|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
69V(18S LiPo) |
MSC 64x23 |
35% |
25191 |
33.2 |
2289.4 |
80.46 |
11.0 |
1842.1 |
/ |
|
37% |
28405 |
39.4 |
2722.5 |
81.49 |
10.4 |
2218.6 |
|||
|
39% |
31893 |
46.6 |
3215.1 |
82.40 |
9.9 |
2649.2 |
|||
|
41% |
35618 |
54.6 |
3767.8 |
83.16 |
9.5 |
3133.3 |
|||
|
43% |
39555 |
63.5 |
4382.0 |
83.75 |
9.0 |
3669.9 |
|||
|
45% |
43682 |
73.3 |
5060.0 |
84.20 |
8.6 |
4260.5 |
|||
|
47% |
47985 |
84.1 |
5804.5 |
84.51 |
8.3 |
4905.4 |
|||
|
49% |
52456 |
95.8 |
6619.0 |
84.73 |
7.9 |
5608.3 |
|||
|
51% |
57087 |
108.7 |
7507.3 |
84.86 |
7.6 |
6370.7 |
|||
|
53% |
61875 |
122.7 |
8473.8 |
84.91 |
7.3 |
7195.1 |
|||
|
55% |
66815 |
137.9 |
9522.8 |
84.91 |
7.0 |
8085.8 |
|||
|
57% |
71902 |
154.3 |
10658.6 |
84.85 |
6.7 |
9043.8 |
|||
|
59% |
77131 |
172.1 |
11885.3 |
84.72 |
6.5 |
10069.3 |
|||
|
61% |
82490 |
191.2 |
13206.2 |
84.51 |
6.2 |
11160.6 |
|||
|
63% |
87966 |
211.7 |
14623.4 |
84.21 |
6.0 |
12314.4 |
|||
|
65% |
93538 |
233.7 |
16137.3 |
83.81 |
5.8 |
13524.6 |
|||
|
67% |
99177 |
256.9 |
17745.8 |
83.29 |
5.6 |
14780.5 |
|||
|
69% |
104847 |
281.5 |
19443.6 |
82.64 |
5.4 |
16068.2 |
|||
|
71% |
110501 |
307.3 |
21221.1 |
81.87 |
5.2 |
17373.7 |
|||
|
80% |
133896 |
428.3 |
29586.1 |
77.54 |
4.5 |
22941.0 |
|||
|
85% |
143049 |
483.3 |
33380.6 |
75.58 |
4.3 |
25229.1 |
|||
|
100% |
145997 |
502.2 |
34685.5 |
74.93 |
4.2 |
25989.9 |
-
Drone Propulsion Systems
-
- INTEGRATED PROPULSION SYSTEM Innovation and Performance for a simplified assembly.
- X Series
- H Series
- P Series
-
-
-
- PROPELLER Superior efficiency, exceptional stability.
- Carbon Plastic Propeller
- Carbon Fiber Propeller
-
- CENTRIFUGAL NOZZLE Efficient atomizing, precise spraying.
- 9L
-
- WATER PUMP Minimal maintenance, long service life.
- 5L
- 8L
- 30L
-
- PROPULSION SYSTEM Innovation and Performance for a simplified assembly.
- P Series
-
-
-
- PROPELLER Powerful burst, high intensity.
- Carbon Fiber Propeller
-
-
RC Power Systems
- e-Vehicle Power Systems
- Service and Support
Emergency Firefighting·Industrial Heavy-Lift Missions
Enhanced Thrust with
Built-in Safety Redundancy
The coaxial dual-rotor architecture, paired with large-diameter carbon fiber propellers,
delivers superior thrust, efficiency, and safety through abundant power redundancy.
This robust design ensures responsive performance and reliable operation for
demanding heavy-duty tasks such as: material lifting,
logistics transportation, and emergency firefighting.
Enabling Safer, More Efficient Industrial Heavy-lift UAV applications.
145kg
60kg
4-Axis multirotor Setup Equipped with Coaxial Systems offers (8 rotors / 8 propellers total), delivering:
-Maximum takeoff weight: >240 kg
-Suitable payloads: 100–150 kg.
featuring 12 rotors and 12 propellers, or 8-axis (octocopter) setups with 16 rotors and 16 propellers,
fully covering mainstream requirements for heavy-duty industrial tasks.
please avoid overloading use.
Responsive and Resilient in
Extreme Environmental Challenges
logistics transportation, emergency firefighting,
and various other heavy-lift operations,
fully meeting the diverse requirements of industrial UAV applications.
with a working temperature range of -40℃ — 60℃
environments.
With Enhanced Operational Efficiency
Enlarged motor vents withcentrifugal fans provide efficient
heat dissipation, increasing
cooling efficiency by 20%.
The 100V high-voltage platform,supporting up to 24S (LiPo),
reducing operating current and
thermal losses while alleviating
stress on wiring and connectors.
enabling real-time thermal supervision
for safer and worry-free operation.
Simplified Installation
With the integrated modular design of the motor, ESC, and motor base,
the system is ready to use, greatly improving installation efficiency.
arm tube outer diameter
thickness options, the product is
provided with liner aluminum sleeves,
a strong four-way locking outer cuff,
and positioning collars to ensure a
secure and reliable connection.
ensuring efficient, stable, and agile flight.
Efficient Operations
The meticulously optimized airfoil design combines high strength,
fatigue resistance, low vibration, and high efficiency,
significantly extending the lifespan.
The large-diameter carbon fiber propellers high-torque motors, and high-power,
high-flow ESCs enhance system responsiveness and operational efficiency.
Under coaxial rated thrust, H15MD offers longer flight endurance.
More Stable and Reliable Flight
a newly designed
self-developed FOC ESC,
high-grade materials and HOBBYWING’s
proprietary control algorithms,
enabling stronger motor compatibility,
lower operating temperature rise,
more linear RPM output,
and faster throttle response.
