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MAD X4229 IPE V1.0 Short Shaft eVTOL Airplane Drone Motor, IP35, 230KV/420KV Options

MAD X4229 IPE V1.0 Short Shaft eVTOL Airplane Drone Motor, IP35, 230KV/420KV Options

MAD

$163.50 USD
$163.50 USD
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Overview

MAD X4229 IPE V1.0 (short shaft) is an eVTOL airplane drone motor designed for efficient endurance operation, with IP35 protection and anticorrosive stator construction. Two KV options are provided: 230KV (12S LiPo nominal) and 420KV (6S LiPo nominal).

Key Features

  • IP35 degree of protection
  • Anticorrosive stator; varnished wire degree 180°C; magnet degree 150°C
  • Centrifugal heat dissipation: YES
  • Rotor balance: ≤5 mg; motor balance: ≤10 mg
  • Propeller mounting: D:20 M3×4 / M8 nut

Specifications

Motor Data (Common)

Motor model MAD X4229 IPE V1.0 (short shaft)
Number of pole pairs 7
Stator TAIWAN / Anticorrosive
Varnished wire degree 180°C
Motor size D:50 × 60.5 mm
Magnet degree 150°C
Degree of protection IP35
Cable length 110 mm 14# Awg(Black) silicone
Centrifugal heat dissipation YES
Rotor balance ≤5 mg
Propeller mounting holes D:20 M3×4 / M8 Nut
Motor balance ≤10 mg
Shaft diameter IN: 6 mm
Motor mounting holes D:30 M4×4, D:56 M4×4, D:60 M4×4
Bearing EZO 686ZZ *2 / EZO 696ZZ
Disruptive test 500 V

230KV Option

  • Recommended hover thrust: 2.5~4.0 kgf
  • Maximum thrust: 8.3 kgf
  • Optimized weight: 393 g
  • Efficiency: >81%
RPM/V 230 KV Nominal voltage 12S lipo battery
No load current 1.2A/25V Internal resistance 42.5mΩ
Motor weight 393 g Product boxed weight 645g (110 x 110 x 95 mm)
Maximum current 53.4 A Maximum power 2233W
Maximum thrust 8.3 kg Maximum torque 2.1 Nm
Recommended ESC MAD AMPX 80A (5-14S) Recommended propellers 16x8, 17x10, 18x8
UAV take-off weight 6S-18" 12kg--Quadcopter 18kg--Hexacopter 24kg--Octocopter Single rotor take-off weight 2.5kg ~4kg

420KV Option

  • Recommended hover thrust: 2.5~4.0 kgf
  • Maximum thrust: 7.8 kgf
  • Optimized weight: 393 g
  • Efficiency: >80%
RPM/V 420 KV Nominal voltage 6S lipo battery
No load current 2.3A/20V Internal resistance 13.7mΩ
Motor weight 393 g Product boxed weight 645g (110 x 110 x 95 mm)
Maximum current 85.9 A Maximum power 2049W
Maximum thrust 7.8 kg Maximum torque 1.9 Nm
Recommended ESC MAD AMPX 80A (5-14S) Recommended propellers 17x10, 18x8
UAV take-off weight 6.5-18" 12kg--Quadcopter 18kg--Hexacopter 24kg--Octocopter Single rotor take-off weight 2.5kg ~4kg

Performance Data

Maximum thrust may depend on battery level, propeller type, air pressure and other conditions.

230KV (12S) Measurement Notes

The data were measured with an input voltage of 48 V, at a temperature of 25°C and sea level. The rotational speed was adjusted by the throttle.

230KV + APC 16x8 + AMPX 80A (5-14S) (12S, MAX 91°C)

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N*m] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 44.62 1.46 65.1 43.7 0.143 2920 671 67.1 10.3
35 44.58 2.17 96.7 70.5 0.196 3434 926 72.9 9.6
40 44.58 2.98 132.8 102.2 0.254 3844 1189 77 9.0
45 44.56 3.88 172.9 136.0 0.306 4245 1444 78.7 8.4
50 44.53 5.28 235.1 189.9 0.385 4710 1811 80.8 7.7
55 44.5 7.13 317.3 261.6 0.478 5226 2227 82.4 7.0
60 44.46 9.09 404.1 337.6 0.568 5676 2633 83.5 6.5
65 44.4 11.34 503.5 424.5 0.666 6086 3070 84.3 6.1
70 44.34 14.02 621.6 530.8 0.786 6449 3558 85.4 5.7
75 44.29 16.98 752.0 644.2 0.901 6828 4022 85.7 5.3
80 44.22 20.2 893.2 764.6 1.010 7229 4495 85.6 5.0
85 44.14 23.97 1058.0 901.7 1.133 7600 4922 85.2 4.7
90 44.04 28.58 1258.7 1071.2 1.284 7967 5480 85.1 4.4
95 43.93 33.78 1484.0 1253.5 1.441 8307 5739 84.5 3.9
100 43.79 40.01 1752.0 1471.4 1.630 8620 6234 84 3.6

