Product overview
T-MOTOR positions the A6 as a propulsion module for agricultural multirotors, with recommendations covering a 5L liquid-load quadcopter and a 10L liquid-load hexacopter. The corresponding recommended aircraft take-off weights are 14–20kg and 21–30kg. Its published architecture combines an A6 motor, a FOC 80A electronic speed controller and an MF2311P propeller. Procurement should therefore treat the product as a propulsion assembly for aircraft integration; the listed configurations identify propulsion components rather than a complete flight platform or an airframe-only kit.
Mechanical integration centers on the published 30mm tube size, 1100±10mm wiring and a folding polymer propeller specified as MF2311P-M, measuring 23 inches (585mm) in length. The stated module weight is 695g ±2%, including wires and propeller. Power wiring is specified as red and black 14#AWG, with 5P Teflon signal wiring. A silicone protective cover has fluorescent orange and industrial gray options. Both a motor-and-ESC configuration and a configuration adding the MF2311P-M, making propeller inclusion a selection-dependent detail.
Electrical planning should account for the recommended 12–14S LiPo battery, 61V maximum voltage, PWM/CAN control and absence of a BEC. The ESC lists DRONE CAN, UAV CAN and CUBE CAN protocols, with a fixed 1100–1940µs throttle range. Its 80A peak-current figure applies only briefly in an open environment at temperature ≤60°C. Published thrust figures are 3.5–5kg rated and 12kg maximum. The laboratory table is reference-only and identifies a FOC 50A test setup, so its results require attention to configuration differences.
Specifications
| Specification | Value & conditions |
|---|---|
| Product identity | T-MOTOR A6 modular propulsion system |
| Intended application | Propulsion system for 5L agricultural quadcopters or 10L agricultural hexacoptersManufacturer recommendations for agricultural drone integration. |
| Recommended liquid load | Quadcopter: 5L; hexacopter: 10LRecommended liquid-load capacities for the respective aircraft layouts. |
| Recommended aircraft take-off weight | Quadcopter: 14–20kg; hexacopter: 21–30kgManufacturer-recommended aircraft take-off weights; not the weight or payload of the propulsion module. |
| Listed configurations | A6 KV180 + 14S FOC 80A; or A6 KV180 + 14S FOC 80A + MF2311P-MTwo selectable configurations; confirm whether the selected configuration includes the propeller. |
| System architecture | A6 motor + FOC 80A ESC + MF2311P propellersPublished system setup; the propeller specification separately names MF2311P-M. |
| Module model | A6 KV180 |
| Tube size | 30mm |
| Wire specification | Power wires: 14#AWG, red and black; signal wires: 5P Teflon |
| Recommended battery | 12–14S LiPoManufacturer-recommended battery specification. |
| Wire length | 1100±10mm |
| Rated thrust | 3.5–5kg |
| Weight | 695g ±2%, including wires and propellerIncludes wires and propeller, with the published ±2% tolerance. |
| Efficiency at rated thrust | 7.09g/W at 5kgPublished efficiency at 5kg rated thrust. |
| Ingress protection | IPX6 |
| Maximum thrust | 12kg |
| Recommended ambient temperature | −30 to 50°CManufacturer-recommended ambient temperature range. |
| Motor stator size | 62 × 15mm |
| Motor KV | 180 |
| ESC throttle range | 1100–1940µs, fixedFixed throttle range. |
| ESC maximum voltage | 61V |
| ESC protocols | DRONE CAN, UAV CAN, CUBE CAN |
| ESC peak current | 80AShort-duration peak current in an open environment at temperature ≤60°C. |
| Control method | PWM/CAN |
| BEC | No BEC |
| Propeller model and construction | MF2311P-M, polymer foldingPublished propeller specification; confirm inclusion in the selected configuration. |
| Propeller length | 23 inches (585mm)Published propeller length. |
| Protective cover options | Silicone protective cover; fluorescent orange or industrial gray |
| Reference test configuration | A6 KV180 + 54V + 14S FOC 50A + MF2311This is the configuration identified in the reference test table; it differs from the listed FOC 80A system setup. |
| Test-data qualification | Reference-only laboratory bench data; temperature measured at the motor bell after 2min at 80% throttleManufacturer laboratory bench-test data are reference values. Chart temperature means motor bell temperature after two minutes at 80% throttle. |
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