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T-MOTOR Air Gear 355 (Quick-Release Version)

By T-MOTOR ↗

The T-MOTOR Air Gear 355 (Quick-Release Version) is a multirotor propulsion combo comprising AIR2213/KV1000 motors, MF9545 quick-release propellers and an AIR 20A four-in-one ESC. It supports recommended 3~4S LiPo operation and several multirotor layouts, with defined aircraft weight ranges, propeller operating limits and a 25% loss allowance for coaxial configurations.

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Product and propulsion configurationT-MOTOR Air Gear 355 (Quick-Release Version) propulsion combo
Component configurationAIR2213/KV1000 quick-release motor; MF9545 quick-release propeller; AIR 20A four-in-one ESC
Assembly architectureQuick-release structure with assembly markings
Overall combo weight reduction13%Motor, propeller and ESC combined.
Recommended thrust and aircraft takeoff weightsThrust per arm: 0.4~0.5 kg; quadcopter MTOW: 1.6~2.0 kg; hexacopter MTOW: 2.4~3.0 kg; non-coaxial octocopter takeoff weight: 3.2~4.0 kgRecommended multirotor configurations; octocopter value applies to non-coaxial arrangement.
Motor idle current and internal resistanceIdle current: 0.5A; internal resistance: 140±10mΩAIR2213 motor; idle current measured at 10V; resistance includes 300mm lead wire.

Product overview

The T-MOTOR Air Gear 355 (Quick-Release Version) provides a propulsion combination for multirotor aircraft, pairing AIR2213/KV1000 motors and MF9545 propellers with an AIR 20A four-in-one ESC. Its quick-release structure and assembly markings simplify fitting and removal. This is a propulsion combo rather than a complete flight platform or airframe kit. Integration planning can use the ESC’s 37.3 × 41.5 × 1.6mm dimensions, 8.1g weight including cable, and 50~400Hz throttle signal range; each motor weighs 56±2g including its 300mm lead wire.

The recommended power supply is a 3~4S LiPo battery, with motor voltage specified as 12.6V–16V; the ESC separately supports 2~4S. Recommended thrust per arm is 0.4~0.5kg, supporting the stated takeoff-weight ranges of 1.6~2.0kg for quadcopters, 2.4~3.0kg for hexacopters and 3.2~4.0kg for non-coaxial octocopters. Coaxial installations require a 25% loss allowance. The nylon-and-glass-fiber MF9545 propeller has a 1.5kg thrust limitation and a −10~40°C working range. Its specified storage conditions are 10~35°C and 65±20% relative humidity.

Specifications

SpecificationValue & conditions
Product and propulsion configurationT-MOTOR Air Gear 355 (Quick-Release Version) propulsion combo
Component configurationAIR2213/KV1000 quick-release motor; MF9545 quick-release propeller; AIR 20A four-in-one ESC
Assembly architectureQuick-release structure with assembly markings
Overall combo weight reduction13%Motor, propeller and ESC combined.
Recommended thrust and aircraft takeoff weights
  • Thrust per arm: 0.4~0.5 kg;
  • quadcopter MTOW: 1.6~2.0 kg;
  • hexacopter MTOW: 2.4~3.0 kg;
  • non-coaxial octocopter takeoff weight: 3.2~4.0 kg
Recommended multirotor configurations; octocopter value applies to non-coaxial arrangement.
Motor idle current and internal resistanceIdle current: 0.5A; internal resistance: 140±10mΩAIR2213 motor; idle current measured at 10V; resistance includes 300mm lead wire.
ESC connection dimensions and throttle signalBanana plug: 30.5*30.5/φ4mm; throttle signal frequency: 50~400HzAIR 20A four-in-one ESC.
Motor KV1000AIR2213 motor.
Motor rated voltage3~4S (4.2V/PC)/12.6V-16VAIR2213 motor; LiPo battery.
Motor peak current (180s)15A/ContinuousAIR2213 motor; specification carries a 180s heading and a continuous qualifier.
Motor weight56±2gAIR2213 motor; including cable and 300mm lead wire.
Motor maximum power (180s)238W/ContinuousAIR2213 motor; specification carries a 180s heading and a continuous qualifier.
Package weight/
ESC dimensions (L×W×H)37.3*41.5*1.6mmAIR 20A four-in-one ESC.
ESC rated voltage2~4SAIR 20A four-in-one ESC; LiPo battery.
ESC continuous current20AAIR 20A four-in-one ESC.
BEC/AIR 20A four-in-one ESC.
ESC peak current30AAIR 20A four-in-one ESC; 10s duration.
ESC weight8.1gAIR 20A four-in-one ESC; including cable.
Plastic propeller modelMF9545
Working temperature-10~40℃MF9545 propeller.
Propeller weight3.36gSingle MF9545 propeller.
Storage temperature10~35℃MF9545 propeller storage.
MaterialNylon+Glass FiberMF9545 propeller.
Storage humidity65±20% RHMF9545 propeller storage.
Surface treatmentMatte TechnologyMF9545 propeller.
Optimum rotational speed6000~7000RPM/minMF9545 propeller.
Propeller typePolymer PropellerMF9545 propeller.
Thrust limitation1.5kgMF9545 propeller.
Coaxial configuration loss allowanceAllow for a loss of 25%Coaxial configuration.
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