230KV + APC 17x10 + AMPX 80A (5-14S) (12S, MAX 103°C)

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N*m] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 44.6 2.02 90.1 64.9 0.218 2841 909 72 10.1
35 44.57 3.11 138.6 105.8 0.302 3345 1276 76.3 9.2
40 44.56 4.26 189.8 149.2 0.380 3750 1589 78.6 8.4
45 44.52 5.61 249.8 201.2 0.465 4131 1932 80.5 7.7
50 44.48 7.54 335.4 275.9 0.578 4559 2364 82.3 7.0
55 44.43 10.28 456.7 379.2 0.721 5022 2963 83 6.5
60 44.37 12.98 575.9 480.2 0.841 5452 3444 83.4 6.0
65 44.32 15.8 700.3 580.9 0.952 5827 3887 83 5.6
70 44.24 19.16 847.6 703.2 1.088 6172 4386 83 5.2
75 44.16 23.08 1019.2 848.0 1.242 6520 4933 83.2 4.8
80 44.07 27.21 1199.1 990.1 1.375 6876 5351 82.6 4.5
85 43.95 32.72 1438.0 1178.3 1.570 7167 5722 81.9 4.0
90 43.82 39.06 1711.6 1380.1 1.761 7484 6007 80.6 3.5
95 43.68 45.67 1994.9 1588.9 1.949 7785 6527 79.6 3.3
100 43.51 53.39 2323.0 1817.4 2.149 8076 7035 78.2 3.0

230KV + APC 18x8 + AMPX 80A (5-14S) (12S, MAX 121°C)

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N*m] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 44.6 1.96 87.4 62.5 0.210 2840 948 71.5 10.8
35 44.58 2.99 133.3 102.3 0.292 3347 1326 76.7 10.0
40 44.57 4.1 182.7 145.3 0.370 3749 1689 79.5 9.2
45 44.53 5.41 240.9 195.1 0.451 4130 2060 81 8.6
50 44.5 7.28 324.0 268.5 0.561 4570 2542 82.9 7.8
55 44.44 9.9 440.0 367.5 0.696 5045 3157 83.6 7.2
60 44.38 12.69 563.2 475.4 0.830 5470 3719 84.4 6.6
65 44.31 15.79 699.7 593.3 0.972 5829 4310 84.8 6.2
70 44.23 19.11 845.2 715.1 1.105 6180 4898 84.6 5.8
75 44.16 22.75 1004.6 845.3 1.235 6536 5452 84.1 5.4
80 44.06 26.9 1185.2 991.9 1.374 6894 5996 83.7 5.1
85 43.98 31.24 1373.9 1137.9 1.499 7249 6517 82.8 4.7
90 43.87 36.67 1608.7 1325.2 1.668 7587 7172 82.4 4.5
95 43.72 43.33 1894.4 1539.4 1.865 7882 7951 81.4 4.2
100 43.57 50.47 2199.0 1755.6 2.050 8178 8257 79.8 3.8

The above data are the theoretical values when the input voltage is 48V, for reference only. In the case of room temperature of 25°C and no additional cooling device, the current over 50A is non-working zone, 16-50A is short-term (about 10-30s) working zone, and below 16A is sustainable working zone. In actual use, control the motor running time according to the working environment temperature and heat dissipation conditions.

420KV (6S) Measurement Notes

The data were measured with an input voltage of 24 V, at a temperature of 25°C and sea level. The rotational speed was adjusted by the throttle.

420KV + APC 16x8 + AMPX 80A (5-14S) (6S, MAX 99°C)

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N*m] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 25.46 3 76.3 46.2 0.147 2994 644 61.83 8.6
35 25.45 4.17 106.1 70.1 0.197 3407 875 67.44 8.4
40 25.39 5.96 151.3 110.0 0.268 3917 1218 73.94 8.2
45 25.34 7.9 200.2 153.6 0.338 4339 1566 77.89 7.9
50 25.31 9.98 252.5 198.5 0.402 4715 1888 79.6 7.5
55 25.3 12.56 317.7 254.2 0.477 5086 2197 80.98 7.0
60 25.24 16.15 407.5 330.9 0.570 5542 2604 81.99 6.5
65 25.07 20.3 509.0 418.2 0.670 5954 3030 82.41 6.0
70 25.05 25.12 629.4 516.3 0.775 6362 3495 83 5.6
75 25 30.43 760.7 619.5 0.881 6713 3937 82.39 5.2
80 24.88 35.67 887.3 723.1 0.981 7036 4344 84.49 5.1
85 24.79 41.47 1028.2 834.9 1.085 7348 4763 83.87 4.8
90 24.6 48.37 1189.9 962.4 1.202 7645 5208 82.89 4.5
95 24.54 55.81 1369.3 1095.4 1.319 7930 5644 81.77 4.2
100 24.26 66.57 1615.3 1278.6 1.475 8279 6182 80 3.9

420KV + APC 17x10 + AMPX 80A (5-14S) (6S, MAX 108°C)

