Mf Variable Pitch
T-Motor MF Variable-Pitch Klapp Propeller 1x CW 1x CCW 16 Zoll - MF1604VP
Artikelnr.: PM-7075 | HAN: MF1604VP
_x000D__x000D__x000D__x000D__x000D_
About MF1604VP Polymer Manual Pitch Folding Propeller
MF1604VP 16.4*5.9 inch polymer manual pitch folding propeller is a new type of propeller designed by T-MOTOR for multi-rotor and drogue UAVs. Compared with traditional propellers, MF1604VP provides a more flexible solution for complex and changeable working conditions and various power requirements, and it can be adjusted manually by changing the positioning block. The MF1604VP adopts an advanced aerodynamic design, which significantly improves flight efficiency at high speed and high altitude. Its large swept back tip and downward curved winglet design effectively improves the vortex distribution of the tip and reduces energy consumption and vibration, making it an ideal choice for professional users in model development and rapid switching between multiple scenarios. The maximum pulling force measured under throttle is 2.8kg (positioning block is 7.5°).
MF1604VP Highlights:
- Adopting new wing shape with large swept back tip and downward curved winglet design to improve the vortex distribution of the tip and realize the double enhancement of pulling force and efficiency; - Enhanced blade root design, together with improved material formula, greatly improves the service life of alternating load, and is more suitable for the large pulling force working condition and co-axial power mode;
Smaller change of rotational damping in the whole life cycle of the paddle: compared with the original hard compression assembly method, the gasket paddle root assembly is always in the state of compression, which greatly reduces the wear of the gasket and makes the rotational damping change in the whole life cycle of the paddle smaller and avoids the situation that the rotational tightness of the blade varies with the life span and there is a big difference between the paddle and the vibration, which is more safe and reliable;
Packing List Includes:
Package size 211*86*42mm MF1604VP polymer manual pitch folding Propeller * 1 pair MF1604 center positioning block (+2.5°)-CCW*1 MF1604 center positioning block (+2.5°)-CW*1 MF1604 Center Positioning Block (-2.5°)-CCW*1 MF1604 Center Positioning Block (-2.5°)-CW*1 MF1604 center positioning block (+5°)-CCW*1 MF1604 Center Positioning Block (+5°)-CW*1 20*14*3.3mm pads*2 M3*10mm cup head socket screws*4
Matching Guide:
T-MOTOR MN4012 KV340 Motor T-MOTOR MN4014 KV330 Motor T-MOTOR U7 KV490 Motor FLAME 60A 12S V2.0 ESC FLAME 180A 12S V2.0 ESC
_x000D__x000D_
MF VP SERIES PROPELLER
Manual Variable-Pitch Series
Simplicity Over Complexity, Consistency in Performance
Specially designed to address the issues of low flight efficiency at high speeds and high altitudes,_x000D_ this series is suitable for aircraft development and professional users requiring_x000D_ rapid switching across multiple scenarios.
Manual Variable-Pitch Series
Flexible and easy-to-use drone propulsion system enhances flight efficiency_x000D_ in various operating conditions.
Typical application scenarios include high-speed flight, high-altitude flight,_x000D_ adjustments for overall aircraft weight, and fine-tuning of custom propeller_x000D_ performance.
Limitations of Traditional Propellers: Fixed pitch and fixed aerodynamic_x000D_ characteristics leading to limited power and flight condition matching.
Drawbacks of the adjustable propellers available from the market:_x000D_ Low adjustment precision, complicated operation, requires large auxiliary_x000D_ tools, and cannot be quickly adjusted on-site.
T-MOTOR (New) manual adjustable variable-pitch series solution:_x000D_ Designed for complex and changing working conditions with diverse_x000D_ power demands, we provide flexible solutions that allow for quick manual_x000D_ pitch adjustment by simply changing the positioning blocks.
Quick Assembly and Disassembly_x000D_ Precise and Reliable
Quick to replace without requiring professional training—easy to learn_x000D_ and use. The pitch adjustment accuracy remains unaffected_x000D_ by manual operation errors with user-friendly operation.
??????,????00:0800:09
Methodical Approach
Using calculation tables derived from extensive experimental data,_x000D_ users can quickly find the required pitch angle based on the operating_x000D_ scenario and simple parameters.
(7.5°, 10°, and other positioning blocks are available upon request for customization.)
Performance Comparison
The efficiency curve of three positioning blocks (pitches) under_x000D_ different airflow speeds
(Example: MN605 KV170 + FLAME 180A 12S V2.0 + MF2211VP, Flight inclination 30°,_x000D_ S0, S5, S10, S15 respectively represents speed 0m/s, 5m/s, 10m/s, 15m/s,_x000D_ D0, D2.5, D5 respectively represents 0° positioning block, 2.5° positioning block, and 5° positioning block.)
Conclusion: As the positioning block angle (pitch) increases, the efficiency of the propeller improves at_x000D_ higher airflow speeds.
Multi-adaptability
The manual variable pitch propellers can not only support multi-rotor aircraft, but also effectively adapt to_x000D_ the needs of vertical take-off and landing aircraft,_x000D_ providing higher flexibility and performance to meet the requirements_x000D_ of different flight missions.
Multirotor
VTOL
Prototype Propellers Customization
Standard Customization
MOQ 1, with pitch angle customizable to 0.01°.
Assisted Customization
For mass production, engineers assist in determining the angle,_x000D_ and the customized pitch angle can be fixed before leaving the factory.
_x000D_ _x000D_ _x000D__x000D__x000D_ Technical Drawing_x000D__x000D_
_x000D__x000D__x000D__x000D_ Specification_x000D__x000D_
Model NO.
MF1604VP
T-MOTOR Series
Folding
Weight (Single Blade)
38.3g
Package Weight
158g
Diameter
16.4inch(416.56mm)
Package Size
211*86*42mm
Pitch
5.9inch(149.86mm)
Material
Polymer+CF
Recommended Thrust
0.5~2.2kg
Recommended Max Thrust
3kg
Ambient Temp
-40?~65?
