Product overview
The HOBBYWING C6225 is presented as a propulsion motor for fixed-wing cruise and VTOL applications, with C6225-200KV identified in the specification. The procurement scope established is a motor component. The recommended installation combines a 20×10 or 21×10 propeller, an XRotor Pro H130A 14S BLDC IPC ESC and a 12S LiPo battery. Its accompanying 20–25 kg takeoff-weight recommendation is expressly stated for a single motor, so it should retain that qualification in procurement documentation.
Installation planning can use the published 69 mm diameter, 50.9 mm height and 530 g weight including wires. The motor mounts through four M4 positions on a 36 mm diameter, while the propeller interface offers four M3 positions on a 20 mm diameter and four M4 positions on a 23 mm diameter. Direct enameled-wire leads are specified, with 100 mm three-phase wires and a 130 mm magnetic encoder cable. Internally, the motor uses three bearings, and its shaft end is retained by copper washers, circlips and screws.
The upper and lower steel mesh is described as preventing entry of particles at least 1 mm in diameter, alongside a published IPX5 protection level. Rotor-bracket clearance is intended to accommodate folding and non-folding propeller roots, while the stator base supports an IPC component. Configurable propeller stopping position depends on pairing with an IPC ESC. Electrical assessment should distinguish the 580 W maximum-continuous output rating from the 86 A maximum-current value, qualified by a non-hermetic environment at ≤25°C. Thrust ratings require 48 V and a 21×10 propeller; separate load tables remain laboratory reference data.
Specifications
| Specification | Value & conditions |
|---|---|
| Model variant | C6225-200KV |
| Protection level | IPX5 |
| Motor dimensions | Diameter 69 mm × height 50.9 mm |
| Slots and poles | 24N28P |
| Stator dimensions | 62 × 25 mm |
| Dynamic balance | ≤15 mg |
| Stator construction and treatment | High-standard silicon steel sheet; rust-proof treatment; paint coating with 180°C temperature resistance |
| Bearing specification | Waterproof bearing |
| Enameled wire temperature rating | 220°CPublished wire-material temperature rating. |
| Motor axle diameter | 10 mm |
| Magnet temperature rating | 160°CPublished magnet-material temperature rating. |
| Propeller mounting dimensions | 4 × M3 on diameter 20 mm and 4 × M4 on diameter 23 mm |
| Insulation test | 500 V AC high-voltage resistance test |
| Motor mounting dimensions | 4 × M4 on diameter 36 mm |
| Rated output power | 580 W maximum continuousThe specification labels rated output power as maximum continuous. |
| KV rating | 200KV |
| Battery specification | 12S LiPo (48 V)Published electrical configuration specifies 12S LiPo at 48 V. |
| No-load current | 3.4 A |
| Maximum current | 86 ANon-hermetic environment with ambient temperature ≤25°C. |
| Rated thrust | 4.5 kg48 V with a 21×10 propeller. |
| Maximum thrust | 14.8 kg48 V with a 21×10 propeller; published maximum-thrust value. |
| Resistance | 23.5 mΩ |
| Wire lead-out specification | Direct lead-out of enameled wireThe wire-size field specifies lead-out construction without stating a conductor gauge. |
| Three-phase wire length | 100 mm |
| Magnetic encoder cable length | 130 mm |
| Motor weight | 530 g with wiresPublished weight includes wires. |
| Recommended integration configuration | C6225-200KV motor; 20×10 or 21×10 propeller; XRotor Pro H130A 14S BLDC IPC ESC; 12S LiPo battery; recommended single-motor takeoff weight 20–25 kgRecommended application combination; inclusion of the propeller, ESC and battery is not established. The takeoff-weight range is explicitly labeled per single motor. |
| Product purpose and hardware category | UAV propulsion motor for fixed-wing and VTOL applicationsMotor application. |
| Physical architecture and integration features | Upper and lower steel mesh described as blocking particles ≥1 mm; IPC-compatible stator base; rotor-bracket boss clearance for folding and non-folding propeller roots; shaft retention with copper washers, circlips and screws; triple-bearing architectureConstruction. Adjustable propeller stopping position requires an IPC ESC; confirm propeller fit and mounting for the selected installation. |
| Load-table measurement qualifications | HOBBYWING Laboratory load-performance measurements are reference values subject to the published environmental, throttle and temperature-measurement conditionsLaboratory reference data measured at 25°C and sea level with varying throttle input. Where stated, motor temperature follows a ten-minute run at 90% throttle. |
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