Intelligent Flight & Redundancy
By default, the system supports intelligent propeller control (IPC),
meeting the needs for vehicle-mounted directional propeller stopping,
providing reliable and worry-free operation.
Digital Control
Dual-throttle
redundancy
Ensures real-time responsiveness
and resistance to electromagnetic
interference,
enhancing flight safety.
Analog Control
Rigorous Verification
- Power-on
Protection - Running
Protection - Rigorous
Reliability Tests
Undervoltagewarning
Overvoltagewarning
MOSshort circuits
Motorphase loss
Fail to resetthrottle to zero
Abnormalsampling offsets
Overcurrent
Motor stall
Throttleloss warning
Temperatureanomaly warning
Voltageimpact
High and low-temperaturecycling operation
Extremetemperature tolerance
Anti-interference
Built-in black box function supports 48 hours of propulsion system log storage.
Logs can be read via the CAN bus, offering reliable fault
data traceability for quick diagnostics and maintenance.
with CAN Communication
- Wide compatibility
- The CAN communication protocol is compatible
with mainstream flight controllers such
as ArduPilot, VK, BOYING, JIYI, PX4, and ACFLY,
enabling the creation of an intelligent ecosystem.
- Real-time monitoring
- The flight controller can obtain key data such as RPM,
throttle, current, voltage,
and temperature via the CAN interface.
- Flexible tuning
- HOBBYWING’s proprietary PC DataLink configuration and built-in ESC
throttle parameter adjustment function allow for easy adjustments to drive parameters,
motor rotation direction, light colors, IPC settings, and more.
ESC firmware can be updated online via the DataLinkBox,
meeting the diverse needs of various operations.
*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying load input, for reference only.
Note: Actual flight performance may vary due to environmental factors (e.g., temperature, humidity, altitude, and airflow conditions) as well as specific operating conditions. To ensure optimal system stability and maximize service life, prolonged operation under overload conditions is strongly discouraged.
-
-
Thank you for your interest in HOBBYWING propulsion systems! For customized solutions,
please provide your contact information and technical requirements,
and we will get in touch with you within 24 hours.
- Thanks for reaching out!We have received your message and will get back to you shortly.
- Best Regards,
HOBBYWING Team 
- 18S
- 24S
-
- Model
- Max Thrust
- Recommended takeoff weight per axis
- Efficiency of recommended takeoff weight
- Compatible lithium battery
- Rated voltage
- Input voltage
- Tube outer diameter
- Weight（with cable,without propellers）
- Cable specification
- Operating temperature
- Ingress Protection
- Rated power input
- Rated power output
- Pinout
-
- H15MD-18S
- 145 kg (Sea level)
- 60 kg
- 7.4 g/W
- 18S (LiPo)
- 18S-69V
- 36-80 V
- 80mm-Thickness:3mm
- 11510±200g
- Power cable:7AWG 2000±50 mm Signal cable:2200±50 mm
- -40~60 ℃
- IPX6
- 8200 W
- 7000 W
- Black-GND, White-PWM & Yellow-GND, Gray-CH, Green-CL
- H15MD-24S
- 145 kg (Sea level)
- 60 kg
- 7.4 g/W
- 24S~28S (LiPo)
- 24S-92V / 28S-108V
- 36~130 V
- 80mm-Thickness:3mm
- 11610±200 g
- Power cable:7AWG 2000±50 mm Signal cable:2200±50 mm
- -40~ 60 ℃
- IPX6
- 8100 W
- 7000 W
- Black-GND, White-PWM & Yellow-GND, Gray-CH, Green-CL
-
- Rated voltage
- Communication protocol
- ESC size
- Weight(without cables)
- Peak current (3s)
- continuous current
- Throttle range calibration
- Throttle Source
- Operating pulse width
- Fault storage & Log
-
- 18S-69V
- UAVCAN
- 155.6*83.6*44.3 mm
- 578±10 g
- 300A (3s)
- 120 A
- Not supported
- PWM+CAN
- 1100-1940 μs
- 2-48 h
- 24S-92V / 28S-108V
- UAVCAN
- 155.6*83.6*54.3 mm
- 616±5 g
- 300A (3s)
- 110 A
- Not supported
- PWM+CAN
- 1100-1940 μs
- 2-48 h
-
- Model
- Weight(with cables)
- Motor diameter
- Slot & Pole
- Stator size
-
- 15623-45KV
- 2800±100 g
- 167.1 mm
- 36N 44P
- Φ155.6 * H23 mm
- 15623-35 KV
- 2800±100 g
- 167.1 mm
- 36N 44P
- Φ155.6 * H23 mm
-
- Model
