Overview
MAD FLUXER VTOL carbon fiber propeller (24.1x9.6 inch) with an integrated structure design for higher strength. The VTOL-optimized prop profile reduces prop surface area to lower air resistance during cruise, while the larger pitch supports higher thrust and faster response. Reinforced installation positions improve durability and operational safety. Designed to pair well with MAD brushless motors.For compatibility checks (motor KV, hub pattern, and installation hardware), contact https://rcdrone.top/ or email support@rcdrone.top.
Key Features
- Integrated structure design for higher intensity
- VTOL-optimized profile for reduced cruise air resistance
- Larger pitch for higher thrust and faster startup/response
- Reinforced mounting areas for improved durability
- High quality carbon fiber + resin construction
Specifications
| Model | FLUXER VTOL Props 24.1x9.6 |
| Size | 612.14 x 243.84 mm |
| Material | High quality carbon fiber + Resin |
| Single weight | 65 g |
| Surface treatment | Polished/matt |
| Working temperature | -40°C to 65°C |
| Storage temperature | -10°C to 50°C |
| Storage humidity | <85% |
| Optimum RPM | 3300-4400RPM/min |
| Single thrust limitation | 15 kg |
| Package | Color box |
| Mounting hole (diagram) | 4x M3; PCD: φ20 mm; center hole: φ10 mm |
| Blade marking | 24.1 x 9.6 CCW |
Test Data
| RPM | Thrust (gf) | Torque (N*m) | Output Power (W) | Efficiency (gf/W) |
|---|---|---|---|---|
| 474 | 70 | 0.0 | 0.9 | 78.38 |
| 947 | 330 | 0.1 | 9.6 | 33.81 |
| 1367 | 700 | 0.2 | 29.9 | 23.55 |
| 1807 | 1210 | 0.4 | 69.1 | 17.53 |
| 2142 | 1600 | 0.5 | 111.2 | 14.39 |
| 2549 | 2370 | 0.7 | 189.6 | 12.50 |
| 2918 | 3200 | 1.0 | 289.7 | 11.04 |
| 3231 | 3910 | 1.2 | 396.6 | 9.86 |
| 3529 | 4610 | 1.4 | 513.3 | 8.99 |
| 3795 | 5380 | 1.6 | 640.6 | 8.40 |
What's Included
- 24.1 x 9.6 propellers: 2 pcs
- Cover plate: 2 pcs
- Hex socket cap head screw M3*28: 8 pcs
Description

Details

The FLUXER VTOL 24.1×9.6 carbon fiber propeller lists key parameters like weight (65 g), mounting pattern, and thrust test data for setup planning.
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