Product overview
The T-MOTOR MF2211VP is a manually adjustable folding propeller for multirotor and VTOL propulsion. Its Polymer+CF construction combines a reinforced root, large swept-back tip and downward-curved winglets, with a revised spacer designed to reduce rotational damping and vibration. Diameter is 22.4inch (568.96mm), nominal pitch is 8inch (203.2mm), and each blade weighs 86.5g. Integration recommendations pair it with the MN605 KV170 motor and either the FLAME 60A 12S V2.0 or FLAME 180A 12S V2.0 ESC, including applications using coaxial power arrangements.
Pitch changes are made manually by replacing positioning blocks without additional tools. The packing list includes one CW and one CCW block at each of +2.5°, -2.5° and +5°, plus four M3*10mm screws. Package dimensions are 300*106*45mm and package weight is 286g. The speed-based block guidance applies at 0~2000m altitude; altitude-based guidance applies below 15m/s. Listed pitches extend from 7.4 to 17.1inch, with 7.5° and 10° blocks explicitly marked not recommended. Those angles and other blocks can be requested as custom options.
Thrust descriptions differ: the principal ratings are 1.5~5kg recommended thrust and 12kg recommended maximum, while another description gives a common range of 0.5–2.2kg. With an MN4012 KV340 motor, FLAME 60A 12S V2.0 ESC and 7.5° block, maximum pull is 2.8kg at maximum throttle, with 3kg recommended maximum. The MN605 KV170/FLAME 60A 12S V2.0 configuration carries burnout warnings at +5° and +7.5°; +10° is discouraged for static testing. Ambient temperature is -40°C to 65°C; storage requires -10°C to 50°C and humidity below 85%.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer, model and application | T-MOTOR MF2211VP Polymer Manual Variable Pitch Folding Propeller for multirotor and VTOL drones. |
| Series | Folding |
| Blade weight | 86.5gSingle blade. |
| Package weight | 286g |
| Diameter | 22.4inch (568.96mm) |
| Package dimensions | 300*106*45mm |
| Nominal pitch | 8inch (203.2mm) |
| Material | Polymer+CF |
| Recommended thrust | 1.5~5kg |
| Recommended maximum thrust | 12kg |
| Ambient temperature range | -40°C to 65°CAmbient temperature. |
| Storage temperature and humidity | -10°C to 50°C / less than 85%Storage. |
| Recommended ESC | FLAME 60A 12S V2.0 / FLAME 180A 12S V2.0 |
| Recommended motor | MN605 KV170 |
| Positioning block selection by flight speed |
|
| Positioning block selection by flight altitude |
|
| Pitch by positioning block |
|
| Efficiency comparison configuration and notation | S0/S5/S10/S15 represent 0/5/10/15m/s; D0/D2.5/D5 represent 0°/2.5°/5° positioning blocks.MN605 KV170 + FLAME 180A 12S V2.0 + MF2211VP; flight inclination 30°. |
| Pitch adjustment | Manual pitch adjustment by replacing the positioning block, without additional tools. |
| Tip architecture | Large swept-back tip and downward-curved winglets. |
| Root and spacer architecture | Reinforced root for high-pull conditions and coaxial power arrangements; improved spacer design to reduce rotational damping and vibration. |
| Packing list | One CW and one CCW positioning block at each of +2.5°, -2.5° and +5°; four M3*10mm cup-head socket-head cap screws.Included equipment. |
| Optional positioning blocks | 7.5°, 10° and other positioning blocks by customization request.Custom configuration. |
| Configuration-specific pull-force description | Maximum pull force 2.8kg; recommended maximum pull force 3kg.T-MOTOR MN4012 KV340 motor + FLAME 60A 12S V2.0 ESC; maximum throttle; 7.5° positioning block. |
| Additional common pulling-force description | 0.5 to 2.2 kilograms. |
| Positive 5° burnout limitation | Risk of burnout.MN605 KV170 + FLAME 60A 12S V2.0 + MF2211VP (+5°); ambient temperature 25°C. |
| Positive 7.5° burnout limitation | Risk of burnout.MN605 KV170 + FLAME 60A 12S V2.0 + MF2211VP (+7.5°); ambient temperature 25°C. |
| Positive 10° static-testing limitation | 10° positioning block is not recommended for static testing.MN605 KV170 + FLAME 60A 12S V2.0 + MF2211VP (+10°); static testing. |
| Impact damage replacement | Replace deformed or cracked propellers.Propellers subjected to a fall or equivalent impact that causes deformation or cracks. |
| Long-term storage requirement | Keep sealed.Storage longer than 6 months. |
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