I'm doing some bench testing with the 4 motors and 5 size/pitch props I have on hand. It's very interesting to see the change in thrust, with the same motor, battery and throttle position. Using a home made thrust meter build over a postal scale. And recharging the 2200 3s battery between each motor swap.
So far I have run 2 of the 4 motors with the props I have. I'll report my results when I have completed the other 2 motors.
At this time I'm not able to check actual rpm. Just working off of 25, 50, 75 and 100% of the throttle stick throw. Actual rpm and amp draw would be useful but I don't have the tools to measure these, and unless I really fall down the rabbit hole with this hobby I probably won't really ever need to have that ability.
It brings up a question.
How much thrust in necessary to fly a given plane? Obviously this isn't an easy question because of all the variables but I'm wondering if there is a sort of baseline that would provide a safe starting point.
For example lets consider a Tiny Trainer at AH E of 300 g.
Would a motor producing 200 grams of thrust be parquet to take off from the ground and fly? How about 100 g of thrust. Thinking of full size planes it's only been a recipient development that plane power exceeds weight so I'm guessing that, in the case of the 300 g. TT anything above 300 g of thrust is overkill, and considering the wing style kill might be just the right word.
I know many keep talking about watts but, to me, watts is still to abstract. How much pushing or pulling power is being actually produced seems much more usefully.
Thanks
So far I have run 2 of the 4 motors with the props I have. I'll report my results when I have completed the other 2 motors.
At this time I'm not able to check actual rpm. Just working off of 25, 50, 75 and 100% of the throttle stick throw. Actual rpm and amp draw would be useful but I don't have the tools to measure these, and unless I really fall down the rabbit hole with this hobby I probably won't really ever need to have that ability.
It brings up a question.
How much thrust in necessary to fly a given plane? Obviously this isn't an easy question because of all the variables but I'm wondering if there is a sort of baseline that would provide a safe starting point.
For example lets consider a Tiny Trainer at AH E of 300 g.
Would a motor producing 200 grams of thrust be parquet to take off from the ground and fly? How about 100 g of thrust. Thinking of full size planes it's only been a recipient development that plane power exceeds weight so I'm guessing that, in the case of the 300 g. TT anything above 300 g of thrust is overkill, and considering the wing style kill might be just the right word.
I know many keep talking about watts but, to me, watts is still to abstract. How much pushing or pulling power is being actually produced seems much more usefully.
Thanks
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