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T-MOTOR MN1325 KV47 UAV motor

By T-MOTOR ↗

The T-MOTOR MN1325 KV47 is a heavy-lift UAV propulsion motor intended for multirotor integration. Its published configuration combines a 24S LiPo rating with a Φ150*61mm motor envelope. Recommended combination: an ESC and propeller pairing and lists customization options; published thrust and bench-performance figures require configuration confirmation and retain reference-only qualifications.

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T-MOTOR MN1325 KV47 UAV motor with a silver face and black housing.
T-MOTOR MN1325 KV47 UAV motor with a silver face and black housing.
Model numberMN1325
Motor sizeΦ150*61mm
Stator technology150℃ high-temperature-resisting coatingsCoating temperature-resistance specification; not the motor operating-temperature range.
Copper wire220℃ high temperature resistanceWire temperature-resistance specification; not the motor operating-temperature range.
Magnet level180℃ high temperature resistanceMagnet temperature-resistance specification; not the motor operating-temperature range.
Coil insulation test1000V withstand voltage testPublished coil insulation test voltage.

Product overview

The T-MOTOR MN1325 KV47 is a propulsion motor for heavy-lift UAV integration. Its silver-and-black design is presented for four-, six- and eight-rotor multirotors, together with coaxial arrangements. The identified product configuration is the MN1325 motor with a KV value of 47. It lists the M200A24S ESC and NS47 x18 propeller as a recommended combination, so procurement should distinguish the motor configuration from those separately identified integration components.

Mechanical integration centres on a published Φ150*61mm motor envelope and a 2425g motor weight including cable. The construction specification lists a 36N42P configuration, imported 6004ZZ bearing and 150mm enameled-wire leads. A slash occupies the output-shaft diameter field, leaving that interface dimension unspecified. Custom hole patterns and cable lengths are listed alongside coating, logo, KV and temperature-sensor options. These options provide scope for adapting the installation.

Electrical selection should retain the stated 24S LiPo rating, 170A peak current and 3400W maximum-power rating qualified by 180 seconds. Higher power figures in its reference-only bench table, leaving a discrepancy to resolve for the selected configuration. Rated thrust is 30~32kg per arm, with 68kg maximum thrust published; these figures should retain the manufacturer's reference-data qualification. IP45 and a -30℃~55℃ operating range are listed, while the higher coating, wire and magnet temperature ratings describe individual components.

Specifications

SpecificationValue & conditions
Model numberMN1325
Motor sizeΦ150*61mm
Stator technology150℃ high-temperature-resisting coatingsCoating temperature-resistance specification; not the motor operating-temperature range.
Copper wire220℃ high temperature resistanceWire temperature-resistance specification; not the motor operating-temperature range.
Magnet level180℃ high temperature resistanceMagnet temperature-resistance specification; not the motor operating-temperature range.
Coil insulation test1000V withstand voltage testPublished coil insulation test voltage.
Ingress protectionIP45
Motor configuration36N42P
Rotor dynamic balance standard≤30mg
BearingImported 6004ZZ
Output shaft diameter/
Wire specification and lengthEnameled wire*150mm
KV value47
Idle current4.0APublished idle-current value at 20V.
Maximum power3400WPublished maximum-power rating for 180s; the separate test table reports higher input-power figures.
Internal resistance17.5mΩ
Rated voltage24SPublished LiPo battery configuration; also specified for the recommended combination.
Peak current170A
Maximum thrust68kgThis as maximum thrust per arm. Published bench data use MN1325 KV47 with NS47 x18 and are for reference only.
Package weight2990g
Recommended motorMN1325 KV47Listed motor in the recommended combination.
Recommended ESCM200A24SListed ESC in the recommended combination; inclusion with the motor is not established.
Recommended propellerNS47 x18Listed propeller in the recommended combination and bench-test configuration; inclusion with the motor is not established.
Motor weight2425gPublished motor weight includes the cable.
Rated thrust per arm30~32 kgPublished thrust per arm; confirm the selected propulsion configuration. Manufacturer bench data are for reference only.
Operating temperature-30℃~55℃Operating range; component temperature-resistance ratings are separate specifications.
MTBF≥2000 hoursReliability figure.
Product purpose and architectureSilver-and-black heavy-lift UAV motor; four-, six-, eight-rotor and coaxial multirotor layoutsMotor purpose and supported layout categories; no complete flight platform or airframe kit is established.
Customization optionsCustom coating, logo, temperature sensor, KV, hole pattern and cable lengthListed customization options.
Bench-data qualificationReference-only T-MOTOR bench data; motor surface temperature measured after 10 minutes at 80% throttleApplies to the manufacturer's published bench data. The table gives 105℃ at an ambient temperature of 25℃; the note defines motor temperature as surface temperature after 10 minutes at 80% throttle.
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