Storage Temp/Humidity
-10?~50?/<85%
Recommendation
Recommended ESC
FLAME 60A 12S V2.0/FLAME 180A 12S V2.0
Recommended Motor
MN4012/MN4014/U7
_x000D__x000D__x000D__x000D__x000D_ Test Data_x000D__x000D_
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (0°)
10%
24
90
0.02
0.30
1405
3
12.43
40 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
24
156
0.04
0.50
1748
7
13.13
20%
24
232
0.05
0.75
2049
11
12.99
25%
24
315
0.07
1.04
2343
17
12.66
30%
24
404
0.08
1.42
2627
22
11.92
35%
24
500
0.10
1.82
2905
30
11.48
40%
24
616
0.13
2.36
3189
43
10.89
45%
24
722
0.14
2.97
3469
51
10.17
50%
24
874
0.17
3.72
3758
67
9.85
55%
24
988
0.20
4.48
4019
84
9.24
60%
24
1132
0.22
5.30
4265
98
8.96
65%
24
1252
0.24
6.17
4501
113
8.51
70%
24
1380
0.27
7.10
4728
134
8.17
75%
24
1503
0.29
8.07
4947
150
7.84
80%
24
1637
0.31
9.14
5154
167
7.55
85%
24
1768
0.34
10.29
5376
191
7.25
90%
24
1921
0.37
11.60
5592
217
7.00
95%
24
2065
0.40
12.92
5801
243
6.77
100%
24
2275
0.44
14.89
6077
280
6.48
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (+2.5°)
10%
24
126
0.03
0.35
1357
4
14.96
42 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
24
200
0.04
0.57
1666
7
14.63
20%
24
300
0.06
0.89
1996
13
14.14
25%
24
437
0.08
1.25
2276
19
14.63
30%
24
527
0.10
1.67
2550
27
13.16
35%
24
607
0.13
2.16
2817
38
11.73
40%
24
725
0.15
2.79
3090
49
10.88
45%
24
854
0.18
3.51
3356
63
10.17
50%
24
1013
0.21
4.43
3641
80
9.59
55%
24
1145
0.24
5.29
3875
97
9.07
60%
24
1304
0.27
6.26
4099
116
8.74
65%
24
1413
0.29
7.28
4316
131
8.16
70%
24
1532
0.32
8.42
4517
151
7.65
75%
24
1671
0.35
9.61
4724
173
7.32
80%
24
1797
0.38
10.83
4919
196
6.99
85%
24
2002
0.41
12.23
5114
220
6.91
90%
24
2147
0.44
13.71
5306
244
6.62
95%
24
2321
0.48
15.37
5499
276
6.39
100%
24
2544
0.53
17.68
5754
319
6.11
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (+5°)
10%
24
153
0.03
0.41
1322
4
15.56
47 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
24
238
0.05
0.66
1634
9
14.97
20%
24
343
0.07
1.02
1951
14
14.03
25%
24
466
0.10
1.42
2169
23
13.70
30%
24
592
0.12
1.91
2488
31
12.97
35%
24
696
0.15
2.49
2734
43
11.69
40%
24
823
0.18
3.20
2995
56
10.75
45%
24
972
0.21
4.07
3244
71
10.00
50%
24
1122
0.24
5.00
3477
87
9.40
55%
24
1281
0.28
6.17
3728
109
8.72
60%
24
1422
0.31
7.24
3935
128
8.26
65%
24
1581
0.35
8.46
4135
152
7.86
70%
24
1708
0.39
9.77
4329
177
7.37
75%
24
1848
0.42
11.14
4507
198
7.00
80%
24
1990
0.45
12.60
4693
221
6.67
85%
24
2138
0.49
14.20
4871
250
6.38
90%
24
2308
0.53
15.95
5040
280
6.14
95%
24
2460
0.56
17.75
5221
306
5.89
100%
23
2709
0.62
20.49
5449
354
5.64
MN4012 KV340 + FLAME 60A 12S V2.0 + MF1604VP (+7.5°)
10%
24
195
0.05
0.46
1293
7
17.78
52 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
24
276
0.07
0.76
1596
12
15.14
20%
24
382
0.09
1.16
1901
18
13.73
25%
24
497
0.12
1.65
2162
27
12.61
30%
24
625
0.15
2.21
2417
38
11.79
35%
24
744
0.18
2.87
2647
50
10.82
40%
24
882
0.21
3.68
2884
63
10.03
45%
24
1028
0.25
4.64
3123
82
9.27
50%
24
1187
0.29
5.73
3341
101
8.69
55%
24
1332
0.33
6.89
3554
123
8.12
60%
24
1483
0.36
8.18
3758
142
7.62
65%
24
1642
0.40
9.70
3962
166
7.13
70%
24
1805
0.44
11.16
4136
191
6.83
75%
24
1965
0.48
12.72
4309
217
6.53
80%
24
2121
0.53
14.43
4472
248
6.23
85%
24
2243
0.56
16.23
4636
272
5.87
90%
T-Motor MF Variable-Pitch Klapp Propeller 1x CW 1x CCW 22 Zoll - MF2211VP
Artikelnr.: PM-7076 | HAN: MF2211VP
_x000D__x000D__x000D__x000D__x000D_
About The MF2211VP Polymer Manual Pitch Folding Propeller
The MF2211VP is a cutting-edge 22.4*8 inch polymer manual pitch folding propeller, expertly designed by T-MOTOR for multi-rotor and VTOL drones. In comparison with conventional propellers, the MF2211VP is engineered to address complex and variable flight conditions and diverse power requirements. Its design facilitates manual pitch adjustment with a straightforward replacement of the positioning block, eliminating the need for additional tools. This feature enhances the efficiency of professional model development in dynamic, multi-scenario environments.
MF2211VP's Highlights:
Its aerodynamic design enhances flight efficiency under high-speed and high-altitude conditions.
The tip design, with its large swept back tip and downward curved winglets, optimizes tip vortex distribution, reducing energy consumption and vibration. This makes it ideal for professional users.
The commonly used pulling force range is from 0.5 to 2.2 kilograms.
The maximum pull force, when paired with the T-MOTOR MN4012 KV340 motor and FLAME 60A 12S V2.0 ESC, is 2.8kg at maximum throttle (with a 7.5° positioning block), and the recommended maximum pull force is 3kg.
Packing List Includes:
Package size: 300*106*45mm MF2211 center positioning block (+2.5°)-CCW*1 MF2211 Center Positioning Block (+2.5°)-CW*1 MF2211 Center Positioning Block (-2.5°)-CCW*1 MF2211 Center Positioning Block (-2.5°)-CW*1 MF2211 Center Positioning Block (+5°)-CCW*1 MF2211 center locating block (+5°)-CW*1 M3*10mm cup head socket head cap screws*4
Matching Guide:
T-MOTOR MN605 KV170 Motor T-MOTOR FLAME 60A 12S V2.0 ESC _x000D_ T-MOTOR FLAME 180A 12S V2.0 ESC
_x000D__x000D_
MF VP SERIES PROPELLER
Manual Variable-Pitch Series
Simplicity Over Complexity, Consistency in Performance
Specially designed to address the issues of low flight efficiency at high speeds and high altitudes,_x000D_ this series is suitable for aircraft development and professional users requiring_x000D_ rapid switching across multiple scenarios.
Manual Variable-Pitch Series
Flexible and easy-to-use drone propulsion system enhances flight efficiency_x000D_ in various operating conditions.
Typical application scenarios include high-speed flight, high-altitude flight,_x000D_ adjustments for overall aircraft weight, and fine-tuning of custom propeller_x000D_ performance.
Limitations of Traditional Propellers: Fixed pitch and fixed aerodynamic_x000D_ characteristics leading to limited power and flight condition matching.
Drawbacks of the adjustable propellers available from the market:_x000D_ Low adjustment precision, complicated operation, requires large auxiliary_x000D_ tools, and cannot be quickly adjusted on-site.
