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MAD AM110 Heavy-Lift Drone Power System Kit AeroMax 110 9KV + SineSic 160A Pro ESC + 73x29in Prop

MAD AM110 Heavy-Lift Drone Power System Kit AeroMax 110 9KV + SineSic 160A Pro ESC + 73x29in Prop

MAD

Regular price $12,748.50 USD
Regular price Sale price $12,748.50 USD
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Overview

MAD AM110 Heavy-Lift Drone Power System Kit (AeroMax 110 KIT 9KV) is a heavy-lift drone power system kit that combines a motor, ESC, and carbon-fiber propeller into one matched propulsion set. Kit A includes a PT1000 temperature sensor. Kit B includes a PT1000 temperature sensor plus an encoder function for blade positioning (locks the propeller at a specified stop position; requires compatible ESC firmware).

Key Features

  • Rated thrust: 110 kg; Peak thrust: 226.3 kg
  • Recommended takeoff weight: 110 kg
  • Lithium compatible: 96S (Lipo)
  • Efficiency (combo): 5.7 gf/W
  • Operating temperature (combo): -20~50°C
  • IP degree (combo): IP45
  • Motor weight (design): 10.75 kg
  • Torque boost: 15%
  • Motor construction notes: 220°C high-temp resistant copper windings; UH arc magnets; Japan bearings; vacuum-sealed coils; real-time temperature monitoring
  • ESC control and comms: dual CAN/PWM throttle support; communication interface CAN*2 (CAN2.0B, 1M bps)
  • ESC system notes: DSP chip (automotive-grade); FOC adaptive algorithm; 0.28 s dynamic response; 3rd-gen SiC MOSFETs (15% improved efficiency); easy tuning & OTA updates; overload protection + voltage monitoring + stall auto-recovery; ±1% current precision
  • Validation notes: 1,000-hour endurance testing; -40°C to 85°C thermal cycling (48H); salt spray corrosion resistance test (48H); IP45 waterproof test

For kit selection, encoder/firmware compatibility, or integration questions, contact https://rcdrone.top/ or support@rcdrone.top.

Specifications

Combo (AM110-Kit)

Model AM110-Kit
Max thrust 226.3 kg
Recommended takeoff weight 110 kg
Lithium compatible 96S (Lipo)
Efficiency 5.7 gf/W
Operating temperature -20~50°C
IP degree IP45
Weight 14650±100 g
Power cable / length 8AWG / 680 mm
Signal wire 9pin / 1230 mm

Motor (AM110)

Model AM110
KV 9 KV
Slot & pole 36N42P
Motor size D: 196.8 x 144.8 mm
Cable length 250 mm (Extended Enameled Wires)
Weight 10.75 kg

ESC (SineSic 160A Pro)

Model SineSic 160A Pro (200V~435V)
Size 212.5*120*68 mm
Weight 2714 g
Degree of protection IPX7
Continuous output current 160A
Peak output current 280A (10S)
PWM input pulse width 1100~1900us
Communication interface CAN*2 (CAN2.0B, 1M bps)

Propeller (FLUXER PRO 73X29" PROP)

Model FLUXER PRO 73X29" PROP
Material of props High quality carbon fiber + resin
Mounting dimensions D25–D75 (M8*6), centre hole D25
Weight 1196±50 g

Curve Chart (Test Condition Note)

  • Chart title: AeroMax 110 kit Curve chart
  • Analytical Graph of Motor Operation: I = Current, P = Input Power, η = Electrical Efficiency, T = Thrust, N = Rotational Speed
  • Measured with an input voltage of 400 V, at a temperature of 25°C and sea level; rotational speed adjusted by the throttle
  • System label: AeroMax 110 9KV + FLUXER PRO 73X29" PROP + SineSic 160A Pro (200V~435V)

Kit Test Data (355V)

