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T-MOTOR HEP-L 22*7.2 carbon fiber propellerT-MOTOR HEP-L 22*7.2 carbon fiber propeller

HEP-L 22*7.2

The T-MOTOR HEP-L 22*7.2 is a lightweight, one-piece straight propeller for long-endurance multirotor UAVs. Built from resin-based carbon fiber composite with a PMI foam core, it weighs about 37g per propeller. Its flange mounting interface and recommended MN6007 II motor combinations support specified 6S and 12S propulsion configurations.

T-MOTORDrone motor
Weight
About 37g
Material
Resin-based carbon fiber composite + PMI foam core

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Product overview

The T-MOTOR HEP-L 22*7.2 is a one-piece straight rotor propeller for long-endurance multirotor UAVs. Its resin-based carbon fiber composite construction incorporates a PMI foam core and a matte finish, with each propeller weighing about 37g. The diameter is 22 inches (562.2mm), with a 7.2-inch (182.9mm) pitch. Its common operating range is 2400~3500 RPM and 1.2~2.6 kg thrust. Recommended maxima are 6550 RPM and 11 kg thrust; the limit values are 7350 RPM and 14 kg.

The flange mount has a Ø6mm center hole, a Ø12mm bolt circle and two Ø3mm mounting holes. Recommended combinations pair the MN6007 II KV160 motor with 12S or the MN6007 II KV320 with 6S, each with a recommended quadcopter takeoff weight of 7kg. Both solutions specify FLAME 60A. Aerodynamic optimization improves hovering efficiency and increases effective flight time by up to 3%, while the enhanced structure reduces cruise vibration and improves wind resistance. A molded QR code supports traceability, and protective packaging helps safeguard transport.

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Specifications

SpecificationValue & conditions
ProductT-MOTOR HEP-L 22*7.2 rotor propeller
ApplicationLong Endurance Multi-Rotor UAV
Diameter22 inches (562.2mm)
Pitch7.2 inches (182.9mm)
Common thrust range1.2~2.6 kg
Common speed range2400~3500 RPM
WeightAbout 37gSingle propeller.
MaterialResin-based carbon fiber composite + PMI foam core
Surface treatmentMatte
TypeOne-piece straight propeller
Recommended maximum speed6550 RPM
Limit speed7350 RPM
Recommended maximum thrust11 kg
Limit thrust14 kg
Mounting interfaceFlange mount; Ø6mm center hole; Ø12mm bolt circle; 2 × Ø3mm mounting holes
Recommended motor configuration and takeoff weightMN6007 II KV160; 12S; recommended quadcopter takeoff weight 7kgMN6007 II KV160 motor; recommended 12S configuration; quadcopter.
Recommended motor configuration and takeoff weightMN6007 II KV320; 6S; recommended quadcopter takeoff weight 7kgMN6007 II KV320 motor; recommended 6S configuration; quadcopter.
Recommended propulsion solutionMN6007 II KV160 + FLAME 60A; 12SMN6007 II KV160 motor; 12S configuration.
Recommended propulsion solutionMN6007 II KV320 + FLAME 60A; 6SMN6007 II KV320 motor; 6S configuration.
Aerodynamic designAerodynamic optimization improves hovering efficiency and increases effective flight time by up to 3%
Vibration and wind resistanceEnhanced structure reduces vibration and improves wind resistanceDuring cruise.
Damage-resistant constructionHigh-toughness resin, surface fiber reinforcement and damage-tolerant design limit micro-damage propagation
Impact resistanceHEP-L impact depth 1.93mm versus 2.54mm for NS; 24% improved impact resistanceIdentical 6J impact energy.
Identification and packagingIntegrated molded QR code and protective packaging

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