T-MOTOR (New) manual adjustable variable-pitch series solution:_x000D_ Designed for complex and changing working conditions with diverse_x000D_ power demands, we provide flexible solutions that allow for quick manual_x000D_ pitch adjustment by simply changing the positioning blocks.
Quick Assembly and Disassembly_x000D_ Precise and Reliable
Quick to replace without requiring professional training—easy to learn_x000D_ and use. The pitch adjustment accuracy remains unaffected_x000D_ by manual operation errors with user-friendly operation.
??????,????00:0300:09
Methodical Approach
Using calculation tables derived from extensive experimental data,_x000D_ users can quickly find the required pitch angle based on the operating_x000D_ scenario and simple parameters.
(7.5°, 10°, and other positioning blocks are available upon request for customization.)
Performance Comparison
The efficiency curve of three positioning blocks (pitches) under_x000D_ different airflow speeds
(Example: MN605 KV170 + FLAME 180A 12S V2.0 + MF2211VP, Flight inclination 30°,_x000D_ S0, S5, S10, S15 respectively represents speed 0m/s, 5m/s, 10m/s, 15m/s,_x000D_ D0, D2.5, D5 respectively represents 0° positioning block, 2.5° positioning block, and 5° positioning block.)
Conclusion: As the positioning block angle (pitch) increases, the efficiency of the propeller improves at_x000D_ higher airflow speeds.
Multi-adaptability
The manual variable pitch propellers can not only support multi-rotor aircraft, but also effectively adapt to_x000D_ the needs of vertical take-off and landing aircraft,_x000D_ providing higher flexibility and performance to meet the requirements_x000D_ of different flight missions.
Multirotor
VTOL
Prototype Propellers Customization
Standard Customization
MOQ 1, with pitch angle customizable to 0.01°.
Assisted Customization
For mass production, engineers assist in determining the angle,_x000D_ and the customized pitch angle can be fixed before leaving the factory.
_x000D_ _x000D__x000D__x000D__x000D_ Technical Drawing_x000D__x000D_
_x000D__x000D__x000D__x000D_ Specification_x000D__x000D_
Model NO.
MF2211VP
T-MOTOR Series
Folding
Weight(Single Blade)
86.5g
Package Weight
286g
Diameter
22.4inch(568.96mm)
Package Size
300*106*45mm
Pitch
8inch(203.2mm)
Material
Polymer+CF
RecommendedThrust
1.5~5kg
Recommended Max Thrust
12kg
Ambient Temp
-40?~65?
StorageTemp/Humidity
-10?~50?/<85%
Recommendation
Recommended ESC
FLAME 60A 12S V2.0/FLAME 180A 12S V2.0
Recommended Motor
MN605 KV170
_x000D__x000D__x000D__x000D__x000D_ Test Data_x000D__x000D_
MN605 KV170 + FLAME 60A 12S V2.0 + MF2211VP (0°)
10%
48
482
0.15
0.81
1397
22
12.44
77 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
48
748
0.22
1.30
1712
39
12.02
20%
48
1043
0.30
1.90
1989
62
11.45
25%
48
1378
0.38
2.65
2262
90
10.86
30%
48
1763
0.49
3.58
2544
131
10.28
35%
48
2266
0.62
5.00
2869
186
9.47
40%
48
2891
0.78
7.04
3239
265
8.59
45%
48
3402
0.92
9.09
3512
338
7.84
50%
48
3961
1.06
10.95
3791
421
7.59
55%
48
4554
1.21
13.33
4052
513
7.17
60%
48
5101
1.35
15.59
4290
606
6.88
65%
47
5670
1.49
18.28
4514
704
6.53
70%
47
6260
1.65
21.27
4764
823
6.21
75%
47
6885
1.81
24.48
4993
946
5.94
80%
47
7495
1.97
27.82
5220
1077
5.70
85%
47
8181
2.14
31.64
5443
1220
5.48
90%
47
8813
2.30
35.56
5661
1363
5.27
95%
47
9474
2.47
39.90
5862
1516
5.06
100%
47
10479
2.73
47.12
6185
1768
4.76
MN605 KV170 + FLAME 60A 12S V2.0 + MF2211VP (+2.5°)
10%
48
563
0.17
0.85
1343
24
13.89
122 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
48
875
0.27
1.45
1662
47
12.61
20%
48
1231
0.37
2.18
1950
76
11.80
25%
48
1618
0.48
3.13
2224
112
10.80
30%
48
2065
0.61
4.30
2498
160
10.04
35%
48
2598
0.76
5.96
2804
223
9.12
40%
48
3371
0.98
8.64
3185
327
8.17
45%
48
3906
1.14
10.74
3424
409
7.63
50%
48
4565
1.33
13.36
3681
513
7.17
55%
48
5211
1.51
16.35
3926
621
6.70
60%
47
5849
1.70
19.54
4160
741
6.30
65%
47
6413
1.86
22.41
4352
848
6.04
70%
47
7101
2.05
26.07
4595
986
5.76
75%
47
7740
2.24
29.97
4788
1123
5.47
80%
47
8444
2.44
34.28
4986
1274
5.23
85%
47
9163
2.64
38.94
5179
1432
5.01
90%
47
9840
2.84
44.00
5366
1596
4.78
95%
47
10553
3.05
49.46
5551
1773
4.57
100%
46
11590
3.35
58.25
5797
2034
4.29
MN605 KV170 + FLAME 60A 12S V2.0 + MF2211VP (+5°)
10%
48
606
0.20
0.88
1306
27
14.28
103 (Motor temperature after 1 minutes of operation) (Ambient Temperature:25?) (There is a risk of burnout)
15%
48
954
0.31
1.57
1620
53
12.67
20%
48
1349
0.44
2.45
1908
88
11.47
25%
48
1782
0.57
3.57
2178
130
10.41
30%
48
2283
0.73
4.99
2446
187
9.56
35%
48
2872
0.91
6.94
2735
261
8.65
40%
48
3502
1.11
9.29
3021
351
7.89
45%
48
4264
1.36
12.58
3331
474
7.11
50%
48
4933
1.57
15.73
3575
588
6.59
55%
48
5606
1.79
19.15
3803
713
6.16
60%
47
6251
2.00
22.69
4018
842
5.81
65%
47
6940
2.22
26.84
4224
982
5.47
70%
47
7539
2.41
30.67
4402
1111
5.21
75%
47
8237
2.63
35.23
4598
1266
4.97
80%
47
8939
2.86
40.55
4768
1428
4.70
85%
47
9586
3.07
45.76
4925
1583
4.48
90%
47
10229
3.29
51.65
5082
1751
4.25
95%
46
10951
3.53
61.90
5246
1939
3.82
100%
46
11680
3.77
72.77
5405
2134
3.49
MN605 KV170 + FLAME 60A 12S V2.0 + MF2211VP (+7.5°)
10%
48
655
0.24
0.98
1268
32
13.91
92 (Motor temperature after 30 Second of operation) (Ambient Temperature:25?) (There is a risk of burnout)
15%
48
1036
0.37
1.79
1582
61
12.06
20%
48
1464
0.53
2.84
1865
104
10.74
25%
48
1941
0.69
4.20
2132
154
9.65
30%
48
2454
0.87
5.84
2394
218
8.78
35%
48
3060
1.08
8.05
2664
301
7.96
40%
48
3731
1.32
10.82
2930
405
7.22
45%
48
4508
1.60
14.56
3216
539
6.51
50%
48
5191
1.85
18.39
3453
669
5.94
55%
47
5845
2.08
22.23
3658
797
5.55
60%
47
6500
2.32
26.43
3851
936
5.20
65%
47
7148
2.56
31.07
4033
1081
4.88
70%
47
7766
2.79
36.01
4208
1230
4.59
75%
47
8413
3.01
40.94
4356
1373
4.38
80%
47
9022
3.24
46.93
4502
1527
4.12
85%
46
9589
3.45
56.90
4625
1671
3.63
90%
46
9962
3.60
63.40
4713
1777
3.40
95%
46
10268
3.72
70.29
4784
1864
3.17
100%
46
10709
3.89
81.39
4878
1987
2.88
MN605 KV170 + FLAME 60A 12S V2.0 + MF2211VP (+10°)
10%
48
660
0.28
1.08
1238
36
12.75
102 (Motor temperature after 20 Second of operation) (Ambient Temperature:25?) (This angle is not recommended for static testing)
15%
48
1074</
T-Motor MF Variable-Pitch Klapp Propeller 1x CW 1x CCW 24 Zoll - MF2412VP
Artikelnr.: PM-7077 | HAN: MF2412VP
_x000D__x000D__x000D__x000D__x000D__x000D__x000D_
MF VP SERIES PROPELLER
Manual Variable-Pitch Series
Simplicity Over Complexity, Consistency in Performance
Specially designed to address the issues of low flight efficiency at high speeds and high altitudes,_x000D_ this series is suitable for aircraft development and professional users requiring_x000D_ rapid switching across multiple scenarios.