- Weight
- Material of blades
- Mounting dimensions
- Model
- Weight
- Material of blades
- Mounting dimensions
-
- MSC 64x23
- 1034±20 g
- Carbon fibre composite material
- D60-6*M6, centre hole D20
- MFC 63x24
- 930±9 g
- Carbon fibre composite material
- D46-4*M6，centre hole D15
- MFC 63x24
- 1034±20 g
- Carbon fibre composite material
- D60-6*M6, centre hole D20
- MFC 63x24
- 930±9 g
- Carbon fibre composite material
- D46-4*M6，centre hole D15
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
69V (18S LiPo) |
MFC 63x24 |
33% |
20328 |
25.4 |
1754.6 |
80.51 |
11.6 |
1412.7 |
/ |
|
38% |
27671 |
38.7 |
2672.0 |
84.21 |
10.4 |
2250.1 |
|||
|
40% |
30933 |
45.5 |
3141.8 |
84.86 |
9.8 |
2666.1 |
|||
|
42% |
34385 |
53.2 |
3673.0 |
85.28 |
9.4 |
3132.3 |
|||
|
44% |
38029 |
61.8 |
4268.5 |
85.58 |
8.9 |
3652.9 |
|||
|
46% |
41868 |
71.3 |
4928.2 |
85.81 |
8.5 |
4228.9 |
|||
|
48% |
45902 |
81.9 |
5654.2 |
86.01 |
8.1 |
4863.2 |
|||
|
50% |
50131 |
93.3 |
6447.9 |
86.18 |
7.8 |
5556.8 |
|||
|
52% |
54552 |
105.8 |
7312.5 |
86.34 |
7.5 |
6313.6 |
|||
|
54% |
59160 |
119.4 |
8249.3 |
86.48 |
7.2 |
7134.0 |
|||
|
56% |
63946 |
134.1 |
9262.2 |
86.57 |
6.9 |
8018.3 |
|||
|
58% |
68901 |
149.9 |
10356.6 |
86.60 |
6.7 |
8968.8 |
|||
|
60% |
74008 |
167.0 |
11537.3 |
86.55 |
6.4 |
9985.6 |
|||
|
62% |
79248 |
185.4 |
12810.7 |
86.40 |
6.2 |
11068.4 |
|||
|
64% |
84598 |
205.3 |
14181.4 |
86.14 |
6.0 |
12215.9 |
|||
|
66% |
90028 |
226.6 |
15653.0 |
85.75 |
5.8 |
13422.5 |
|||
|
68% |
95505 |
249.3 |
17225.5 |
85.25 |
5.5 |
14684.8 |
|||
|
70% |
100986 |
273.5 |
18894.0 |
84.63 |
5.3 |
15990.0 |
|||
|
72% |
106426 |
298.9 |
20647.5 |
83.92 |
5.2 |
17327.4 |
|||
|
80% |
126578 |
404.9 |
27975.9 |
80.58 |
4.5 |
22543.0 |
|||
|
87% |
139172 |
478.9 |
33083.7 |
78.17 |
4.2 |
25861.6 |
|||
|
100% |
142696 |
500.0 |
34547.1 |
77.48 |
4.1 |
26767.1 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
92V(24S LiPo) |
MSC 64x23 |
33% |
18334 |
15.6 |
1434.2 |
78.83 |
12.8 |
1130.6 |
/ |
|
38% |
24935 |
23.9 |
2197.0 |
82.51 |
11.3 |
1812.7 |
|||
|
42% |
31294 |
33.1 |
3046.0 |
84.20 |
10.3 |
2564.7 |
|||
|
44% |
34803 |
38.7 |
3556.8 |
84.76 |
9.8 |
3014.7 |
|||
|
46% |
38529 |
44.9 |
4129.2 |
85.18 |
9.3 |
3517.2 |
|||
|
48% |
42474 |
51.8 |
4766.9 |
85.51 |
8.9 |
4076.1 |
|||
|
50% |
46643 |
59.5 |
5474.1 |
85.77 |
8.5 |
4695.1 |
|||
|
52% |
51041 |
68.0 |
6255.6 |
85.99 |
8.2 |
5379.2 |
|||
|
54% |
55674 |
77.3 |
7116.6 |
86.16 |
7.8 |
6131.7 |
|||
|
56% |
60544 |
87.6 |
8062.9 |
86.30 |
7.5 |
6958.3 |
|||
|
58% |
65650 |
98.9 |
9100.6 |
86.40 |
7.2 |
7862.9 |
|||
|
60% |
70987 |
111.2 |
10236.1 |
86.46 |
6.9 |
8850.2 |
|||
|
62% |
76544 |
124.7 |
11476.1 |
86.44 |
6.7 |
9919.9 |
|||
|
64% |
82302 |
139.4 |
12826.6 |
86.33 |
6.4 |
11073.2 |
|||
|
66% |
88234 |
155.3 |
14293.2 |
86.10 |
6.2 |
12306.4 |
|||
|
68% |
94302 |
172.6 |
15878.9 |
85.71 |
5.9 |
13609.8 |
|||
|
70% |
100459 |
191.1 |
17583.7 |
85.17 |
5.7 |
14976.0 |
|||
|
72% |
106643 |
210.8 |
19401.4 |
84.45 |
5.5 |
16384.5 |
|||
|
76% |
118776 |
253.3 |
23307.5 |
82.55 |
5.1 |
19240.3 |
|||
|
80% |
129906 |
297.0 |
27329.8 |
80.36 |
4.8 |
21962.2 |
|||
|
85% |
140730 |
344.4 |
31688.8 |
77.99 |
4.4 |
24714.1 |
|||
|
100% |
144500 |
362.2 |
33331.7 |
77.17 |
4.3 |
25722.1 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
108V(28S LiPo) |
MSC 64x23 |
33% |
24912 |
20.6 |
2220.5 |
81.72 |
11.2 |
1814.6 |
/ |
|
38% |
33942 |
31.8 |
3431.8 |
84.57 |
9.9 |
2902.3 |
|||
|
42% |
42087 |
43.7 |
4726.1 |
85.38 |
8.9 |
4035.2 |
|||
|
44% |
46626 |
51.0 |
5509.8 |
85.61 |
8.5 |
4716.9 |
|||
|
46% |
51514 |
59.2 |
6395.0 |
85.78 |
8.1 |
5485.7 |
|||
|
48% |
56756 |
68.4 |
7387.6 |
85.92 |
7.7 |
6347.4 |
|||
|
50% |
62343 |
78.6 |
8491.8 |
86.04 |
7.3 |
7306.4 |
|||
|
52% |
68251 |
89.9 |
9711.5 |
86.11 |
7.0 |
8362.6 |
|||
|
54% |
74440 |
102.3 |
11050.7 |
86.12 |
6.7 |
9516.8 |
|||
|
56% |
80863 |
115.8 |
12514.4 |
86.03 |
6.5 |
10766.1 |
|||
|
58% |
87456 |
130.6 |
14108.2 |
85.82 |
6.2 |
12107.6 |
