Overview
MAD M50C35 PRO IPE adalah motor drone berawak yang direka sebagai penyelesaian pendorongan berkuasa tinggi untuk drone berawak dan platform UAV ultra-berat, dengan sokongan untuk sistem voltan 12S dan 24S.
| Pendorongan berterusan |
30~45kg |
| Pendorongan maksimum |
113.7kg |
| Sokongan voltan |
12S,24S |
| Berat |
4300g |
Ciri Utama
- Pendorongan yang dinilai: 30–40 kgf
- Pendorongan puncak: 92.6 kgf
- Output berterusan: 25 kW
- Berat motor: 4360g
- Menyokong sistem voltan 12–24S
Untuk pengesahan konfigurasi dan sokongan teknikal (padanan ESC/prop), hubungi support@rcdrone.top or lawati https://rcdrone.top/.
Spesifikasi
Data Motor
| Model Motor |
MAD M50C35 IPE V1.0 |
Bilangan pasangan tiang |
31 |
| Stator |
Antikorosif |
Gred wayar berlakur |
220°C |
| Saiz Motor |
D:191 × 94 mm |
Gred Magnet |
180°C |
| Gred Perlindungan |
IP35 |
Panjang Kabel |
150 mm (kabel berlakur yang dilanjutkan) |
| Pelepasan Haba Sentifugal |
YA |
Keseimbangan Rotor |
≤20 mg |
| Lubang Pemasangan Propeller |
D:50 M6×6 |
Keseimbangan Motor |
≤30 mg |
| Diameter Shaft |
IN: 25 mm |
Lubang Pemasangan Motor |
D:80 M6×6 |
| Galas |
NSK 6818ZZCM |
Ujian gangguan |
1000 V |
Pelan dan Lubang Pemasangan
| Lubang pemasangan motor |
Ø80-M6×6 |
| Lubang pemasangan propeller |
Ø50-M6×6 |
| Diameter luar motor |
Ø191 |
| Dimensi pandangan sisi |
83 |
| Dimensi langkah/offset |
11 |
| Diameter boss/ciri |
Ø90 |
| Poros |
Ø25, 35 |
| Nota corak lubang |
Ø50-Ø6.2×6 |
9KV (Edisi Profesional Industri)
- Daya angkat yang disyorkan: 30~40 kgf
- Daya maksimum: 92.6 kgf
- Berat yang dioptimumkan: 4360 g
- Kecekapan: >78%
- Header ujian: MAD M50C35 IPE 9KV + FLUXER PRO 63x22 GLOSSY + FOC IGBT 60A (80-440V)
- Label: 400V, MAX 128°C
| RPM/V |
9 KV |
Voltan Nominal |
100S bateri lipo |
| Arus Tanpa Beban |
0.92A/30V |
Rintangan dalaman |
58.8mΩ |
| Berat Motor |
4360 g |
Berat Kotak Produk |
5910g (330 x 265 x 135 mm) |
| Arus Maksimum |
49.1 A |
Kuasa Maksimum |
19494W |
| Daya angkat maksimum |
92.6 kg |
Tork Maksimum |
63.9 Nm |
| ESC Disyorkan |
FOC IGBT 60A (80-440V) |
Propeller Disyorkan |
63x22 |
| Berat lepas landas UAV |
24S-63"/ 140kg--Quadcopter 210kg--Hexacopter 280kg--Octocopter |
Berat lepas landas rotor tunggal |
30kg ~ 40kg |
Jadual Prestasi 9KV (400V)
| Throttle [%] |
Voltan [V] |
Arus [A] |
Kuasa Masukan [W] |
Kuasa Keluaran [W] |
Tork [N*m] |
RPM |
Thrust [kgf] |
Kecekapan [%] |
Kecekapan [gf/W] |
| 30 |
398 |
2.74 |
1090.0 |
696.7 |
7.930 |
839 |
11 |
63.92 |
10.5 |
| 35 |
398 |
3.7 |
1472.0 |
1117.6 |
10.880 |
981 |
16 |
75.93 |
10.7 |
| 40 |
398 |
5.85 |
2328.0 |
1730.3 |
14.820 |
1115 |
21 |
74.33 |
8.8 |
| 45 |
398 |
8.09 |
3219.0 |
2360.2 |