Manual Variable-Pitch Series
Flexible and easy-to-use drone propulsion system enhances flight efficiency_x000D_ in various operating conditions.
Typical application scenarios include high-speed flight, high-altitude flight,_x000D_ adjustments for overall aircraft weight, and fine-tuning of custom propeller_x000D_ performance.
Limitations of Traditional Propellers: Fixed pitch and fixed aerodynamic_x000D_ characteristics leading to limited power and flight condition matching.
Drawbacks of the adjustable propellers available from the market:_x000D_ Low adjustment precision, complicated operation, requires large auxiliary_x000D_ tools, and cannot be quickly adjusted on-site.
T-MOTOR (New) manual adjustable variable-pitch series solution:_x000D_ Designed for complex and changing working conditions with diverse_x000D_ power demands, we provide flexible solutions that allow for quick manual_x000D_ pitch adjustment by simply changing the positioning blocks.
Quick Assembly and Disassembly_x000D_ Precise and Reliable
Quick to replace without requiring professional training—easy to learn_x000D_ and use. The pitch adjustment accuracy remains unaffected_x000D_ by manual operation errors with user-friendly operation.
??????,????00:0200:09
Methodical Approach
Using calculation tables derived from extensive experimental data,_x000D_ users can quickly find the required pitch angle based on the operating_x000D_ scenario and simple parameters.
(7.5°, 10°, and other positioning blocks are available upon request for customization.)
Performance Comparison
The efficiency curve of three positioning blocks (pitches) under_x000D_ different airflow speeds
(Example: MN605 KV170 + FLAME 180A 12S V2.0 + MF2211VP, Flight inclination 30°,_x000D_ S0, S5, S10, S15 respectively represents speed 0m/s, 5m/s, 10m/s, 15m/s,_x000D_ D0, D2.5, D5 respectively represents 0° positioning block, 2.5° positioning block, and 5° positioning block.)
Conclusion: As the positioning block angle (pitch) increases, the efficiency of the propeller improves at_x000D_ higher airflow speeds.
Multi-adaptability
The manual variable pitch propellers can not only support multi-rotor aircraft, but also effectively adapt to_x000D_ the needs of vertical take-off and landing aircraft,_x000D_ providing higher flexibility and performance to meet the requirements_x000D_ of different flight missions.
Multirotor
VTOL
Prototype Propellers Customization
Standard Customization
MOQ 1, with pitch angle customizable to 0.01°.
Assisted Customization
For mass production, engineers assist in determining the angle,_x000D_ and the customized pitch angle can be fixed before leaving the factory.
_x000D_ _x000D__x000D__x000D__x000D_ Technical Drawing_x000D__x000D_
_x000D__x000D__x000D__x000D_ Specification_x000D__x000D_
Model NO.
MF2412VP
T-MOTOR Series
Folding
Weight(Single Blade)
115.8g
Package Weight
337.2g
Diameter
24.4inch(619.76mm)
Package Size
305*127*48mm
Pitch
8.7inch(220.98mm)
Material
Polymer+CF
RecommendedThrust
2.8~6kg
RecommendedMax Thrust
13kg
Ambient Temp
-40?~65?
Storage Temp/Humidity
-10?~50?/<85%
Recommendation
Recommended ESC
FLAME 180A 12S V2.0
Recommended Motor
MN705 KV140/MN701 KV135
_x000D__x000D__x000D__x000D__x000D_ Test Data_x000D__x000D_
MN705 KV140 + FLAME 180A 12S V2.0 + MF2412VP (0°)
10%
48
48
0.01
0.13
374
0
8.00
65 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
48
193
0.06
0.34
733
5
11.92
20%
48
408
0.13
0.69
1077
15
12.24
25%
48
708
0.22
1.21
1409
32
12.15
30%
48
1073
0.34
1.91
1717
61
11.68
35%
48
1555
0.47
3.09
2048
101
10.50
40%
48
2070
0.63
4.30
2334
154
10.06
45%
48
2597
0.77
5.63
2614
211
9.63
50%
48
3364
1.00
8.36
2971
311
8.42
55%
48
4166
1.21
11.15
3297
418
7.82
60%
48
4933
1.44
14.29
3586
541
7.24
65%
48
5704
1.65
17.32
3850
665
6.93
70%
47
6622
1.92
21.66
4147
834
6.44
75%
47
7782
2.23
27.69
4493
1049
5.94
80%
47
8613
2.46
32.23
4783
1232
5.67
85%
47
9496
2.69
37.31
4960
1397
5.41
90%
47
10286
2.92
42.31
5167
1580
5.18
95%
47
10941
3.11
46.51
5333
1737
5.03
100%
47
10948
3.10
46.76
5334
1732
5.00
MN705 KV140 + FLAME 180A 12S V2.0 + MF2412VP (+2.5°)
10%
48
47
0.00
0.14
373
0
6.89
82 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
48
225
0.06
0.37
728
5
12.56
20%
48
491
0.15
0.79
1076
17
12.94
25%
48
852
0.26
1.45
1404
38
12.24
30%
48
1249
0.40
2.25
1697
71
11.59
35%
48
1803
0.57
3.52
2007
120
10.69
40%
48
2395
0.75
5.07
2281
179
9.85
45%
48
3066
0.95
6.88
2550
254
9.30
50%
48
3953
1.23
10.05
2894
373
8.24
55%
48
4881
1.53
13.92
3217
515
7.35
60%
48
5761
1.81
17.62
3484
660
6.87
65%
47
6601
2.06
21.46
3727
804
6.48
70%
47
7640
2.40
26.92
4007
1007
6.00
75%
47
8900
2.77
34.18
4319
1253
5.52
80%
47
9734
3.05
39.72
4516
1442
5.22
85%
47
10600
3.31
45.56
4791
1661
4.97
90%
47
11438
3.58
51.91
4932
1849
4.72
95%
47
12130
3.78
57.46
5080
2011
4.54
100%
47
12140
3.80
57.57
5072
2018
4.54
MN705 KV140 + FLAME 180A 12S V2.0 + MF2412VP (+5°)
10%
48
53
0.02
0.12
373
1
9.43
72 (Motor temperature after 1 minutes of operation) (Ambient Temperature:25?)
