Hobbywing X8 Power System G2 Integrated Motor System

X8 G2 Propulsion System-D35 CAD X8 G2 Propulsion System-D40 CAD Product NameX8 G2 Propulsion System Specifications 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 and Props） Cable specification Operating temperature Ingress Protection Rated output power (Max continuous) Pinout DataLink Version X8 G2 17.5 kg (Sea level) 5~7.5kg (Sea level) 9.7~8.4 g/W 12S~14S（LiPo） 14S-54V / 12S-46V 18~63 V D35 / D40mm 1095 g* Power cable: 14AWG 905 mm* Signal cable: 915 mm* -20~50℃ IPX6 810 W Black-GND, White-PWM & Yellowe-GND, Gray-CH, Green-CL DataLinkBox G3 ESC specification Model Communication protocol Peak current （3 seconds） Continuous current Throttle travel calibration Double throttle signal Operating pulse width Failure storage & Log 80A-FOC Cyphal（UAVCAN） 80A（3s） 20 A Nonsupport PWM + CAN 1050~1950 μs Supported Motor specification Model Slot& Pole Stator diameter Motor diameter 8120-100KV 36N40P 81*20 mm 88.6 mm Propeller specification Model Total Weight Material of blades Single blade weight MFP 30x11S (Folding propeller) 193 g* Carbon fiber reinforced plastics 54.5 g* Optional Propeller specification Model Total Weight Material of blades Single blade weight MFP 30x11 (Folding propeller) 188 g* Carbon fibre-reinforced nylon composite material 51.6 g* *Subject to the actual product. Two types of propellers available, MFP 30x11S high speed propeller is mainly used. X8 G2-12S & MFP 30x11S Load performance parameters X8 G2-12S & MFP 30x11S Technical Parameters 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 30x11S / MFP 30x11 35% 2021 3.5 161.2 1571 12.5 0.74 121.7 / 39% 2472 4.4 204.0 1721 12.1 0.89 160.4 42% 2968 5.6 256.5 1877 11.6 1.06 208.3 45% 3493 6.9 317.3 2032 11.0 1.24 263.8 48% 3999 8.3 380.4 2171 10.5 1.41 320.5 51% 4476 9.6 443.5 2294 10.1 1.58 379.5 54% 4994 11.2 515.8 2419 9.7 1.76 445.8 57% 5456 12.7 583.9 2524 9.3 1.92 507.4 60% 6043 14.6 674.2 2650 9.0 2.12 588.3 63% 6452 16.1 740.0 2733 8.7 2.26 646.8 66% 6977 18.0 828.9 2836 8.4 2.45 727.6 69% 7951 21.8 1004.4 3017 7.9 2.79 881.4 72% 8500 24.1 1110.3 3115 7.7 2.99 975.3 75% 9050 26.5 1221.7 3212 7.4 3.18 1069.5 78% 10034 31.2 1434.5 3384 7.0 3.55 1257.9 81% 10467 33.3 1533.5 3459 6.8 3.71 1343.8 84% 11007 36.1 1660.6 3553 6.6 3.92 1458.4 87% 11548 38.9 1792.3 3646 6.4 4.13 1576.8 90% 12542 44.4 2042.8 3813 6.1 4.51 1800.7 100% 15006 57.7 2658.5 4132 5.6 5.35 2314.8 The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input adjustments. The test data of two types of propellers are the same. X8 G2-14S & MFP 30x11S Load performance parameters X8 G2-14S & MFP 30x11S Technical Parameters Voltage(V) Propeller Throttle(%) Thrust(g) Current(A) Power Input(W) Speed(RPM) Efficiency(g/W) Torque(N·m) Power Output(W) Temperature(℃) 54V(14S LiPo) MFP 30x11S / MFP 30x11 35% 4459 8.4 451.4 2250 9.9 1.58 372.3 / 39% 4965 9.7 524.4 2371 9.5 1.75 434.5 42% 6007 12.7 688.6 2602 8.7 2.12 577.6 45% 6450 14.1 763.2 2694 8.5 2.28 643.2 48% 7031 16.0 864.8 2810 8.1 2.48 729.7 51% 8026 19.4 1048.4 2995 7.7 2.83 887.5 54% 8552 21.3 1149.4 3088 7.4 3.02 976.5 57% 9509 24.8 1342.4 3248 7.1 3.35 1139.4 60% 10495 28.7 1552.8 3403 6.8 3.70 1318.4 63% 11062 31.1 1680.3 3489 6.6 3.89 1421.2 66% 12045 35.4 1912.8 3633 6.3 4.24 1613.0 69% 12992 39.9 2152.8 3766 6.0 4.57 1802.2 72% 13506 42.4 2290.0 3836 5.9 4.76 1912.0 75% 14456 47.3 2555.3 3962 5.7 5.10 2115.8 78% 14984 50.2 2710.3 4031 5.5 5.29 2232.9 81% 15544 53.3 2879.3 4101 5.4 5.49 2357.5 84% 16017 56.0 3025.6 4160 5.3 5.67 2469.9 87% 16518 59.0 3184.3 4219 5.2 5.85 2584.4 90% 17005 61.9 3340.3 4276 5.1 6.02 2695.6 100% 17464 64.7 3489.8 4326 5.0 6.18 2799.4 The above data was measured by HOBBYWING Laboratory at room temperature 25°C, at sea level, with varying throttle input adjustments. The test data of two types of propellers are the same.