18.090 |
1246 |
26 |
73.32 |
8.0 |
| 50 |
398 |
10.23 |
4071.0 |
3107.0 |
21.690 |
1368 |
31 |
76.32 |
7.7 |
| 55 |
398 |
12.7 |
5052.0 |
3993.6 |
25.700 |
1484 |
37 |
79.05 |
7.3 |
| 60 |
398 |
15.38 |
6114.0 |
4991.2 |
29.810 |
1599 |
43 |
81.64 |
7.1 |
| 65 |
398 |
18.79 |
7471.0 |
6168.2 |
34.590 |
1703 |
48 |
82.56 |
6.5 |
| 70 |
398 |
22.56 |
8968.0 |
7369.9 |
38.950 |
1807 |
56 |
82.18 |
6.2 |
| 75 |
398 |
25.18 |
9986.0 |
8364.9 |
42.200 |
1893 |
59 |
83.77 |
5.9 |
| 80 |
397 |
29.22 |
11586.0 |
10498.4 |
49.930 |
2008 |
68 |
90.61 |
5.8 |
| 85 |
397 |
34.95 |
13861.0 |
11991.3 |
54.480 |
2102 |
75 |
86.51 |
5.4 |
| 90 |
396 |
40.04 |
15868.0 |
13572.0 |
59.130 |
2192 |
81 |
85.53 |
5.1 |
| 95 |
397 |
48.14 |
19102.0 |
15072.8 |
63.440 |
2269 |
89 |
78.91 |
4.6 |
| 100 |
397 |
49.14 |
19494.0 |
15334.1 |
63.920 |
2291 |
93 |
78.66 |
4.8 |
34KV (Edisi Profesional Industri)
- Daya angkat yang disyorkan: 35~45 kgf
- Daya maksimum: 113.7 kgf
- Berat yang dioptimumkan: 4365 g
- Kecekapan: >83%
- Header ujian: MAD M50C35 IPE 34KV + FLUXER PRO 63x22 GLOSSY + AMPX 300A (12-24S)
- Label: 24S
| RPM/V |
34 KV |
Voltan Nominal |
24S bateri lipo |
| Arus Tanpa Beban |
3.7A / 30V |
Rintangan dalaman |
14.7mΩ |
| Berat Motor |
4365 g |
Berat Kotak Produk |
5915g (330 x 265 x 135 mm) |
| Arus Maksimum |
251.5 A |
Kuasa Maksimum |
24987W |
| Daya angkat maksimum |
113.7 kg |
Tork Maksimum |
78.4 Nm |
| ESC Disyorkan |
MAD AMPX 300A (12-24S) |
Propeller Disyorkan |
63x22 |
| Berat lepas landas UAV |
24S-63"/ 160kg--Quadcopter 240kg--Hexacopter 320kg--Octocopter |
Berat lepas landas rotor tunggal |
35kg ~ 45kg |
Jadual Prestasi 34KV (24S)
| Throttle [%] |
Voltan [V] |
Arus [A] |
Kuasa Masukan [W] |
Kuasa Keluaran [W] |
Tork [N*m] |
RPM |
Thrust [gf] |
Kecekapan [%] |
Kecekapan [gf/W] |
| 30 |
100.6 |
10.63 |
1069.4 |
855.5 |
8.841 |
924 |
13360 |
80.00 |
12.5 |
| 35 |
100.54 |
15.2 |
1528.2 |
1246.2 |
11.259 |
1057 |
17031 |
81.50 |
11.1 |
| 40 |
100.78 |
21.82 |
2199.0 |
1775.0 |
14.232 |
1191 |
22773 |
80.70 |
10.4 |
| 45 |
100.61 |
30.57 |
3075.6 |
2511.5 |
17.858 |
1343 |
28863 |
81.70 |
9.4 |
| 50 |
100.46 |
42 |
4219.3 |
3534.7 |
22.608 |
1493 |
35262 |
83.80 |
8.4 |
| 55 |
100.58 |
54.55 |
5486.6 |
4706.2 |
27.554 |
1631 |
42642 |
85.80 |
7.8 |
| 60 |
100.56 |
68.22 |
6860.2 |
5919.3 |
32.374 |
1746 |
49381 |
86.30 |
7.2 |
| 65 |
100.52 |
83.9 |
8433.6 |
7198.8 |
36.761 |
1870 |
56551 |
85.40 |
6.7 |
| 70 |
100.4 |
102.19 |
10259.9 |
8889.7 |
42.723 |
1987 |
63961 |
86.60 |
6.2 |
| 75 |
100.27 |
122.51 |
12284.1 |
10566.1 |
48.070 |
2099 |
72525 |
86.00 |
5.9 |
| 80 |
100.2 |
147.52 |
14781.5 |
12591.8 |
54.532 |
2205 |
80002 |
85.20 |