15%
48
245
0.09
0.38
724
7
13.42
20%
48
524
0.19
0.83
1059
21
13.21
25%
48
905
0.33
1.55
1377
48
12.15
30%
48
1360
0.49
2.51
1667
86
11.29
35%
48
1947
0.70
4.00
1966
144
10.15
40%
48
2565
0.91
5.76
2234
213
9.31
45%
48
3248
1.15
7.83
2493
300
8.68
50%
48
4234
1.49
11.78
2828
441
7.53
55%
48
5191
1.83
15.90
3123
598
6.86
60%
47
6136
2.15
20.53
3387
763
6.29
65%
47
7023
2.46
25.03
3615
931
5.92
70%
47
8120
2.85
31.69
3877
1157
5.43
75%
47
9156
3.22
38.54
4112
1387
5.06
80%
47
10208
3.59
46.60
4329
1627
4.68
85%
47
11148
3.93
54.78
4515
1858
4.37
90%
46
12032
4.25
63.35
4706
2095
4.10
95%
46
12725
4.50
71.38
4801
2263
3.87
100%
46
12676
4.49
71.13
4788
2251
3.87
MN705 KV140 + FLAME 180A 12S V2.0 + MF2412VP (+7.5°)
10%
48
64
0.03
0.16
371
1
8.12
82 (Motor temperature after 1 minutes of operation) (Ambient Temperature:25?) (This angle is not recommended for static testing)
15%
48
273
0.12
0.45
716
9
12.61
20%
48
602
0.24
0.97
1047
26
12.93
25%
48
1039
0.41
1.83
1353
58
11.85
30%
48
1546
0.62
2.97
1636
106
10.86
35%
48
2168
0.84
4.68
1921
169
9.68
40%
48
2830
1.10
6.73
2177
251
8.79
45%
48
3524
1.37
9.09
2428
348
8.11
50%
48
4553
1.76
13.53
2750
507
7.06
55%
48
5575
2.16
18.80
3038
687
6.24
60%
47
6513
2.53
23.65
3275
868
5.81
65%
47
7467
2.90
29.37
3498
1062
5.38
70%
47
8512
3.32
37.00
3732
1298
4.89
75%
47
9532
3.72
44.88
3939
1534
4.54
80%
47
10395
4.06
52.19
4102
1744
4.28
85%
46
11264
4.41
65.19
4267
1971
3.74
90%
46
11594
4.54
82.51
4329
2058
3.07
95%
45
11728
4.61
92.94
4353
2102
2.78
100%
45
11554
4.54
91.07
4326
2057
2.79
MN705 KV140 + FLAME 180A 12S V2.0 + MF2412VP (+10°)
10%
48
63
0.03
0.14
365
1
9.10
104 (Motor temperature after 1 minutes of operation) (Ambient Temperature:25?) (This angle is not recommended for static testing)
15%
48
264
0.14
0.46
705
10
11.92
20%
48
607
0.31
1.09
1030
33
11.63
25%
48
1078
0.48
2.00
1338
67
11.23
30%
48
1603
0.69
3.25
1607
116
10.28
35%
48
2236
0.96
5.17
1889
190
9.04
40%
48
2905
1.24
7.33
2140
278
8.29
45%
48
3626
1.55
10.05
2383
387
7.56
50%
48
4678
1.98
14.96
2695
559
6.57
55%
47
5693
2.41
20.59
2976
751
5.82
60%
47
6622
2.82
26.15
3205
947
5.35
65%
47
7553
3.22
32.36
3416
1152
4.95
70%
47
8562
3.69
41.32
3635
1405
4.42
75%
47
9525
4.13
51.50
3828
1655
3.97
80%
46
10243
4.46
59.70
3966
1852
3.70
85%
46
10794
4.72
73.01
4073
2013
3.21
90%
46
10802
4.73
90.81
4074
2018
2.61
95%
45
10988
4.84
98.19
4115
2086
2.47
100%
45
10749
4.74
97.09
4077
2024
2.44
MN705 KV140 + FLAME 180A 12S V2.0 + MF2412VP (-2.5°)
10%
48
32
0.01
0.15
375
0
4.50
53 (Motor temperature after 1 minutes of operation) (Ambient Temperature:25?)
15%
48
136
0.05
0.33
741
4
8.50
20%
48
317
0.10
0.67
1063
11
9.86
25%
48
5
T-Motor MF Variable-Pitch Klapp Propeller 1x CW 1x CCW 26 Zoll - MF2614VP
Artikelnr.: PM-7078 | HAN: MF2614VP
_x000D__x000D_
MF VP SERIES PROPELLER
Manual Variable-Pitch Series
Simplicity Over Complexity, Consistency in Performance
Specially designed to address the issues of low flight efficiency at high speeds and high altitudes,_x000D_ this series is suitable for aircraft development and professional users requiring_x000D_ rapid switching across multiple scenarios.
Manual Variable-Pitch Series
Flexible and easy-to-use drone propulsion system enhances flight efficiency_x000D_ in various operating conditions.
Typical application scenarios include high-speed flight, high-altitude flight,_x000D_ adjustments for overall aircraft weight, and fine-tuning of custom propeller_x000D_ performance.
Limitations of Traditional Propellers: Fixed pitch and fixed aerodynamic_x000D_ characteristics leading to limited power and flight condition matching.
Drawbacks of the adjustable propellers available from the market:_x000D_ Low adjustment precision, complicated operation, requires large auxiliary_x000D_ tools, and cannot be quickly adjusted on-site.
T-MOTOR (New) manual adjustable variable-pitch series solution:_x000D_ Designed for complex and changing working conditions with diverse_x000D_ power demands, we provide flexible solutions that allow for quick manual_x000D_ pitch adjustment by simply changing the positioning blocks.