|||
|
60% |
94149 |
146.6 |
15836.9 |
85.44 |
5.9 |
13531.1 |
|||
|
62% |
100861 |
163.9 |
17702.2 |
84.86 |
5.7 |
15022.1 |
|||
|
64% |
107503 |
182.3 |
19698.8 |
84.07 |
5.5 |
16560.8 |
|||
|
66% |
113982 |
201.9 |
21810.2 |
83.07 |
5.2 |
18117.8 |
|||
|
68% |
120197 |
222.2 |
24005.7 |
81.87 |
5.0 |
19653.4 |
|||
|
70% |
126043 |
242.8 |
26236.9 |
80.52 |
4.8 |
21126.0 |
|||
|
72% |
131412 |
263.2 |
28437.9 |
79.10 |
4.6 |
22494.4 |
|||
|
74% |
136195 |
282.5 |
30526.7 |
77.67 |
4.5 |
23710.1 |
|||
|
76% |
140281 |
300.0 |
32409.7 |
76.34 |
4.3 |
24741.5 |
|||
|
80% |
145919 |
325.4 |
35162.5 |
74.33 |
4.1 |
26136.3 |
|||
|
100% |
147509 |
333.0 |
35979.8 |
73.75 |
4.1 |
26535.1 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
92V (24S LiPo) |
MFC 63x24 |
33% |
16043 |
14.4 |
1326.2 |
80.27 |
12.1 |
1064.5 |
/ |
|
38% |
22145 |
22.2 |
2038.5 |
82.61 |
10.9 |
1684.0 |
|||
|
42% |
27949 |
30.4 |
2795.0 |
84.77 |
10.0 |
2369.3 |
|||
|
44% |
31158 |
35.3 |
3247.7 |
85.69 |
9.6 |
2783.0 |
|||
|
46% |
34577 |
40.8 |
3756.7 |
86.45 |
9.2 |
3247.6 |
|||
|
48% |
38211 |
47.0 |
4328.2 |
87.04 |
8.8 |
3767.2 |
|||
|
50% |
42068 |
54.0 |
4968.7 |
87.47 |
8.5 |
4346.1 |
|||
|
52% |
46150 |
61.8 |
5684.7 |
87.74 |
8.1 |
4987.7 |
|||
|
54% |
50464 |
70.4 |
6481.7 |
87.88 |
7.8 |
5696.1 |
|||
|
56% |
55009 |
80.0 |
7366.1 |
87.92 |
7.5 |
6476.3 |
|||
|
58% |
59785 |
90.6 |
8340.7 |
87.89 |
7.2 |
7330.6 |
|||
|
60% |
64785 |
102.3 |
9410.1 |
87.82 |
6.9 |
8263.9 |
|||
|
62% |
69999 |
114.9 |
10575.2 |
87.74 |
6.6 |
9278.7 |
|||
|
64% |
75410 |
128.6 |
11836.0 |
87.65 |
6.4 |
10374.2 |
|||
|
66% |
80997 |
143.3 |
13191.6 |
87.56 |
6.1 |
11550.5 |
|||
|
68% |
86729 |
159.1 |
14640.1 |
87.44 |
5.9 |
12801.3 |
|||
|
70% |
92568 |
175.8 |
16181.6 |
87.28 |
5.7 |
14123.3 |
|||
|
72% |
98466 |
193.6 |
17814.2 |
87.02 |
5.5 |
15502.0 |
|||
|
76% |
110202 |
232.0 |
21355.1 |
86.01 |
5.2 |
18367.5 |
|||
|
80% |
121346 |
274.0 |
25219.9 |
84.14 |
4.8 |
21220.0 |
|||
|
85% |
133223 |
327.8 |
30171.6 |
80.86 |
4.4 |
24396.8 |
|||
|
100% |
142372 |
378.4 |
34830.7 |
77.38 |
4.1 |
26952.0 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
108V (28S LiPo) |
MFC 63x24 |
33% |
21935 |
18.8 |
2032.6 |
82.7 |
10.8 |
1680.9 |
/ |
|
38% |
30188 |
28.8 |
3110.4 |
85.90 |
9.7 |
2671.8 |
|||
|
42% |
37917 |
40.1 |
4327.6 |
86.73 |
8.8 |
3753.3 |
|||
|
44% |
42184 |
46.9 |
5064.1 |
86.97 |
8.3 |
4404.3 |
|||
|
46% |
46730 |
54.5 |
5887.1 |
87.18 |
7.9 |
5132.4 |
|||
|
48% |
51560 |
63.0 |
6800.8 |
87.37 |
7.6 |
5941.8 |
|||
|
50% |
56677 |
72.3 |
7807.3 |
87.55 |
7.3 |
6835.3 |
|||
|
52% |
62075 |
82.5 |
8912.2 |
87.70 |
7.0 |
7816.0 |
|||
|
54% |
67746 |
93.7 |
10121.8 |
87.80 |
6.7 |
8886.9 |
|||
|
56% |
73671 |
106.0 |
11443.7 |
87.82 |
6.4 |
10049.8 |
|||
|
58% |
79825 |
119.4 |
12890.9 |
87.73 |
6.2 |
11309.2 |
|||
|
60% |
86172 |
134.0 |
14476.3 |
87.50 |
6.0 |
12666.8 |
|||
|
62% |
92664 |
150.1 |
16212.3 |
87.10 |
5.7 |
14120.9 |
|||
|
64% |
99244 |
167.6 |
18103.6 |
86.52 |
5.5 |
15663.2 |
|||
|
66% |
105837 |
186.6 |
20150.3 |
85.76 |
5.3 |
17280.9 |
|||
|
68% |
112358 |
206.8 |
22338.6 |
84.82 |
5.0 |
18947.6 |
|||
|
70% |
118704 |
228.1 |
24632.8 |
83.72 |
4.8 |
20622.5 |
|||
|
72% |
124754 |
249.8 |
26977.7 |
82.48 |
4.6 |
22251.2 |
|||
|
74% |
130371 |
271.2 |
29295.0 |
81.16 |
4.5 |
23775.8 |
|||
|
76% |
135398 |
291.4 |
31475.9 |
79.83 |
4.3 |
25127.2 |
|||
|
78% |
139657 |
309.2 |
33401.9 |
78.58 |
4.2 |
26247.2 |
|||
|
100% |
142949 |
323.5 |
34941.2 |
77.52 |
4.1 |
27086.4 |
Support
Manuals & Documents
Disclaimer
The purpose of this website is only to introduce you to the basic situation of HOBBYWING company and product information. Unless otherwise stated, all information provided on this website should not be regarded as an offer or acceptance, and this website will not assume any binding obligations to you as a result of the provision of information. For all your requests, HOBBYWING reserves the full right to decide whether to commit or not.
