This prop has a high pitch and that could be intresting when executing coaxial benchmarks with different propellors. As for a single prop benchmarks it looks like a higher pitch increases the negative prop wash effect on the pull motor. So the difference in consumption between the push and pull motor is lager then with props that have a smaler pitch.
For this prop I have the same motor temperature remark as for the 10 inch Slow Fly prop.
The difference between puller and pusher configuration is ~10% .
The values in bold at 225 gram thrust is what I need for my current Y6-copter project.
Test is performed with a 12V power supply (= 3Cell lipo battery).
Test is performed with a 12V power supply (= 3Cell lipo battery).
Thrust
grams
|
10x60 pull
watt
|
10x60 push
watt
|
push-pull
%
|
25
|
3,8
|
3,5
|
7,9
|
50
|
6,9
|
6,3
|
8,7
|
75
|
10,6
|
8,8
|
17,0
|
100
|
13,9
|
11,9
|
14,4
|
125
|
17,3
|
14,7
|
15,0
|
150
|
20,7
|
17,5
|
15,5
|
175
|
23,9
|
20,1
|
15,9
|
200
|
27,8
|
23,9
|
14,0
|
225
|
31
|
27,8
|
10,3
|
250
|
35
|
31,4
|
10,3
|
275
|
39,1
|
34,7
|
11,3
|
300
|
42,9
|
38,7
|
9,8
|
325
|
47,6
|
42,5
|
10,7
|
350
|
51,5
|
46,8
|
9,1
|
375
|
55,5
|
50,5
|
9,0
|
400
|
61,1
|
55
|
10,0
|
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