Quick Assembly and Disassembly_x000D_ Precise and Reliable
Quick to replace without requiring professional training—easy to learn_x000D_ and use. The pitch adjustment accuracy remains unaffected_x000D_ by manual operation errors with user-friendly operation.
??????,????00:0900:09
Methodical Approach
Using calculation tables derived from extensive experimental data,_x000D_ users can quickly find the required pitch angle based on the operating_x000D_ scenario and simple parameters.
(7.5°, 10°, and other positioning blocks are available upon request for customization.)
Performance Comparison
The efficiency curve of three positioning blocks (pitches) under_x000D_ different airflow speeds
(Example: MN605 KV170 + FLAME 180A 12S V2.0 + MF2211VP, Flight inclination 30°,_x000D_ S0, S5, S10, S15 respectively represents speed 0m/s, 5m/s, 10m/s, 15m/s,_x000D_ D0, D2.5, D5 respectively represents 0° positioning block, 2.5° positioning block, and 5° positioning block.)
Conclusion: As the positioning block angle (pitch) increases, the efficiency of the propeller improves at_x000D_ higher airflow speeds.
Multi-adaptability
The manual variable pitch propellers can not only support multi-rotor aircraft, but also effectively adapt to_x000D_ the needs of vertical take-off and landing aircraft,_x000D_ providing higher flexibility and performance to meet the requirements_x000D_ of different flight missions.
Multirotor
VTOL
Prototype Propellers Customization
Standard Customization
MOQ 1, with pitch angle customizable to 0.01°.
Assisted Customization
For mass production, engineers assist in determining the angle,_x000D_ and the customized pitch angle can be fixed before leaving the factory.
_x000D_ _x000D__x000D__x000D__x000D_ Technical Drawing_x000D__x000D_
_x000D__x000D__x000D__x000D_ Specification_x000D__x000D_
Model NO.
MF2614VP
T-MOTOR Series
Folding
Weight(Single Blade)
142.6g
Package Weight
457.6g
Diameter
26.4inch(670.56mm)
Package Size
334*134*61mm
Pitch
9.4inch(238.76mm)
Material
Polymer+CF
RecommendedThrust
3~8kg
RecommendedMax Thrust
18.5kg
Ambient Temp
-40?~65?
StorageTemp/Humidity
-10?~50?/<85%
Recommendation
Recommended ESC
FLAME 180A 12S V2.0
Recommended Motor
MN805S KV170/KV150
_x000D__x000D__x000D__x000D__x000D_ Test Data_x000D__x000D_
MN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (0°)
10%
48
247
0.09
0.44
708
7
11.69
104 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
48
596
0.20
1.02
1080
23
12.20
20%
48
1070
0.34
1.89
1433
51
11.81
25%
48
1615
0.51
3.05
1750
93
11.05
30%
48
2280
0.72
4.68
2070
156
10.16
35%
48
3016
0.93
6.61
2370
231
9.53
40%
48
3803
1.17
9.01
2660
326
8.83
45%
48
4674
1.44
11.93
2950
445
8.21
50%
48
5879
1.84
16.81
3317
639
7.35
55%
47
7089
2.16
22.41
3646
825
6.67
60%
47
8326
2.50
27.96
3937
1031
6.30
65%
47
9308
2.79
32.91
4183
1222
6.00
70%
47
11002
3.30
43.62
4573
1580
5.38
75%
47
12203
3.65
51.00
4829
1846
5.13
80%
46
13339
3.97
58.58
5054
2101
4.91
85%
46
14389
4.28
66.10
5265
2360
4.71
90%
46
15402
4.57
74.12
5471
2618
4.52
95%
46
16489
4.87
83.41
5686
2900
4.32
100%
45
17376
5.12
91.69
5875
3150
4.17
MN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (+2.5°)
10%
48
300
0.11
0.49
704
8
12.70
157 (Motor temperature after 2.5 minutes of operation) (Ambient Temperature:25?) (There is a risk of burnout)
15%
48
691
0.25
1.12
1066
28
12.85
20%
48
1228
0.44
2.12
1409
65
12.07
25%
48
1838
0.64
3.41
1714
115
11.25
30%
48
2592
0.89
5.40
2021
188
10.02
35%
48
3403
1.16
7.77
2307
280
9.16
40%
48
4290
1.46
10.69
2587
395
8.40
45%
48
5248
1.78
14.22
2858
533
7.75
50%
47
6673
2.27
20.67
3210
763
6.80
55%
47
8137
2.75
27.91
3533
1017
6.17
60%
47
9433
3.19
35.02
3800
1269
5.72
65%
47
10593
3.57
41.12
4006
1498
5.49
70%
47
12466
4.23
55.00
4344
1924
4.87
75%
46
13670
4.64
64.75
4547
2209
4.56
80%
46
14845
5.03
74.71
4728
2490
4.32
85%
46
15955
5.42
85.57
4898
2780
4.08
90%
45
17002
5.78
98.56
5054
3059
3.81
95%
45
17907
6.08
116.15
5182
3299
3.44
100%
44
18371
6.24
134.44
5241
3425
3.09
MN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (+5°)
10%
48
334
0.13
0.52
692
9
13.42
102 (Motor temperature after 1 minutes of operation) (Ambient Temperature:25?) (There is a risk of burnout)
15%
48
778
0.30
1.27
1048
33
12.71
20%
48
1395
0.54
2.45
1377
78
11.85
25%
48
2093
0.81
4.11
1673
142
10.63
30%
48
2922
1.11
6.37
1967
229
9.58
35%
48
3825
1.44
9.24
2218
335
8.66
40%
48
4822
1.82
12.80
2506
478
7.89
45%
48
5875
2.25
17.02
2763
651
7.25
50%
47
7412
2.78
24.71
3090
899
6.33
55%
47
8983
3.40
33.62
3386
1206
5.67
60%
47
10373
3.94
42.57
3630
1498
5.20
65%
47
11578
4.41
50.68
3822
1765
4.89
70%
46
12966
4.94
62.60
4033
2087
4.47
75%
46
14364
5.49
78.66
4232
2433
3.98
80%
45
15160
5.81
99.58
4337
2639
3.36
85%
45
14919
5.72
123.93
4304
2578
2.70
90%
44
14700
5.61
144.67
4270
2508
2.31
MN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (+7.5°)
10%
48
368
0.16
0.55
687
12
13.84
/ (Ambient Temperature:25?) (This angle is not recommended for static testing)
15%
48
857
0.36
1.38
1034
39
12.92
20%
48
1492
0.62
2.68
1349
88