5.4 |
| 85 |
100.08 |
171.25 |
17138.7 |
14472.0 |
59.414 |
2326 |
87814 |
84.40 |
5.1 |
| 90 |
99.9 |
203.99 |
20378.6 |
16845.9 |
66.584 |
2416 |
96733 |
82.70 |
4.7 |
| 95 |
99.58 |
232.09 |
23111.5 |
18677.9 |
71.430 |
2497 |
106740 |
80.80 |
4.6 |
| 100 |
99.36 |
251.48 |
24987.1 |
20739.3 |
78.409 |
2526 |
113654 |
83.00 |
4.5 |
40KV (Edisi Profesional Industri)
- Thrust hover yang disyorkan: 30~40 kgf
- Thrust maksimum: 90.9 kgf
- Berat yang dioptimumkan: 4337 g
- Kecekapan: >82%
- Header ujian: MAD M50C35 IPE 40KV + PROP CB2 60x20 MATT + AMPX 300A (12-24S)
- Label: 24S, MAX 140°C
| RPM/V |
40 KV |
Voltan Nominal |
24S bateri lipo |
| Arus Tanpa Beban |
3.6A/20V |
Rintangan dalaman |
10mΩ |
| Berat Motor |
4337 g |
Berat Kotak Produk |
5887g (330 x 265 x 135 mm) |
| Arus Maksimum |
216.6 A |
Kuasa Maksimum |
20967W |
| Thrust maksimum |
90.9 kg |
Tork Maksimum |
52.1 Nm |
| ESC Disyorkan |
MAD AMPX 300A (12-24S) |
Propeller Disyorkan |
57x19, 60x20 |
| Berat lepas UAV |
24S-60"/ 140kg--Quadcopter 210kg--Hexacopter 280kg--Octocopter |
Berat lepas rotor tunggal |
30kg ~ 40kg |
Jadual Prestasi 40KV (CB2 PROP 57x19 MATT, 24S, MAX 130°C)
| Throttle [%] |
Voltan [V] |
Arus [A] |
Kuasa Masukan [W] |
Kuasa Keluaran [W] |
Tork [N*m] |
RPM |
Thrust [gf] |
Kecekapan [%] |
Kecekapan [gf/W] |
| 30 |
98.66 |
12.3 |
1213.5 |
910.8 |
8.091 |
1075 |
12865 |
75.10 |
10.6 |
| 35 |
98.68 |
18.03 |
1779.2 |
1361.3 |
10.569 |
1230 |
16662 |
76.50 |
9.4 |
| 40 |
98.54 |
25.34 |
2497.0 |
1991.0 |
13.688 |
1389 |
21496 |
79.70 |
8.6 |
| 45 |
98.53 |
36.78 |
3623.9 |
2921.9 |
17.637 |
1582 |
27746 |
80.60 |
7.7 |
| 50 |
98.37 |
49.01 |
4821.1 |
3998.3 |
21.830 |
1749 |
34236 |
82.90 |
7.1 |
| 55 |
98.3 |
63.68 |
6259.7 |
5276.9 |
26.482 |
1903 |
40549 |
84.30 |
6.5 |
| 60 |
98.17 |
77.5 |
7608.2 |
6398.5 |
29.851 |
2047 |
46604 |
84.10 |
6.1 |
| 65 |
98.17 |
98.03 |
9623.6 |
7949.1 |
34.791 |
2182 |
53790 |
82.60 |
5.6 |
| 70 |
98.01 |
118.31 |
11595.6 |
9438.8 |
38.938 |
2315 |
61280 |
81.40 |
5.3 |
| 75 |
97.92 |
140.81 |
13788.1 |
11195.9 |
43.606 |
2452 |
68220 |
81.20 |
4.9 |
| 80 |
97.94 |
164.23 |
16084.7 |
12996.4 |
48.407 |
2564 |
74006 |
80.80 |
4.6 |
| 85 |
97.83 |
195.21 |
19097.4 |
15201.5 |
54.069 |
2685 |
81462 |
79.60 |
4.3 |
| 90 |
98.12 |
229.66 |
22534.2 |
17847.1 |
60.871 |
2800 |
85765 |
79.20 |
3.8 |
Jadual Prestasi 40KV (CB2 PROP 60x20 MATT, 24S, MAX 140°C)
| Throttle [%] |
Voltan [V] |
Arus [A] |
Kuasa Masukan [W] |
Kuasa Keluaran [W] |
Tork [N*m] |
RPM |
Dorongan [gf] |
Kecekapan [%] |
Kecekapan [gf/W] |
| 30 |
98.47 |
12.4 |
1221.0 |
895.0 |
7.117 |
1201 |
14430 |
73.30 |
11.8 |
| 35 |
98.46 |
19.2 |
1890.4 |
1414.0 |