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (Nxm) RPM (RPM) Thrust (kgf) Efficiency (%) Efficiency (gf/W)
30 355.50 12.40 4408.9 3971.0 32.000 1185 38.4 90.07 8.7
35 355.22 18.44 6551.2 5847.8 41.730 1338 51.3 89.26 7.8
40 354.97 25.34 8995.6 8126.6 51.770 1499 65.0 90.34 7.2
45 354.82 32.96 11693.7 10645.0 61.660 1649 76.5 91.03 6.5
50 354.58 43.69 15491.8 14120.7 75.450 1787 92.2 91.15 6.0
55 354.36 53.35 18906.6 17246.8 85.850 1918 107.0 91.22 5.7
60 353.83 65.05 23015.8 21014.3 98.470 2038 123.7 91.30 5.4
65 353.58 75.84 26815.7 24412.4 108.590 2147 134.5 91.04 5.0
70 353.42 88.16 31158.1 28068.4 119.690 2239 149.1 90.08 4.8
75 352.83 101.56 35834.9 32290.8 131.230 2350 162.9 90.11 4.5
80 353.14 115.10 40645.1 36340.9 142.130 2442 176.4 89.41 4.3
85 352.66 129.26 45585.2 40541.8 153.270 2526 188.7 88.94 4.1
90 352.42 144.23 50831.2 44772.7 164.000 2607 201.0 88.08 4.0
95 352.23 160.19 56425.3 48751.2 175.560 2682 212.9 86.40 3.8
100 351.90 161.77 56927.6 49180.0 174.023 2689 214.2 86.39 3.8

Kit Test Data (400V)

Throttle (%) Voltage (V) Current (A) Input Power (W) Output Power (W) Torque (Nxm) RPM (RPM) Thrust (kgf) Efficiency (%) Efficiency (gf/W)
30 400.50 11.68 4676.2 4061.4 33.480 1158 41.7 86.85 8.9
35 400.20 17.32 6932.7 6145.5 43.870 1338 55.0 88.65 7.9
40 399.80 24.07 9623.2 8646.6 55.090 1499 68.3 89.85 7.1
45 399.38 31.46 12564.4 11386.7 65.960 1649 82.9 90.63 6.6
50 398.90 40.06 15980.3 14519.7 77.490 1789 96.7 90.86 6.1
55 399.10 49.17 19622.9 17842.6 88.750 1920 110.8 90.93 5.6
60 398.63 58.65 23380.2 21231.2 99.540 2037 124.2 90.81 5.3
65 398.49 69.42 27661.9 25060.0 111.470 2147 138.9 90.59 5.0
70 398.24 79.32 31589.1 28417.2 120.870 2245 150.1 89.96 4.8
75 397.97 91.36 36358.9 32695.6 132.770 2352 164.2 89.93 4.5
80 397.65 105.24 41849.7 37286.5 145.950 2440 178.3 89.10 4.3
85 397.67 115.17 45800.0 40578.9 153.620 2522 190.6 88.60 4.2
90 397.19 127.99 50837.7 44770.0 163.990 2607 203.7 88.07 4.0
95 396.57 143.27 56815.1 49371.6 175.650 2684 214.4 86.90 3.8
100 396.00 159.94 63337.0 54175.6 188.260 2748 226.3 85.54 3.6

Mechanical Dimensions (Additional Drawings)

  • Motor dimension callouts: Ø80–M6*6; Ø75–M8*6; Ø50–M6*6; motor three-phase line output 250 mm; encoder and thermal output 450 mm±10 mm
  • Propeller dimension callouts: 1854.2; 6–60°; 6–Ø8.2; Ø25; Ø75; 35.4±0.02

ESC Line Sequence / Interfaces (Diagram Labels)

  • Three-phase outputs: Output A, Output B, Output C
  • Power leads: Red V+, Black V-
  • Functions labeled: Blade positioning / Temperature monitoring; LED light interface
Signal Wire color
GND Blue
CAN1 Green
GND Yellow
CAN1 Black
CAN2_Yel Yellow
CAN2_Gre Green
CAN2_Org Orange
12V-A Output Red
GND Black
PWM Input White

What’s Included

  • Motor x 1 pc
  • ESC x 1 pc
  • Propeller x 1 pc

Applications

  • Heavy-lift multirotor propulsion (matched motor + ESC + prop set)
  • Drone delivery and logistics
  • Aerial mapping and surveying
  • Public-safety support and industrial operations requiring high thrust-to-weight propulsion

Details