11.62
25%
48
2260
0.93
4.60
1643
160
10.25
30%
48
3112
1.28
7.04
1920
257
9.24
35%
48
4080
1.68
10.43
2191
385
8.18
40%
48
5062
2.08
14.17
2439
531
7.49
45%
48
6223
2.55
19.22
2691
719
6.81
50%
47
7708
3.18
27.48
2988
995
5.93
55%
47
9314
3.85
37.88
3274
1320
5.23
60%
47
10683
4.44
47.34
3496
1625
4.83
65%
47
11812
4.92
56.42
3668
1890
4.50
70%
46
13054
5.44
69.84
3855
2196
4.05
75%
46
14093
5.90
88.11
4004
2474
3.51
80%
45
13754
5.77
116.68
3957
2391
2.63
85%
44
12845
5.32
145.42
3819
2128
2.01
MN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (+10°)
10%
48
356
0.20
0.60
674
14
12.39
/ (Ambient Temperature:25?) (This angle is not recommended for static testing)
15%
48
886
0.42
1.54
1019
45
11.97
20%
48
1539
0.72
2.96
1326
100
10.85
25%
48
2328
1.07
5.11
1613
181
9.50
30%
48
3196
1.46
7.89
1880
287
8.46
35%
48
4161
1.90
11.56
2141
426
7.54
40%
48
5220
2.38
15.65
2380
593
7.01
45%
47
6349
2.88
21.21
2619
790
6.30
50%
47
7834
3.60
30.72
2903
1094
5.40
55%
47
9372
4.30
41.80
3164
1425
4.78
60%
47
10672
4.91
52.63
3368
1732
4.35
65%
46
11742
5.42
63.34
3532
2004
4.00
70%
46
12765
5.92
78.92
3682
2283
3.53
75%
45
11920
5.49
117.64
3554
2043
2.26
MN805 KV170 + FLAME 180A 12S V2.0 + MF2614VP (-2.5°)
10%
48
218
0.07
0.43
716
5
10.63
72 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
48
519
0.16
0.96
1094
18
11.31
20%
48
914
0.28
1.70
1445
42
11.20
25%
48
1394
0.43
2.66
1782
80
10.92
30%
48
1994
0.58
4.07
2112
128
10.21
35%
48
2630
0.76
5.74
2426
193
9.57
40%
48
3319
0.96
7.74
2727
274
8.97
45%
48
4060
1.17
10.19
3027
371
8.34
50%
48
5135
1.46
14.47
3412
522
7.44
55%
48
6152
1.74
18.57
3746
683
6.97
60%
47
7147
2.02
23.06
4054
858
6.54
65%
47
8503
2.38
30.01
4415
1100
6.00
70%
47
9514
2.65
35.42
4755
1320
5.70
75%
47
10548
2.91
41.55
5043
1537
5.41
80%
47
11469
3.15
47.03
5313</
T-Motor MF Variable-Pitch Klapp Propeller 1x CW 1x CCW 30 Zoll - MF3016VP
Artikelnr.: PM-7079 | HAN: MF3016VP
MF VP SERIES PROPELLER
Manual Variable-Pitch Series
Simplicity Over Complexity, Consistency in Performance
Specially designed to address the issues of low flight efficiency at high speeds and high altitudes, this series is suitable for aircraft development and professional users requiring rapid switching across multiple scenarios.
Manual Variable-Pitch Series
Flexible and easy-to-use drone propulsion system enhances flight efficiency in various operating conditions.
Typical application scenarios include high-speed flight, high-altitude flight, adjustments for overall aircraft weight, and fine-tuning of custom propeller performance.
Limitations of Traditional Propellers: Fixed pitch and fixed aerodynamic characteristics leading to limited power and flight condition matching.
Drawbacks of the adjustable propellers available from the market: Low adjustment precision, complicated operation, requires large auxiliary tools, and cannot be quickly adjusted on-site.
T-MOTOR (New) manual adjustable variable-pitch series solution: Designed for complex and changing working conditions with diverse power demands, we provide flexible solutions that allow for quick manual pitch adjustment by simply changing the positioning blocks.
Quick Assembly and Disassembly Precise and Reliable
Quick to replace without requiring professional training—easy to learn and use. The pitch adjustment accuracy remains unaffected by manual operation errors with user-friendly operation.
Methodical Approach
Using calculation tables derived from extensive experimental data, users can quickly find the required pitch angle based on the operating scenario and simple parameters.
(7.5°, 10°, and other positioning blocks are available upon request for customization.)
Performance Comparison
The efficiency curve of three positioning blocks (pitches) under different airflow speeds
(Example: MN605 KV170 + FLAME 180A 12S V2.0 + MF2211VP, Flight inclination 30°, S0, S5, S10, S15 respectively represents speed 0m/s, 5m/s, 10m/s, 15m/s, D0, D2.5, D5 respectively represents 0° positioning block, 2.5° positioning block, and 5° positioning block.)
Conclusion: As the positioning block angle (pitch) increases, the efficiency of the propeller improves at higher airflow speeds.
Multi-adaptability
The manual variable pitch propellers can not only support multi-rotor aircraft, but also effectively adapt to the needs of vertical take-off and landing aircraft, providing higher flexibility and performance to meet the requirements of different flight missions.
Multirotor
VTOL
Prototype Propellers Customization
Standard Customization
MOQ 1, with pitch angle customizable to 0.01°.
Assisted Customization
For mass production, engineers assist in determining the angle, and the customized pitch angle can be fixed before leaving the factory.
Technical Drawing
Specification
Model NO.
MF3016VP
T-MOTOR Series
Folding
Weight(Single Blade)
190g
Package Weight
640g
Diameter
30.4inch(772.16mm)
Package Size
400*190*70mm
Pitch
10.9inch(276.86mm)
Material
Polymer+CF
Recommended Thrust
4~12kg
RecommendedMax Thrust
20kg
Ambient Temp
-40?~65?
