Overview
The Hobbywing XRotor V9626 IPC 12S VTOL motor (V9626 160KV / HV-9626-160KV) is designed for VTOL rotor power series applications and supports Intelligent Propeller Control (IPC). Key rated and maximum performance figures include max power of 9340W and max thrust of 38.5kg.
For compatibility checks (propellers, ESC, wiring), contact support@rcdrone.top or visit https://rcdrone.top/.
Key Features
- Intelligent Propeller Control (IPC): low power consumption with precision positioning; propeller stop positioning can reduce cruising resistance and improve flight time when used with a Hobbywing ESC; standardized installation interface.
- Optimized magnetic circuit design for improved performance, supporting high torque and strong burst power.
- Stator process: high standard silicon steel sheet, rust proof, with 180°C high temperature resistance paint-coat.
- Enamelled wire temperature rating: 200°C; magnet temperature rating: 180°C.
- Isolation test: 500V AC high voltage resistance test.
- Protection level: IP5; bearing: water proof bearing.
- Dynamic balance: ≤15mg.
- High-load figures shown: motor weight 975g; thrust-to-weight ratio up to 39:1; suitable for VTOL take-off weight of 65kg (conventional four-rotor VTOL layout).
- Maximum thrust test note: 38.5kg (tested with MSC 32x10.5 propellers under 46V at full throttle in the laboratory).
Specifications
| Model | V9626 160KV |
| Series / Marking | V9626 160KV; HV-9626-160KV |
| Motor size | Φ104.5*H64.2mm |
| Stator size | Φ96mm |
| Slot & pole | 36N 42P |
| KV | 160 |
| Battery (LiPo) | 12S LiPo |
| No-load current | 9.45A |
| Maximum current (Non-hermetic, ambient temperature ≤ 25°C) | 171.5A |
| Resistance | 8.95mΩ |
| Max power | 9340W |
| Max thrust | 38.5kg |
| Rated power input | 2500W |
| Rated power output | 2125W |
| Weight (with wire) | 975g |
| Wire size | enamelled wire outlet |
| Wire length | 150 mm |
| Motor axle diameter | Φ10mm |
| Props mounting dimensions | 4×M3@D20mm + 4×M4@D23mm |
| Motor mounting dimensions | 4×M5@D50mm |
| Protection level | IP5 |
| Bearing | Water proof bearing |
| Dynamic balance | ≤15mg |
| Stator process | High standard silicon steel sheet, rust proof, 180°C high temperature resistance paint-coat |
| Enamelled wire | 200°C |
| Magnet | 180°C |
| Isolation test | 500V AC high voltage resistance test |
| Thrust-to-weight ratio (shown) | 39:1 |
| VTOL take-off weight (shown) | 65kg (conventional four-rotor VTOL layout) |
| CAD reference dimensions (shown) | 64.20 mm; 58.20 mm; 55.20 mm; 65 mm; Φ30; Φ20; 4-Φ6; 4-Φ3.20 |
Applications
- VTOL rotor power series motors
- Drone application scenarios (shown)
Recommended application combinations (provided)
- Motor: V9626 160KV
- Propeller: MSC 30x9.8 / MSC 32x10.5 (also provided: MFP 30x9.8 / MFP 32x10.5)
- ESC: XRotor Pro-H200A-14S-BLDC-IPC (also provided: XRotor Pro H200A 14S BLDC IPC)
- Battery: 12S LiPo
- Thrust/rotor: 12~16kg
- Takeoff weight of quadrotor: 50~64kg
Performance
V9626 160KV + MFP 30x9.8 Load performance parameters

V9626 160KV + MFP 30x9.8 Motor Propeller Pull Test Data
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|---|
|
46V (12S LiPo) |
MFP 30x9.8 |
33% |
4578 |
11.2 |
514.0 |
2349 |
8.9 |
1.25 |
436.9 |
83.2°C |
|
35% |
5109 |
12.7 |
585.2 |
2479 |
8.7 |
1.41 |
497.4 |
|||
|
37% |
5667 |
14.4 |
663.9 |
2608 |
8.5 |
1.59 |
564.3 |
|||
|
39% |
6250 |
16.3 |
750.0 |
2735 |
8.3 |
1.77 |
637.5 |
|||
|
42% |
7163 |
19.4 |
892.6 |
2921 |
8.0 |
2.05 |
758.7 |
|||
|
45% |
8119 |
22.8 |
1051.1 |
3100 |
7.7 |
2.34 |
893.4 |
|||
|
48% |
9113 |
26.6 |
1225.1 |
3273 |
7.4 |
2.64 |
1041.3 |
|||
|
51% |
10145 |
30.7 |
1414.6 |
3440 |
7.2 |
2.96 |
1202.4 |
|||
|
54% |
11213 |
35.2 |
1619.9 |
3602 |
6.9 |
3.28 |
1376.9 |
|||
|
57% |
12318 |
40.0 |
1841.8 |
3761 |
6.7 |
3.62 |
1565.5 |
|||
|
60% |
13464 |
45.2 |
2081.4 |
3917 |
6.5 |
3.97 |
1769.2 |
|||
|
63% |
14652 |
50.9 |
2340.2 |
4072 |
6.3 |
4.33 |
1989.1 |
|||
|
66% |
15885 |
56.9 |
2620.1 |
4226 |
6.1 |
4.71 |
2227.1 |
|||
|
69% |
17166 |
63.5 |
2923.4 |
4381 |
5.9 |
5.11 |
2484.9 |
|||
|
72% |
18498 |
70.7 |
3252.9 |
4535 |
5.7 |
5.53 |
2764.9 |
|||
|
75% |
19884 |
78.5 |
3611.1 |
4689 |
5.5 |
5.98 |
3069.5 |
|||
|
78% |
21324 |
86.9 |
4001.1 |
4842 |
5.3 |
6.45 |
3401.0 |
|||
|
81% |
22818 |
96.2 |
4425.5 |
4992 |
5.2 |
6.94 |
3761.7 |
|||
|
84% |
24366 |
106.2 |
4886.4 |
5138 |
5.0 |
7.47 |
4153.4 |
|||
|
87% |
25962 |
117.0 |
5384.6 |
5279 |
4.8 |
8.02 |
4576.9 |
|||
|
90% |
27603 |
128.6 |
5919.7 |
5414 |
4.7 |
8.59 |
5031.7 |
|||
|
100% |
32977 |
169.5 |
7800.5 |
5828 |
4.2 |
10.46 |
6630.4 |
V9626 160KV + MFP 32x10.5Load performance parameters