10.040 |
1345 |
18964 |
74.80 |
10.0 |
| 40 |
98.33 |
26.8 |
2635.2 |
1976.4 |
12.592 |
1499 |
22645 |
75.00 |
8.6 |
| 45 |
98.33 |
35.8 |
3520.2 |
2678.9 |
15.571 |
1643 |
27640 |
76.10 |
7.9 |
| 50 |
98.43 |
47.4 |
4665.6 |
3601.8 |
19.270 |
1785 |
33945 |
77.20 |
7.3 |
| 55 |
98.35 |
59.8 |
5881.3 |
4593.3 |
23.075 |
1901 |
39362 |
78.10 |
6.7 |
| 60 |
98.26 |
73.1 |
7182.8 |
5753.4 |
31.419 |
2024 |
45693 |
80.10 |
6.4 |
| 65 |
98.43 |
86.5 |
8514.2 |
6777.3 |
32.284 |
2123 |
51637 |
79.60 |
6.1 |
| 70 |
98.42 |
100.8 |
9920.7 |
7847.3 |
33.471 |
2239 |
56700 |
79.10 |
5.7 |
| 75 |
98.49 |
118.4 |
11661.2 |
9200.7 |
37.012 |
2374 |
62129 |
78.90 |
5.3 |
| 80 |
98.47 |
131 |
12899.6 |
10100.4 |
39.211 |
2460 |
67134 |
78.30 |
5.2 |
| 85 |
98.37 |
148.6 |
14617.8 |
11416.5 |
42.112 |
2589 |
72374 |
78.10 |
5.0 |
| 90 |
96.56 |
169.7 |
16386.2 |
12699.3 |
44.935 |
2699 |
78315 |
77.50 |
4.8 |
| 95 |
97.35 |
193 |
18788.6 |
14523.5 |
48.976 |
2832 |
86016 |
77.30 |
4.6 |
| 100 |
96.8 |
216.6 |
20966.9 |
16102.6 |
52.129 |
2950 |
90890 |
76.80 |
4.3 |
Konfigurasi Disyorkan
- 34KV ESC Disyorkan: AMPX 300A (12-24S); propeller: CB2 prop 63X22" inci propeller serat karbon.
- 40KV ESC Disyorkan: AMPX 300A (12-24S); propeller: CB2 57X19. Alternatif: AMPX 200A (12-24S) dengan propeller: fluxer pro 60X20.
- 59KV FOC combo Disyorkan: set lengan drone HB40-63X22; set lengan drone HB40-64x20; set lengan drone HB40-60X19; set lengan drone HB40-57X19.
Apa yang Termasuk
- Motor x1
- Papan Propeller x1
- Paku Lokasi x1
- 8.0mm Penyambung Bullet x3
- Tiub Panas Mengecut x3
- Skru Motor M6*25 x6
- Skru Penyesuai Prop M6*45 x6
- Skru Propeller M6*60 x6
- Pelekat x2
Permohonan
- Sistem pendorong drone berawak
- Pesawat eVTOL, UAV kargo, dan platform paramotor elektrik
- Projek yang memerlukan kombinasi ESC + prop yang disahkan untuk konfigurasi daya tinggi
Butiran

MAD Lukisan motor M50C35 PRO IPE menunjukkan dimensi keseluruhan dan susun atur lubang pemasangan untuk membantu merancang pemasangan dan instalasi.

Pakej motor MAD M50C35 PRO IPE termasuk plat propeller, pin lokasi, penyambung bullet 8.0mm, tiub panas mengecut, skru pemasangan, dan pelekat untuk pemasangan.

Data prestasi motor MAD M50C35 termasuk penilaian 9kW pada 400V, dengan angka daya penggerak dan kecekapan serta jadual spesifikasi terperinci.

Jadual spesifikasi motor MAD M50C35 menyenaraikan persediaan 24S dengan data kecekapan dan daya penggerak, termasuk sehingga 113.7 kgf daya penggerak maksimum.

Jadual spesifikasi motor drone M50C35 40KV menyenaraikan angka utama seperti julat 30–40 kgf, berat 433.7 g, dan sehingga 82% kecekapan bersama dengan lengkung prestasi dan jadual.