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HOBBYWING reserves the right to correct, modify and update this statement at any time.
Software Download
Emergency Firefighting·Industrial Heavy-Lift Missions
Enhanced Thrust with
Built-in Safety Redundancy
The coaxial dual-rotor architecture, paired with large-diameter carbon fiber propellers,
delivers superior thrust, efficiency, and safety through abundant power redundancy.
This robust design ensures responsive performance and reliable operation for
demanding heavy-duty tasks such as: material lifting,
logistics transportation, and emergency firefighting.
Enabling Safer, More Efficient Industrial Heavy-lift UAV applications.
145kg
60kg
4-Axis multirotor Setup Equipped with Coaxial Systems offers (8 rotors / 8 propellers total), delivering:
-Maximum takeoff weight: >240 kg
-Suitable payloads: 100–150 kg.
featuring 12 rotors and 12 propellers, or 8-axis (octocopter) setups with 16 rotors and 16 propellers,
fully covering mainstream requirements for heavy-duty industrial tasks.
please avoid overloading use.
Responsive and Resilient in
Extreme Environmental Challenges
logistics transportation, emergency firefighting,
and various other heavy-lift operations,
fully meeting the diverse requirements of industrial UAV applications.
with a working temperature range of -40℃ — 60℃
environments.
With Enhanced Operational Efficiency
Enlarged motor vents withcentrifugal fans provide efficient
heat dissipation, increasing
cooling efficiency by 20%.
The 100V high-voltage platform,supporting up to 24S (LiPo),
reducing operating current and
thermal losses while alleviating
stress on wiring and connectors.
enabling real-time thermal supervision
for safer and worry-free operation.
Simplified Installation
With the integrated modular design of the motor, ESC, and motor base,
the system is ready to use, greatly improving installation efficiency.
arm tube outer diameter
thickness options, the product is
provided with liner aluminum sleeves,
a strong four-way locking outer cuff,
and positioning collars to ensure a
secure and reliable connection.
ensuring efficient, stable, and agile flight.
Efficient Operations
The meticulously optimized airfoil design combines high strength,
fatigue resistance, low vibration, and high efficiency,
significantly extending the lifespan.
The large-diameter carbon fiber propellers high-torque motors, and high-power,
high-flow ESCs enhance system responsiveness and operational efficiency.
Under coaxial rated thrust, H15MD offers longer flight endurance.
More Stable and Reliable Flight
a newly designed
self-developed FOC ESC,
high-grade materials and HOBBYWING’s
proprietary control algorithms,
enabling stronger motor compatibility,
lower operating temperature rise,
more linear RPM output,
and faster throttle response.
Intelligent Flight & Redundancy
By default, the system supports intelligent propeller control (IPC),
meeting the needs for vehicle-mounted directional propeller stopping,
providing reliable and worry-free operation.
Digital Control
Dual-throttle
redundancy
Ensures real-time responsiveness
and resistance to electromagnetic
interference,
enhancing flight safety.
Analog Control
Rigorous Verification
- Power-on
Protection - Running
Protection - Rigorous
Reliability Tests
Undervoltagewarning
Overvoltagewarning
MOSshort circuits
Motorphase loss
Fail to resetthrottle to zero
Abnormalsampling offsets
OvercurrentMotor stallThrottleloss warning
Temperatureanomaly warning
Voltageimpact
High and low-temperaturecycling operation
Extremetemperature tolerance
Anti-interference
Built-in black box function supports 48 hours of propulsion system log storage.
Logs can be read via the CAN bus, offering reliable fault
data traceability for quick diagnostics and maintenance.
with CAN Communication
- Wide compatibility
- The CAN communication protocol is compatible
with mainstream flight controllers such
as ArduPilot, VK, BOYING, JIYI, PX4, and ACFLY,
enabling the creation of an intelligent ecosystem.
- Real-time monitoring
- The flight controller can obtain key data such as RPM,
throttle, current, voltage,
and temperature via the CAN interface.
- Flexible tuning
- HOBBYWING’s proprietary PC DataLink configuration and built-in ESC
throttle parameter adjustment function allow for easy adjustments to drive parameters,
motor rotation direction, light colors, IPC settings, and more.
ESC firmware can be updated online via the DataLinkBox,
meeting the diverse needs of various operations.
*The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying load input, for reference only.
Note: Actual flight performance may vary due to environmental factors (e.g., temperature, humidity, altitude, and airflow conditions) as well as specific operating conditions. To ensure optimal system stability and maximize service life, prolonged operation under overload conditions is strongly discouraged.
-
- Thank you for your interest in HOBBYWING propulsion systems! For customized solutions, please provide your contact information and technical requirements, and we will get in touch with you within 24 hours.
- Thanks for reaching out!We have received your message and will get back to you shortly.