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N*m] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 25.46 3.91 99.4 67.6 0.224 2882 831 69.37 8.5
35 25.43 5.45 138.5 100.1 0.292 3278 1127 73.71 8.3
40 25.38 8 203.0 156.4 0.397 3766 1597 78.28 8.0
45 25.33 10.92 276.7 217.4 0.495 4195 2013 79.73 7.4
50 25.29 13.93 352.2 281.5 0.591 4549 2398 80.86 6.9
55 25.21 17.56 442.8 355.3 0.692 4905 2810 80.97 6.4
60 25.13 22.23 558.5 450.7 0.813 5295 3281 81.11 5.9
65 24.94 27.8 693.2 561.3 0.949 5647 3806 83.6 5.7
70 24.91 33.59 836.8 673.1 1.070 6005 4264 83.51 5.3
75 24.79 40.36 1000.5 798.8 1.206 6324 4791 82.45 4.9
80 24.68 47.1 1162.4 919.3 1.328 6613 5209 81.32 4.6
85 24.53 54.32 1332.4 1041.9 1.448 6872 5641 79.89 4.3
90 24.35 63.11 1536.8 1187.7 1.559 7094 5945 78.39 3.9
95 24.18 72.5 1753.1 1332.6 1.742 7304 6154 76.56 3.5
100 23.92 85.65 2048.8 1534.6 1.934 7577 6411 77.9 3.3

420KV + APC 18x8 + AMPX 80A (5-14S) (6S, MAX 118°C)

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [N*m] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 25.47 3.89 99.0 67.2 0.222 2892 966 69.31 10.0
35 25.44 5.41 137.5 99.5 0.289 3284 1275 73.75 9.5
40 25.39 7.84 199.1 152.6 0.386 3775 1710 77.95 8.7
45 25.34 10.77 272.9 214.7 0.488 4204 2173 79.83 8.1
50 25.29 13.66 345.5 275.8 0.577 4555 2541 81.01 7.4
55 25.23 17.18 433.4 348.0 0.675 4924 2977 81.05 6.9
60 25.15 21.79 548.2 442.9 0.796 5313 3503 81.31 6.4
65 25.05 27.05 677.4 549.0 0.923 5680 4014 81.19 6.0
70 24.94 33.01 823.3 663.3 1.049 6038 4566 83.74 5.8
75 24.8 39.72 985.1 790.1 1.186 6359 5148 82.86 5.4
80 24.69 46.34 1144.2 910.3 1.308 6646 5624 82.84 5.1
85 24.57 53.46 1313.8 1031.6 1.425 6913 6103 80.38 4.8
90 24.41 61.32 1496.9 1165.2 1.553 7156 6644 79.16 4.5
95 24.25 69.93 1695.7 1300.1 1.676 7406 7141 77.45 4.3
100 23.99 82.16 1971.1 1488.6 1.845 7704 7704 80 4.0

The above data are the theoretical values when the input voltage is 24V, for reference only. In the case of room temperature of 25°C and no additional cooling device, the current over 82A is non-working zone, 27-82A is short-term (about 10-30s) working zone, and below 27A is sustainable working zone. In actual use, control the motor running time according to the working environment temperature and heat dissipation conditions.

What's Included

  • Motor x1
  • Prop Adaper x1
  • Propeller Plate x1
  • Cross Grating x1
  • Support Rod x1
  • 4.0mm Bullet Connector x3
  • Heat Shrinkable Tube x3
  • M4*10 Motor Screws x4
  • M3*8 Prop Adaper Screws x4
  • M4*10 Countersunk Head Bracket Screw x4
  • M3 Machine Screw x1
  • M8 Nut x1
  • Sticker x2

Support

For compatibility checks (propeller/ESC/battery) and order support, contact https://rcdrone.top/ or email support@rcdrone.top.

Details

MAD X4229 (short shaft) eVTOL Airplane Drone Motor

The MAD X4229 short-shaft motor layout includes detailed overall dimensions and mounting-hole spacing to help plan fitment and hardware.

MAD X4229 (short shaft) eVTOL Airplane Drone Motor

The MAD X4229 IPE V1.0 motor package includes a prop adapter and plate, mounting hardware, and 4.0mm bullet connectors with heat-shrink tubing for wiring.

MAD X4229 (short shaft) eVTOL Airplane Drone Motor

The MAD X4229 IPE V1.0 short-shaft motor is listed at 230KV, 393 g weight, >81% efficiency, and up to 12S input in the provided performance data.

MAD X4229 (short shaft) eVTOL Airplane Drone Motor

MAD X4229 IPE V1.0 short shaft motor documentation includes dimensioned mounting layouts and a 12S performance table for 230KV and 420KV variants.

MAD X4229 (short shaft) eVTOL Airplane Drone Motor

The MAD X4229 IPE short shaft motor data lists throttle vs voltage, current, RPM, thrust, power, torque, and efficiency, with 12S noted as the max setup.

MAD X4229 (short shaft) eVTOL Airplane Drone Motor

The X4229 short shaft motor spec sheet lists a 420KV option with max power up to 3939W and efficiency noted above 80%.

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