SPIDER Automation | A2212 13T 1000KV Brushless DC Motor | 2S–3S LiPo & Multirotor Propulsion
Description
The SPIDER Automation A2212 13T 1000KV Brushless DC Motor is designed for brushless propulsion systems used in multirotors, quadcopters and compatible radio-controlled aircraft. Its A2212 13T model configuration and 1000KV rating provide a defined motor specification for selecting compatible batteries, ESCs and propeller combinations.
The motor is specified for 2S–3S LiPo battery systems, with a listed current-handling capacity of 12A. Its electrical specifications include a 500mA no-load current, a 4–10A maximum-efficiency current range and a stated maximum efficiency of 80%. These values provide useful reference points when designing and evaluating a compatible propulsion system.
This motor is supplied without pre-soldered connectors, allowing the installer to select suitable connector types and wiring arrangements for the intended ESC. The package includes one A2212 13T 1000KV brushless motor. Verify the shaft dimensions, mounting arrangement and propeller adapter compatibility before installation.
Key Features
- A2212 13T Configuration: Brushless motor model designation for compatible aircraft propulsion applications.
- 1000KV Motor Rating: Nominal speed constant of 1000 RPM per volt under no-load theoretical conditions.
- 2S–3S LiPo Compatibility: Specified for 2-cell and 3-cell LiPo battery configurations.
- 12A Current-Handling Capacity: Listed current capacity for electrical-system and ESC selection.
- 500mA No-Load Current: Specified current consumption under no-load conditions.
- 4–10A Efficiency Operating Range: Listed current range associated with maximum-efficiency operation.
- 80% Maximum Efficiency: Stated maximum motor efficiency rating.
- Customisable Connector Installation: Supplied without pre-soldered connectors for flexible ESC connection arrangements.
- Compact A2212 Motor Format: Intended for compatible multirotor and RC aircraft installations.
Electrical Configuration & Performance Characteristics
The motor’s 1000KV rating represents its nominal rotational speed constant in revolutions per minute per volt. It is not a guaranteed loaded operating RPM. Actual motor speed depends on battery voltage, propeller loading, ESC operation and the overall propulsion configuration.
The supplied electrical specifications include a 12A current-handling capacity, a 500mA no-load current and a 4–10A maximum-efficiency current range. The listed maximum efficiency is 80%. These figures should be considered when selecting the ESC, battery and wiring. The 12A current specification should not be interpreted as a verified continuous rating unless its operating conditions are confirmed.
The motor is specified for 2S–3S LiPo batteries. Propeller selection should be based on measured current consumption and motor temperature under the intended battery voltage and operating load. No specific propeller size, thrust output or maximum power rating is supplied.
Connector & Wiring Configuration
This motor is supplied without pre-soldered connectors. This allows the installer to select suitable motor connectors according to the ESC output leads and the electrical requirements of the aircraft.
- Connector Status: No pre-soldered connectors supplied.
- Connector Selection: Select compatible connectors based on the ESC motor-output interface.
- Connection Method: Connector installation and soldering are required according to the selected wiring arrangement.
- Motor Control: Requires a compatible brushless electronic speed controller.
Ensure all three motor phase connections are properly insulated and mechanically secure. Confirm motor rotation direction during testing with the propeller removed before completing the aircraft assembly.
Mechanical Design & Installation
The A2212 13T motor is intended for installation in compatible brushless aircraft propulsion assemblies. The supplied dimensional information lists a length of 40mm and a width of 30mm. However, the exact measurement reference and mounting-hole arrangement are not provided.
The source also lists a 13mm shaft diameter. This value requires physical verification before selecting a propeller adapter or mounting hardware, as the shaft specification may contain a data-entry error. Confirm the actual shaft diameter and usable shaft length against the motor in hand before installation.
Applications
The A2212 13T 1000KV motor is intended for compatible brushless aircraft propulsion systems. Potential applications include:
- Quadcopters: Four-motor aircraft configurations designed around compatible A2212 brushless motors.
- Multirotors: Multi-motor aircraft propulsion systems using suitable ESCs and propellers.
- RC Drones: Radio-controlled drone platforms with compatible 2S–3S brushless propulsion systems.
- RC Aircraft: Fixed-wing radio-controlled aircraft where the motor’s electrical and mechanical specifications meet the design requirements.
- UAV Propulsion Systems: Unmanned aircraft configurations using compatible brushless motor and ESC combinations.
- 2S LiPo Aircraft Builds: Propulsion setups designed around a compatible 2-cell LiPo supply.
- 3S LiPo Aircraft Builds: Brushless propulsion arrangements designed for a compatible 3-cell LiPo battery.
- Brushless Motor Integration: Engineering projects involving motor, ESC, battery and connector selection.
- Multirotor Maintenance: Replacement motor installations in aircraft designed for compatible A2212 motor specifications.
- Propulsion System Evaluation: Testing motor current, no-load behaviour and efficiency under suitable operating conditions.
- Flight-Control System Projects: Aircraft builds using flight controllers and ESCs compatible with brushless motor propulsion.
Package Includes
- 1 × A2212 13T 1000KV BLDC Brushless DC Motor
Product Specifications
| Parameter | Specification |
|---|---|
| Product Type | Brushless DC Motor |
| Motor Model | A2212 13T |
| Motor Technology | Brushless DC (BLDC) |
| Motor KV Rating | 1000KV |
| Speed Constant | 1000 RPM/V (nominal no-load speed constant) |
| Motor Configuration | 13T (model designation) |
| Compatible Battery Chemistry | LiPo (Lithium Polymer) |
| Compatible Battery Configuration | 2S–3S LiPo |
| Current-Handling Capacity | 12A (rating type not further defined) |
| No-Load Current | 500mA |
| Maximum-Efficiency Current Range | 4–10A |
| Maximum Efficiency | 80% |
| Motor Length | 40mm (listed dimension) |
| Motor Width | 30mm (listed dimension) |
| Shaft Diameter | Source-listed as 13mm; verify before selecting mounting hardware |
| Connector Status | No Pre-Soldered Connectors |
| Connector Configuration | Custom Connector Installation Required |
| ESC Compatibility | Compatible Brushless ESC Required; Specific ESC Rating Not Supplied |
| Intended Aircraft Types | Drones, Quadcopters, Multirotors, RC Airplanes and UAV Platforms |
| Package Quantity | 1 Motor |
Installation & Operating Recommendations
- Battery Selection: Use a compatible 2S–3S LiPo battery and verify the fully charged battery voltage against the motor and ESC operating limits.
- ESC Selection: Select a brushless ESC with an appropriate current rating and support for the intended battery cell count. The source does not provide a specific ESC rating.
- Current Monitoring: Check actual current draw under the selected propeller load and keep operation within verified motor and ESC limits.
- Connector Installation: Fit connectors compatible with the ESC motor leads and ensure all soldered joints are mechanically secure and properly insulated.
- Shaft Verification: Physically measure the motor shaft before selecting a propeller adapter. Do not rely on the source-listed 13mm shaft value without confirmation.
- Mounting Compatibility: Confirm the mounting-hole pattern, screw length and frame clearance before installation.
- Propeller Selection: Select a propeller only after checking motor current, operating voltage, ESC capability and available frame clearance.
- Rotation Testing: Check motor rotation with the propeller removed. If necessary, reverse rotation by exchanging any two of the three motor phase connections, following ESC instructions.
- Thermal Monitoring: Monitor motor and ESC temperatures during controlled testing, particularly when evaluating propeller loads.
- Propeller Safety: Keep propellers removed during wiring, configuration and initial motor tests.
