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COMPONENT

MF3016VP

By T-MOTOR ↗

The T-MOTOR MF3016VP is a folding, manually adjustable variable-pitch UAV propeller for multirotor and VTOL propulsion. Interchangeable positioning blocks allow pitch changes for different speeds, altitudes and aircraft weights. Its Polymer+CF construction, recommended propulsion components and configuration-specific operating limits support selection for professional aircraft development.

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Manufacturer and modelT-MOTOR MF3016VP
Model numberMF3016VP
Series architectureFolding
Single-blade weight190g
Package weight640g
Diameter30.4inch (772.16mm)

Product overview

The T-MOTOR MF3016VP uses folding blades made from Polymer+CF, with a diameter of 30.4inch (772.16mm) and a single-blade weight of 190g. Its manual adjustment mechanism changes pitch through interchangeable positioning blocks, supporting propulsion integration for multirotor and vertical take-off and landing aircraft. Recommended components include the FLAME 180A 12S V2.0 ESC and MN1010/P80ll/U12ll/U13ll motors. Recommended thrust is 4~12kg, with a recommended maximum of 20kg. Package dimensions are 400*190*70mm and package weight is 640g.

Pitch selection depends on flight speed and altitude: the speed reference applies at 0~2000m, while the altitude reference applies below 15m/s. The selection tables mark 7.5° and 10° blocks as not recommended, and these blocks are offered through customization. Certain positive-angle configurations carry a motor burnout risk, while +10° is not recommended for static testing. Ambient temperature spans -40℃ to 65℃; storage requires -10℃ to 50℃ and humidity below 85%. Damaged propellers require replacement, and storage beyond six months requires sealed preservation.

Specifications

SpecificationValue & conditions
Manufacturer and modelT-MOTOR MF3016VP
Model numberMF3016VP
Series architectureFolding
Single-blade weight190g
Package weight640g
Diameter30.4inch (772.16mm)
Package size400*190*70mm
Specified pitch10.9inch (276.86mm)
MaterialPolymer+CF
Recommended thrust4~12kg
Recommended maximum thrust20kg
Ambient temperature-40℃ to 65℃
Storage temperature and humidity-10℃ to 50℃ / less than 85%Storage.
Recommended ESCFLAME 180A 12S V2.0
Recommended motorsMN1010/P80ll/U12ll/U13ll
Flight-speed positioning-block selection
  • 0~10m/s: 0°;
  • 5~15m/s: 2.5°;
  • 10~20m/s: 5°;
  • 15~25m/s: 7.5° (not recommended);
  • 20~30m/s: 10° (not recommended).
Flight altitude 0~2000m.
Flight-altitude positioning-block selection
  • 0~1000m: 0°;
  • 0~2000m: 2.5°;
  • 0~3000m: 5°;
  • 1000~4000m: 7.5° (not recommended);
  • 2000~5000m: 10° (not recommended).
Flight speed below 15m/s.
Pitch selection
  • 0°: 10.2inch;
  • 2.5°: 13.5inch;
  • 5°: 16.7inch;
  • 7.5°: 20.1inch (not recommended);
  • 10°: 23.5inch (not recommended).
Pitch varies with positioning-block angle.
Pitch adjustmentManual pitch adjustment by replacing positioning blocks.
Aircraft integrationPropellers for multirotor and vertical take-off and landing aircraft.
Pitch customizationMinimum order quantity 1; pitch angle customizable to 0.01°.Custom configuration.
Additional positioning blocks7.5°, 10° and other positioning blocks available upon request for customization.Custom configuration.
Motor burnout limitationThe +2.5°, +5° and +7.5° test configurations carry a motor burnout risk.P80III KV120 + FLAME 180A 12S V2.0 with MF3016VP at +2.5°, +5° or +7.5°.
Static-testing limitationThe +10° angle is not recommended for static testing.P80III KV120 + FLAME 180A 12S V2.0 + MF3016VP (+10°); ambient temperature 25℃.
Impact damageReplace propellers with deformation or cracks following a fall or equivalent impact.After a fall or equivalent impact causing deformation or cracks.
Disassembly restrictionDo not disassemble the propellers.
Long-term preservationKeep sealed during storage exceeding 6 months.Storage exceeding 6 months.
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