- Best Regards,
HOBBYWING Team
- 18S
- 24S
-
- Model
- Max Thrust
- Recommended takeoff weight per axis
- Efficiency of recommended takeoff weight
- Compatible lithium battery
- Rated voltage
- Input voltage
- Tube outer diameter
- Weight（with cable,without propellers）
- Cable specification
- Operating temperature
- Ingress Protection
- Rated power input
- Rated power output
- Pinout
-
- H15MD-18S
- 145 kg (Sea level)
- 60 kg
- 7.4 g/W
- 18S (LiPo)
- 18S-69V
- 36-80 V
- 80mm-Thickness:3mm
- 11510±200g
- Power cable:7AWG 2000±50 mm Signal cable:2200±50 mm
- -40~60 ℃
- IPX6
- 8200 W
- 7000 W
- Black-GND, White-PWM & Yellow-GND, Gray-CH, Green-CL
- H15MD-24S
- 145 kg (Sea level)
- 60 kg
- 7.4 g/W
- 24S~28S (LiPo)
- 24S-92V / 28S-108V
- 36~130 V
- 80mm-Thickness:3mm
- 11610±200 g
- Power cable:7AWG 2000±50 mm Signal cable:2200±50 mm
- -40~ 60 ℃
- IPX6
- 8100 W
- 7000 W
- Black-GND, White-PWM & Yellow-GND, Gray-CH, Green-CL
-
- Rated voltage
- Communication protocol
- ESC size
- Weight(without cables)
- Peak current (3s)
- continuous current
- Throttle range calibration
- Throttle Source
- Operating pulse width
- Fault storage & Log
-
- 18S-69V
- UAVCAN
- 155.6*83.6*44.3 mm
- 578±10 g
- 300A (3s)
- 120 A
- Not supported
- PWM+CAN
- 1100-1940 μs
- 2-48 h
- 24S-92V / 28S-108V
- UAVCAN
- 155.6*83.6*54.3 mm
- 616±5 g
- 300A (3s)
- 110 A
- Not supported
- PWM+CAN
- 1100-1940 μs
- 2-48 h
-
- Model
- Weight(with cables)
- Motor diameter
- Slot & Pole
- Stator size
-
- 15623-45KV
- 2800±100 g
- 167.1 mm
- 36N 44P
- Φ155.6 * H23 mm
- 15623-35 KV
- 2800±100 g
- 167.1 mm
- 36N 44P
- Φ155.6 * H23 mm
-
- Model
- Weight
- Material of blades
- Mounting dimensions
- Model
- Weight
- Material of blades
- Mounting dimensions
-
- MSC 64x23
- 1034±20 g
- Carbon fibre composite material
- D60-6*M6, centre hole D20
- MFC 63x24
- 930±9 g
- Carbon fibre composite material
- D46-4*M6，centre hole D15
- MFC 63x24
- 1034±20 g
- Carbon fibre composite material
- D60-6*M6, centre hole D20
- MFC 63x24
- 930±9 g
- Carbon fibre composite material
- D46-4*M6，centre hole D15
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
69V(18S LiPo) |
MSC 64x23 |
35% |
25191 |
33.2 |
2289.4 |
80.46 |
11.0 |
1842.1 |
/ |
|
37% |
28405 |
39.4 |
2722.5 |
81.49 |
10.4 |
2218.6 |
|||
|
39% |
31893 |
46.6 |
3215.1 |
82.40 |
9.9 |
2649.2 |
|||
|
41% |
35618 |
54.6 |
3767.8 |
83.16 |
9.5 |
3133.3 |
|||
|
43% |
39555 |
63.5 |
4382.0 |
83.75 |
9.0 |
3669.9 |
|||
|
45% |
43682 |
73.3 |
5060.0 |
84.20 |
8.6 |
4260.5 |
|||
|
47% |
47985 |
84.1 |
5804.5 |
84.51 |
8.3 |
4905.4 |
|||
|
49% |
52456 |
95.8 |
6619.0 |
84.73 |
7.9 |
5608.3 |
|||
|
51% |
57087 |
108.7 |
7507.3 |
84.86 |
7.6 |
6370.7 |
|||
|
53% |
61875 |
122.7 |
8473.8 |
84.91 |
7.3 |
7195.1 |
|||
|
55% |
66815 |
137.9 |
9522.8 |
84.91 |
7.0 |
8085.8 |
|||
|
57% |
71902 |
154.3 |
10658.6 |
84.85 |
6.7 |
9043.8 |
|||
|
59% |
77131 |
172.1 |
11885.3 |
84.72 |
6.5 |
10069.3 |
|||
|
61% |
82490 |
191.2 |
13206.2 |
84.51 |
6.2 |
11160.6 |
|||
|
63% |
87966 |
211.7 |
14623.4 |
84.21 |
6.0 |
12314.4 |
|||
|
65% |
93538 |
233.7 |
16137.3 |
83.81 |
5.8 |
13524.6 |
|||
|
67% |
99177 |
256.9 |
17745.8 |
83.29 |
5.6 |
14780.5 |
|||
|
69% |
104847 |
281.5 |
19443.6 |
82.64 |
5.4 |
16068.2 |
|||
|
71% |
110501 |
307.3 |
21221.1 |
81.87 |
5.2 |
17373.7 |
|||
|
80% |
133896 |
428.3 |
29586.1 |
77.54 |
4.5 |
22941.0 |
|||
|
85% |
143049 |
483.3 |
33380.6 |
75.58 |
4.3 |
25229.1 |
|||
|
100% |
145997 |
502.2 |
34685.5 |
74.93 |
4.2 |
25989.9 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
69V (18S LiPo) |
MFC 63x24 |
33% |
20328 |
25.4 |