Storage Temp/Humidity
-10?~50?/<85%
Recommendation
Recommended ESC
FLAME 180A 12S V2.0
Recommended Motor
MN1010/P80ll/U12ll/U13ll
Test Data
P80III KV120 + FLAME 180A 12S V2.0 + MF3016VP (0°)
10%
48
242
0.10
0.41
559
6
12.26
85 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
48
598
0.23
0.93
853
21
13.43
20%
48
1077
0.41
1.69
1125
48
13.29
25%
48
1619
0.59
2.71
1374
85
12.45
30%
48
2291
0.82
4.12
1622
139
11.60
35%
48
3005
1.08
5.93
1854
210
10.58
40%
48
3817
1.34
8.03
2075
291
9.93
45%
48
4723
1.64
10.61
2305
396
9.32
50%
48
5876
2.04
14.88
2556
546
8.29
55%
48
7143
2.49
20.06
2822
736
7.50
60%
47
8756
3.03
26.87
3121
990
6.89
65%
47
9854
3.40
31.72
3305
1177
6.58
70%
47
11075
3.82
37.90
3501
1400
6.21
75%
47
12284
4.21
44.44
3691
1627
5.90
80%
47
13408
4.62
50.92
3860
1867
5.64
85%
47
14450
4.96
57.42
4015
2085
5.41
90%
46
15550
5.31
64.76
4173
2320
5.19
95%
46
16632
5.67
72.30
4328
2570
4.99
100%
46
17590
6.00
79.43
4462
2804
4.83
P80III KV120 + FLAME 180A 12S V2.0 + MF3016VP (+2.5°)
10%
48
279
0.12
0.44
553
7
13.31
132 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?) (There is a risk of burnout)
15%
48
685
0.28
1.02
842
25
13.98
20%
48
1203
0.48
1.87
1100
55
13.37
25%
48
1828
0.72
3.08
1346
101
12.37
30%
48
2562
0.99
4.75
1579
164
11.24
35%
48
3364
1.30
6.69
1806
246
10.51
40%
48
4270
1.63
9.38
2023
345
9.52
45%
48
5228
1.99
12.41
2232
465
8.82
50%
48
6510
2.47
17.45
2478
641
7.83
55%
47
7838
2.97
22.85
2710
843
7.23
60%
47
9717
3.68
32.09
3005
1158
6.41
65%
47
10858
4.12
37.92
3171
1368
6.08
70%
47
12151
4.60
45.09
3347
1612
5.75
75%
47
13419
5.05
52.78
3509
1856
5.45
80%
46
14588
5.49
60.39
3656
2102
5.20
85%
46
15704
5.92
68.04
3787
2348
5.00
90%
46
16878
6.37
77.47
3920
2615
4.74
95%
46
18044
6.80
87.19
4042
2878
4.53
100%
45
19006
7.18
96.03
4150
3120
4.36
P80III KV120 + FLAME 180A 12S V2.0 + MF3016VP (+5°)
10%
48
329
0.15
0.46
547
9
14.88
77 (Motor temperature after 1 minutes of operation) (Ambient Temperature:25?) (There is a risk of burnout)
15%
48
803
0.35
1.13
828
30
14.85
20%
48
1368
0.60
2.12
1078
-68
13.42
25%
48
2086
0.90
3.56
1312
124
12.21
30%
48
2864
1.22
5.47
1534
196
10.92
35%
48
3764
1.60
8.01
1749
293
9.82
40%
48
4719
1.99
10.90
1950
406
9.06
45%
48
5773
2.45
14.65
2149
551
8.26
50%
48
7129
3.03
20.43
2377
754
7.34
55%
47
8643
3.66
27.59
2604
998
6.62
60%
47
9951
4.23
34.53
2782
1232
6.11
65%
47
11736
4.98
45.88
3007
1568
5.47
70%
47
12993
5.52
54.35
3153
1822
5.13
75%
46
14125
6.02
63.05
3281
2068
4.84
80%
46
15287
6.53
73.05
3406
2329
4.54
85%
46
16266
6.97
82.38
3506
2559
4.31
90%
45
17331
7.40
93.96
3606
2794
4.06
95%
45
18164
7.78
104.64
3691
3007
3.84
100%
45
18908
8.12
116.20
3762
3199
3.63
P80III KV120 + FLAME 180A 12S V2.0 + MF3016VP (+7.5°)
10%
48
326
0.18
0.50
541
10
13.45
112 (Motor temperature after 1 minutes of operation) (Ambient Temperature:25?) (There is a risk of burnout)
15%
48
825
0.40
1.27
807
34
13.51
20%
48
1470
0.71
2.41
1058
79
12.70
25%
48
2209
1.04
4.00
1276
139
11.50
30%
48
3067
1.43
6.29
1495
224
10.18
35%
48
4002
1.87
9.11
1698
333
9.18
40%
48
5010
2.33
12.45
1890
461
8.43
45%
48
6145
2.85
16.69
2076
620
7.73
50%
47
7525
3.49
23.14
2280
833
6.85
55%
47
9064
4.21
31.46
2498
1101
6.10
60%
47
10313
4.81
38.69
2659
1339
5.67
65%
47
11663
5.43
48.70
2818
1602
5.12
70%
46
13172
6.16
62.03
2986
1926
4.58
75%
46
14216
6.65
72.88
3093
2154
4.23
80%
46
15160
7.10
83.55
3186
2369
3.97
85%
45
15930
7.48
94.64
3258
2552
3.70
90%
45
16543
7.80
106.88
3315
2708
3.43
95%
45
16991
8.03
118.83
3359
2824
3.20
100%
44
17414
8.23
130.37
3400
2930
3.01
P80III KV120 + FLAME 180A 12S V2.0 + MF3016VP (+10°)
10%
48
379
0.22
0.56
528
12
14.01
/ (Ambient Temperature:25?) (This angle is not recommended for static testing)
15%
48
916
0.50
1.41
799
42
13.48
20%
48
1574
0.83
2.74
1032
90
11.97
25%
48
2362
1.23
4.60
1249
161
10.71
30%
48
3235
1.66
7.04
1452
252
9.60
35%
48
4196
2.18
10.22
1648
376
8.59
40%
48
5224
2.70
14.05
1830
517
7.80
45%
48
6352
3.28
18.76
2008
690
7.12
50%
47
7773
4.03
26.02
2204
930
6.31
55%
47
9236
4.80
34.95
2396
1204
5.61
60%
47
10503
5.47
43.61
2552
1462
5.14
65%
47
11561
6.05
51.68
2675
1695
4.80
70%
46
12765
6.71
65.42
2807
1972
4.22
75%
46
13552
7.14
82.15
2889
2160
3.60
80%
45
14065
7.41
96.62
2938
2280
3.21
85%
45
14420
7.59
108.28
2971
2362
2.96
90%
45
14639
7.70
120.47
2990
2411
2.72
95%
44
14846
7.81
131.39
3010
2462
2.55
100%
44
15183
7.99
141.30
3042
2545
2.44
P80III KV120 + FLAME 180A 12S V2.0 + MF3016VP (-2.5°)
10%
48
266
0.09
0.39
566
5
14.23
64 (Motor temperature after 3 minutes of operation) (Ambient Temperature:25?)
15%
48
583
0.20
0.87
865
18
13.98
20%
48
990
0.34
1.54
1137
40
13.38
25%
48
1504
0.52
2.45
1398
76
12.81
30%
48
2075
0.71
3.66
1648
123
11.82
35%
48
2750
0.92
5.26
1897
183
10.91
40%
48
3437
1.15
7.06
2122
256
10.17
45%
48
4212
1.40
9.30
2354
345
9.48
50%
48
5237
1.73
12.82
2626
476
8.56
55%
48
6567
2.17
18.22
2959
672
7.58
60%
47
7754
2.54
22.81
3224
857
7.16
65%
47
8700
2.83
26.97
3422
1014
6.82
70%
47
9818
3.16
31.87
3637
1204
6.53
75%
47
10843
3.49
37.33
3847
1406
6.17
80%
47
11852
3.79
42.69
4048
1607
5.92
85%
47
12713
4.02
47.28
4220
1776
5.75
90%
47
13677
4.30
53.12
4410
1986
5.52
95%
46
14565
4.56
58.76
4615
2204
5.34
100%
46
15299
4.77
63.53
4762
2379
5.20
Note:Motortemperatureisthebelltemperatureat80%throttle. (Date above based on benchtest are for reference only, comparion with that of other motor types is not recommended.)
<
Last updated