T-MOTOR MF2412VP

The T-MOTOR MF2412VP is a polymer and carbon fiber folding UAV propeller with manually adjustable pitch. Interchangeable positioning blocks adapt blade pitch for different flight conditions, supporting multirotor and VTOL applications including high-speed flight, high-altitude operation and aircraft development.

T-MOTORDrone motor

Material: Polymer + carbon fiber

Product overview

Built from polymer and carbon fiber, the MF2412VP combines folding blades with a 24.4-inch (619.76mm) diameter and a reference individual weight of 115.8g. Replacing the positioning block changes blade pitch manually, supporting aircraft development and transitions between flight conditions. Applications include high-speed and high-altitude flight, aircraft weight changes and fine adjustment of customized blade performance. The propeller supports multirotor and vertical takeoff and landing aircraft. Recommended drive components are the FLAME 180A 12S V2.0 ESC and MN705 KV140 or MN701 KV135 motors.

Typical thrust is 2.8~6kg, with a recommended maximum of 13kg. The operating ambient temperature range is -40°C to 65°C; storage requires -10°C to 50°C and humidity below 85%. Positioning blocks at 7.5°, 10° and other custom angles require separate customization, and static testing is not recommended at 7.5° or 10°. Custom propeller orders start from one unit, with angle precision to 0.01°. For bulk production, engineers can help determine a custom angle that can then be fixed at the factory before shipment.

Motors & ESCs

Specifications

T-MOTOR MF2412VP specifications
Specification	Value & conditions
Model	T-MOTOR MF2412VP
Product type	Polymer manually variable-pitch UAV propeller
Construction type	Folding propeller
Reference weight per individual propeller	115.8g
Package weight	337.2g
Diameter	24.4 inches (619.76mm)
Package dimensions	30512748mm
Material	Polymer + carbon fiber
Typical thrust	2.8~6kg
Recommended maximum thrust	13kg
Operating ambient temperature	-40°C to 65°C
Storage temperature and humidity	-10°C to 50°C / less than 85%Storage.
Recommended ESC	FLAME 180A 12S V2.0
Recommended motors	MN705 KV140 / MN701 KV135
Positioning-block selection by flight speed	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 within 0~2000m.
Positioning-block selection by flight altitude	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 by positioning-block angle	0°: 8.4 inches; 2.5°: 11 inches; 5°: 13.6 inches; 7.5°: 16.3 inches; 10°: 17.9 inches Positioning-block angles of 0°, 2.5°, 5°, 7.5° and 10°, respectively; 7.5° and 10° are marked not recommended.
Pitch adjustment method	Blade pitch is adjusted manually by replacing the positioning block.
Applications	High-speed flight, high-altitude flight, aircraft weight changes and fine adjustment of customized blade performance
Aircraft applications	Multirotor and vertical takeoff and landing aircraft
Custom block requirement	7.5°, 10° and other positioning blocks require separate customization.Custom positioning blocks.
Customization	Customization starts from one propeller, with angle precision to 0.01°.Custom propeller orders.
Factory angle setting	The custom angle can be fixed before shipment.Bulk custom production after engineers help determine the angle.
Static testing limitation	Static testing is not recommended at 7.5°.7.5° or 10° positioning-block configuration.
Static testing limitation at 10°	Static testing is not recommended at 10°.10° positioning-block configuration.