1754.6 |
80.51 |
11.6 |
1412.7 |
/ |
|
38% |
27671 |
38.7 |
2672.0 |
84.21 |
10.4 |
2250.1 |
|||
|
40% |
30933 |
45.5 |
3141.8 |
84.86 |
9.8 |
2666.1 |
|||
|
42% |
34385 |
53.2 |
3673.0 |
85.28 |
9.4 |
3132.3 |
|||
|
44% |
38029 |
61.8 |
4268.5 |
85.58 |
8.9 |
3652.9 |
|||
|
46% |
41868 |
71.3 |
4928.2 |
85.81 |
8.5 |
4228.9 |
|||
|
48% |
45902 |
81.9 |
5654.2 |
86.01 |
8.1 |
4863.2 |
|||
|
50% |
50131 |
93.3 |
6447.9 |
86.18 |
7.8 |
5556.8 |
|||
|
52% |
54552 |
105.8 |
7312.5 |
86.34 |
7.5 |
6313.6 |
|||
|
54% |
59160 |
119.4 |
8249.3 |
86.48 |
7.2 |
7134.0 |
|||
|
56% |
63946 |
134.1 |
9262.2 |
86.57 |
6.9 |
8018.3 |
|||
|
58% |
68901 |
149.9 |
10356.6 |
86.60 |
6.7 |
8968.8 |
|||
|
60% |
74008 |
167.0 |
11537.3 |
86.55 |
6.4 |
9985.6 |
|||
|
62% |
79248 |
185.4 |
12810.7 |
86.40 |
6.2 |
11068.4 |
|||
|
64% |
84598 |
205.3 |
14181.4 |
86.14 |
6.0 |
12215.9 |
|||
|
66% |
90028 |
226.6 |
15653.0 |
85.75 |
5.8 |
13422.5 |
|||
|
68% |
95505 |
249.3 |
17225.5 |
85.25 |
5.5 |
14684.8 |
|||
|
70% |
100986 |
273.5 |
18894.0 |
84.63 |
5.3 |
15990.0 |
|||
|
72% |
106426 |
298.9 |
20647.5 |
83.92 |
5.2 |
17327.4 |
|||
|
80% |
126578 |
404.9 |
27975.9 |
80.58 |
4.5 |
22543.0 |
|||
|
87% |
139172 |
478.9 |
33083.7 |
78.17 |
4.2 |
25861.6 |
|||
|
100% |
142696 |
500.0 |
34547.1 |
77.48 |
4.1 |
26767.1 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
92V(24S LiPo) |
MSC 64x23 |
33% |
18334 |
15.6 |
1434.2 |
78.83 |
12.8 |
1130.6 |
/ |
|
38% |
24935 |
23.9 |
2197.0 |
82.51 |
11.3 |
1812.7 |
|||
|
42% |
31294 |
33.1 |
3046.0 |
84.20 |
10.3 |
2564.7 |
|||
|
44% |
34803 |
38.7 |
3556.8 |
84.76 |
9.8 |
3014.7 |
|||
|
46% |
38529 |
44.9 |
4129.2 |
85.18 |
9.3 |
3517.2 |
|||
|
48% |
42474 |
51.8 |
4766.9 |
85.51 |
8.9 |
4076.1 |
|||
|
50% |
46643 |
59.5 |
5474.1 |
85.77 |
8.5 |
4695.1 |
|||
|
52% |
51041 |
68.0 |
6255.6 |
85.99 |
8.2 |
5379.2 |
|||
|
54% |
55674 |
77.3 |
7116.6 |
86.16 |
7.8 |
6131.7 |
|||
|
56% |
60544 |
87.6 |
8062.9 |
86.30 |
7.5 |
6958.3 |
|||
|
58% |
65650 |
98.9 |
9100.6 |
86.40 |
7.2 |
7862.9 |
|||
|
60% |
70987 |
111.2 |
10236.1 |
86.46 |
6.9 |
8850.2 |
|||
|
62% |
76544 |
124.7 |
11476.1 |
86.44 |
6.7 |
9919.9 |
|||
|
64% |
82302 |
139.4 |
12826.6 |
86.33 |
6.4 |
11073.2 |
|||
|
66% |
88234 |
155.3 |
14293.2 |
86.10 |
6.2 |
12306.4 |
|||
|
68% |
94302 |
172.6 |
15878.9 |
85.71 |
5.9 |
13609.8 |
|||
|
70% |
100459 |
191.1 |
17583.7 |
85.17 |
5.7 |
14976.0 |
|||
|
72% |
106643 |
210.8 |
19401.4 |
84.45 |
5.5 |
16384.5 |
|||
|
76% |
118776 |
253.3 |
23307.5 |
82.55 |
5.1 |
19240.3 |
|||
|
80% |
129906 |
297.0 |
27329.8 |
80.36 |
4.8 |
21962.2 |
|||
|
85% |
140730 |
344.4 |
31688.8 |
77.99 |
4.4 |
24714.1 |
|||
|
100% |
144500 |
362.2 |
33331.7 |
77.17 |
4.3 |
25722.1 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
108V(28S LiPo) |
MSC 64x23 |
33% |
24912 |
20.6 |
2220.5 |
81.72 |
11.2 |
1814.6 |
/ |
|
38% |
33942 |
31.8 |
3431.8 |
84.57 |
9.9 |
2902.3 |
|||
|
42% |
42087 |
43.7 |
4726.1 |
85.38 |
8.9 |
4035.2 |
|||
|
44% |
46626 |
51.0 |
5509.8 |
85.61 |
8.5 |
4716.9 |
|||
|
46% |
51514 |
59.2 |
6395.0 |
85.78 |
8.1 |
5485.7 |
|||
|
48% |
56756 |
68.4 |
7387.6 |
85.92 |
7.7 |
6347.4 |
|||
|
50% |
62343 |
78.6 |
8491.8 |
86.04 |
7.3 |
7306.4 |
|||
|
52% |
68251 |
89.9 |
9711.5 |
86.11 |
7.0 |
8362.6 |
|||
|
54% |
74440 |
102.3 |
11050.7 |
86.12 |
6.7 |
9516.8 |
|||
|
56% |
80863 |
115.8 |
12514.4 |
86.03 |
6.5 |
10766.1 |
|||
|
58% |
87456 |
130.6 |
14108.2 |
85.82 |
6.2 |
12107.6 |
|||
|
60% |
94149 |
146.6 |
15836.9 |
85.44 |
5.9 |
13531.1 |
|||
|
62% |
100861 |
163.9 |
17702.2 |
84.86 |
5.7 |
15022.1 |
|||
|
64% |