V9626 160KV + MFP 32x10.5Motor Propeller Pull Test Data
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Speed(RPM) |
Efficiency(g/W) |
Torque(N·m) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|---|
|
46V (12S LiPo) |
MFP 32x10.5 |
33% |
5823 |
13.9 |
638.1 |
2286 |
9.1 |
1.75 |
542.4 |
87.1°C |
|
35% |
6480 |
15.8 |
725.4 |
2406 |
8.9 |
1.96 |
616.6 |
|||
|
37% |
7171 |
17.9 |
823.6 |
2526 |
8.7 |
2.18 |
700.1 |
|||
|
39% |
7889 |
20.3 |
932.3 |
2646 |
8.5 |
2.41 |
792.5 |
|||
|
42% |
9009 |
24.2 |
1113.8 |
2821 |
8.1 |
2.77 |
946.7 |
|||
|
45% |
10170 |
28.6 |
1315.9 |
2992 |
7.7 |
3.14 |
1118.5 |
|||
|
48% |
11365 |
33.4 |
1536.9 |
3157 |
7.4 |
3.53 |
1306.3 |
|||
|
51% |
12589 |
38.6 |
1775.8 |
3317 |
7.1 |
3.92 |
1509.4 |
|||
|
54% |
13841 |
44.2 |
2032.2 |
3472 |
6.8 |
4.32 |
1727.4 |
|||
|
57% |
15123 |
50.1 |
2306.5 |
3623 |
6.6 |
4.72 |
1960.5 |
|||
|
60% |
16439 |
56.5 |
2599.5 |
3772 |
6.3 |
5.14 |
2209.6 |
|||
|
63% |
17793 |
63.3 |
2913.1 |
3919 |
6.1 |
5.57 |
2476.1 |
|||
|
66% |
19191 |
70.6 |
3249.6 |
4065 |
5.9 |
6.01 |
2762.2 |
|||
|
69% |
20638 |
78.5 |
3612.0 |
4210 |
5.7 |
6.48 |
3070.2 |
|||
|
72% |
22140 |
87.0 |
4003.7 |
4355 |
5.5 |
6.97 |
3403.2 |
|||
|
75% |
23703 |
96.2 |
4428.4 |
4500 |
5.4 |
7.48 |
3764.1 |
|||
|
78% |
25329 |
106.2 |
4889.8 |
4645 |
5.2 |
8.03 |
4156.4 |
|||
|
81% |
27020 |
117.1 |
5391.4 |
4788 |
5.0 |
8.61 |
4582.7 |
|||
|
84% |
28776 |
129.0 |
5935.7 |
4929 |
4.8 |
9.22 |
5045.4 |
|||
|
87% |
30592 |
141.7 |
6523.8 |
5066 |
4.7 |
9.86 |
5545.2 |
|||
|
90% |
32463 |
155.4 |
7154.1 |
5200 |
4.5 |
10.53 |
6080.9 |
|||
|
100% |
38584 |
202.9 |
9340.0 |
5598 |
4.1 |
12.59 |
7939.0 |
Details

The XRotor V9626 motor drawing details the overall size and multiple mounting hole patterns to help plan fitment and hardware selection.

The XRotor V9626 160KV VTOL motor features a vented aluminum housing, central mounting hub, and extended leads for easier routing.

The Hobbywing XRotor HV-9626 160KV motor is listed at 975g with a quoted maximum thrust of 38.5kg and a 39:1 thrust-to-weight ratio.

The XRotor V9626 VTOL motor is positioned for drone applications such as emergency response operations.

The Hobbywing XRotor V9626 VTOL motor features a vented black housing with a clean, low-profile can design for compact installations.

The XRotor V9626 IPC motor uses Intelligent Propeller Control for precise propeller stop positioning with a standardized installation interface.

Recommended setups pair the V9626 160KV motor with a 12S LiPo, MSC 30x9.8 or 32x10.5 propeller, and XRotor Pro-H200A-14S-BLDC-IPC ESC.
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