Product overview
HOBBYWING’s X9 Plus provides a motor, ESC and propeller propulsion configuration for UAV integration. The manufacturer lists agriculture, education and training, logistics, firefighting, surveying and inspection as intended applications. Its integrated motor-and-ESC assembly mounts to a circular carbon-fiber tube with a 40mm outer diameter. The published configuration pairs a 9620-100KV motor with an XRotor 150A-FOC ESC and MFP 36x19.0 composite propellers. Procurement should therefore treat it as a propulsion subsystem, rather than a complete flight platform or an airframe-only kit.
Installation planning should use the published 149.6 × 104 × 130.5mm assembly dimensions and 1760g weight, which includes cables and propellers, while confirming the selected configuration. The power cable is specified as 12AWG with a 1000±10mm length, and the signal line as 1090±20mm. Electrical integration must accommodate the 18-65V input range and specified 12S/14S LiPo configurations. The ESC uses UART, accepts a 1050-1950μs operating pulse width and has no BEC. Throttle travel calibration and dual throttle signals are listed as unsupported.
The current specification table gives 27kg maximum thrust, an 11-13kg recommended takeoff weight per axis and corresponding efficiency of 8.1-7.4g/W. These are configuration values, not guaranteed aircraft performance; the accompanying thrust tests specify 54V, MFP 36x19.0 propellers, 25°C and sea level. Continuous limits are 1700W rated output and 40A ESC current, while 150A is a three-second peak. The table specifies IPX6 for key parts despite conflicting descriptive protection claims. Operating-status integration is described, but the eight-channel DataLinkBox requires separate purchase.
Specifications
| Specification | Value & conditions |
|---|---|
| Product name | HOBBYWING X9 Plus |
| Maximum thrust | 27kgCurrent specification-table value; descriptive text elsewhere states 26.5kg. And operating conditions. |
| Recommended takeoff weight per axis | 11-13kgRecommended takeoff weight per propulsion axis, not a complete-aircraft payload rating. |
| Efficiency at recommended takeoff weight | 8.1-7.4g/WPublished efficiency for the recommended takeoff-weight range. The accompanying thrust-test data were measured at 25°C and sea level using 54V (14S LiPo) and MFP 36x19.0 propellers. |
| Input voltage | 18-65V |
| Rated voltage | 12S: 46V; 14S: 54VPublished rated voltages for the respective battery configurations. |
| Compatible lithium batteries | 12S/14S LiPoSpecified LiPo battery configurations. |
| Tube outer diameter | 40mmSpecified mounting-tube outer diameter. |
| System weight | 1760gIncludes cable and propellers. |
| Cable specification | Power cord: 12AWG × 1000±10mm; signal line: 1090±20mmPublished cable gauge, lengths and tolerances. |
| Operating temperature | -20 to 50°C |
| Ingress protection | Key parts: IPX6The specification table limits IPX6 to key parts. Descriptive passages contain conflicting overall IPX6 and IPX7 claims; confirm the protection scope. |
| Rated output power | 1700WMaximum continuous rated output power. |
| System size | 149.6 × 104 × 130.5mmDimensions; axis order is not stated. |
| Pinout | Black White—GND, PWM, GND; Black Red White—GND, 5V, PPublished pinout wording; confirm connector assignments before integration. |
| DataLink version | DataLink V2 |
| ESC model | XRotor 150A-FOC |
| Communication protocol | UARTESC communication protocol. |
| ESC peak current | 150A for 3sPeak current is qualified by a three-second duration. |
| ESC continuous current | 40APublished continuous ESC current. |
| Throttle travel calibration | Not supported |
| Dual throttle signal | Not supported |
| Operating pulse width | 1050-1950μsSpecified ESC operating pulse-width range. |
| BEC | NoneThe ESC is specified without a BEC. |
| Motor specification |
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| Propeller specification |
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| DataLink V2 telemetry hardware |
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| Product purpose | UAV propulsion system for agriculture, education and training, logistics, firefighting, surveying and inspectionManufacturer-listed applications; suitability for a particular aircraft and mission requires configuration confirmation. |
| Physical architecture | Integrated motor and ESC assembly for a 40mm circular carbon-fiber tubeIntegrated motor-and-ESC architecture with a specified circular carbon-fiber mounting tube; the product is a propulsion system rather than a complete flight platform or airframe-only kit. |
| Protection and data integration | Power-on self-test, abnormal-voltage, current and stall protection; operating-status output to a flight controller; separately purchased DataLinkBox supports simultaneous data collection from eight propulsion channelsFunctions. DataLinkBox must be purchased separately; confirm the flight-controller interface and selected configuration. |
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