107503 |
182.3 |
19698.8 |
84.07 |
5.5 |
16560.8 |
|||
|
66% |
113982 |
201.9 |
21810.2 |
83.07 |
5.2 |
18117.8 |
|||
|
68% |
120197 |
222.2 |
24005.7 |
81.87 |
5.0 |
19653.4 |
|||
|
70% |
126043 |
242.8 |
26236.9 |
80.52 |
4.8 |
21126.0 |
|||
|
72% |
131412 |
263.2 |
28437.9 |
79.10 |
4.6 |
22494.4 |
|||
|
74% |
136195 |
282.5 |
30526.7 |
77.67 |
4.5 |
23710.1 |
|||
|
76% |
140281 |
300.0 |
32409.7 |
76.34 |
4.3 |
24741.5 |
|||
|
80% |
145919 |
325.4 |
35162.5 |
74.33 |
4.1 |
26136.3 |
|||
|
100% |
147509 |
333.0 |
35979.8 |
73.75 |
4.1 |
26535.1 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
92V (24S LiPo) |
MFC 63x24 |
33% |
16043 |
14.4 |
1326.2 |
80.27 |
12.1 |
1064.5 |
/ |
|
38% |
22145 |
22.2 |
2038.5 |
82.61 |
10.9 |
1684.0 |
|||
|
42% |
27949 |
30.4 |
2795.0 |
84.77 |
10.0 |
2369.3 |
|||
|
44% |
31158 |
35.3 |
3247.7 |
85.69 |
9.6 |
2783.0 |
|||
|
46% |
34577 |
40.8 |
3756.7 |
86.45 |
9.2 |
3247.6 |
|||
|
48% |
38211 |
47.0 |
4328.2 |
87.04 |
8.8 |
3767.2 |
|||
|
50% |
42068 |
54.0 |
4968.7 |
87.47 |
8.5 |
4346.1 |
|||
|
52% |
46150 |
61.8 |
5684.7 |
87.74 |
8.1 |
4987.7 |
|||
|
54% |
50464 |
70.4 |
6481.7 |
87.88 |
7.8 |
5696.1 |
|||
|
56% |
55009 |
80.0 |
7366.1 |
87.92 |
7.5 |
6476.3 |
|||
|
58% |
59785 |
90.6 |
8340.7 |
87.89 |
7.2 |
7330.6 |
|||
|
60% |
64785 |
102.3 |
9410.1 |
87.82 |
6.9 |
8263.9 |
|||
|
62% |
69999 |
114.9 |
10575.2 |
87.74 |
6.6 |
9278.7 |
|||
|
64% |
75410 |
128.6 |
11836.0 |
87.65 |
6.4 |
10374.2 |
|||
|
66% |
80997 |
143.3 |
13191.6 |
87.56 |
6.1 |
11550.5 |
|||
|
68% |
86729 |
159.1 |
14640.1 |
87.44 |
5.9 |
12801.3 |
|||
|
70% |
92568 |
175.8 |
16181.6 |
87.28 |
5.7 |
14123.3 |
|||
|
72% |
98466 |
193.6 |
17814.2 |
87.02 |
5.5 |
15502.0 |
|||
|
76% |
110202 |
232.0 |
21355.1 |
86.01 |
5.2 |
18367.5 |
|||
|
80% |
121346 |
274.0 |
25219.9 |
84.14 |
4.8 |
21220.0 |
|||
|
85% |
133223 |
327.8 |
30171.6 |
80.86 |
4.4 |
24396.8 |
|||
|
100% |
142372 |
378.4 |
34830.7 |
77.38 |
4.1 |
26952.0 |
|
Voltage(V) |
Propeller |
Throttle(%) |
Thrust(g) |
Current(A) |
Power Input(W) |
Efficiency(%) |
Efficiency(g/W) |
Power Output(W) |
Temperature(℃) |
|---|---|---|---|---|---|---|---|---|---|
|
108V (28S LiPo) |
MFC 63x24 |
33% |
21935 |
18.8 |
2032.6 |
82.7 |
10.8 |
1680.9 |
/ |
|
38% |
30188 |
28.8 |
3110.4 |
85.90 |
9.7 |
2671.8 |
|||
|
42% |
37917 |
40.1 |
4327.6 |
86.73 |
8.8 |
3753.3 |
|||
|
44% |
42184 |
46.9 |
5064.1 |
86.97 |
8.3 |
4404.3 |
|||
|
46% |
46730 |
54.5 |
5887.1 |
87.18 |
7.9 |
5132.4 |
|||
|
48% |
51560 |
63.0 |
6800.8 |
87.37 |
7.6 |
5941.8 |
|||
|
50% |
56677 |
72.3 |
7807.3 |
87.55 |
7.3 |
6835.3 |
|||
|
52% |
62075 |
82.5 |
8912.2 |
87.70 |
7.0 |
7816.0 |
|||
|
54% |
67746 |
93.7 |
10121.8 |
87.80 |
6.7 |
8886.9 |
|||
|
56% |
73671 |
106.0 |
11443.7 |
87.82 |
6.4 |
10049.8 |
|||
|
58% |
79825 |
119.4 |
12890.9 |
87.73 |
6.2 |
11309.2 |
|||
|
60% |
86172 |
134.0 |
14476.3 |
87.50 |
6.0 |
12666.8 |
|||
|
62% |
92664 |
150.1 |
16212.3 |
87.10 |
5.7 |
14120.9 |
|||
|
64% |
99244 |
167.6 |
18103.6 |
86.52 |
5.5 |
15663.2 |
|||
|
66% |
105837 |
186.6 |
20150.3 |
85.76 |
5.3 |
17280.9 |
|||
|
68% |
112358 |
206.8 |
22338.6 |
84.82 |
5.0 |
18947.6 |
|||
|
70% |
118704 |
228.1 |
24632.8 |
83.72 |
4.8 |
20622.5 |
|||
|
72% |
124754 |
249.8 |
26977.7 |
82.48 |
4.6 |
22251.2 |
|||
|
74% |
130371 |
271.2 |
29295.0 |
81.16 |
4.5 |
23775.8 |
|||
|
76% |
135398 |
291.4 |
31475.9 |
79.83 |
4.3 |
25127.2 |
|||
|
78% |
139657 |
309.2 |
33401.9 |
78.58 |
4.2 |
26247.2 |
|||
|
100% |
142949 |
323.5 |
34941.2 |
77.52 |
4.1 |
27086.4 |
Support
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