otherwise. I personally believe that heat and Amps are not joined at the hip, but when you are spinning 20 to 22 inch props on 550 to 700 gram motors to an RPM level that begins to produce 72+ Amps on 12S, you will begin to see an increase in heat versus time that is much higher than if you were not.
HP is calculated from Watt-out, PSPD is pitch speed and Mthrust is the actual measured thrust off the Rapala digital scale. In most instances, they are the statistical equivalent of the calculated thrust (CThrust).
There is a P/CF field as well that will be addressed at another time and deals with load constants and performance values relative to static testing carbon fiber props, composite props, and props with a D/P ratio of 1 or less.
Let me know if you have any questions.
View attachment Prop Comparisons 062214.pdf