| Single-blade weight | 273gPer blade for the VZ42*16.5 model. |
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| Model | T-MOTOR VZ42*16.5 propeller |
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| Diameter | 42.2 inches (1071.9 mm) |
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| Material | Resin-based carbon fiber composite with PMI sandwich core |
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| Pitch | 16.5 inches (419.1 mm) |
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| Surface finish | Matte |
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| Average weight per propeller | 273 g |
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| Type | One-piece straight propeller |
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| Recommended maximum speed | 3970 RPM |
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| Application | VTOL hybrid fixed-wing UAV, multirotor mode |
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| Recommended maximum thrust | 52.8 kg |
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| Mounting interface | Flange connection; Ø12 mm center hole; Ø30 mm bolt circle; four Ø5 mm mounting holes |
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| Limit speed | 4460 RPM |
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| Recommended power system | V13L KV65 + THUNDER 200A 24S / VL1165 KV60 + VL200A |
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| Limit thrust | 66 kg |
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| Measured performance | - Torque: 4.66 N·m;
- thrust: 9375 gf;
- output power: 810.21 W;
- thrust efficiency: 11.57 gf/W
1660 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 5.75 N·m;
- thrust: 11852 gf;
- output power: 1120.44 W;
- thrust efficiency: 10.58 gf/W
1860 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 6.98 N·m;
- thrust: 14572 gf;
- output power: 1505.47 W;
- thrust efficiency: 9.68 gf/W
2060 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 8.34 N·m;
- thrust: 17535 gf;
- output power: 1973.76 W;
- thrust efficiency: 8.88 gf/W
2260 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 9.84 N·m;
- thrust: 20742 gf;
- output power: 2533.78 W;
- thrust efficiency: 8.19 gf/W
2460 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 11.47 N·m;
- thrust: 24192 gf;
- output power: 3194.00 W;
- thrust efficiency: 7.57 gf/W
2660 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 13.23 N·m;
- thrust: 27886 gf;
- output power: 3962.90 W;
- thrust efficiency: 7.04 gf/W
2860 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 15.13 N·m;
- thrust: 31823 gf;
- output power: 4848.92 W;
- thrust efficiency: 6.56 gf/W
3060 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 17.17 N·m;
- thrust: 36003 gf;
- output power: 5860.55 W;
- thrust efficiency: 6.14 gf/W
3260 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 19.34 N·m;
- thrust: 40427 gf;
- output power: 7006.25 W;
- thrust efficiency: 5.77 gf/W
3460 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 21.64 N·m;
- thrust: 45094 gf;
- output power: 8294.49 W;
- thrust efficiency: 5.44 gf/W
3660 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 24.08 N·m;
- thrust: 50005 gf;
- output power: 9733.74 W;
- thrust efficiency: 5.14 gf/W
3860 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 26.65 N·m;
- thrust: 55159 gf;
- output power: 11332.46 W;
- thrust efficiency: 4.87 gf/W
4060 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 29.36 N·m;
- thrust: 60556 gf;
- output power: 13099.12 W;
- thrust efficiency: 4.62 gf/W
4260 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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| Measured performance | - Torque: 32.21 N·m;
- thrust: 66197 gf;
- output power: 15042.19 W;
- thrust efficiency: 4.40 gf/W
4460 RPM; ambient temperature 22 °C; altitude 25 m. Data may vary with test equipment, methods, environment and standards. |
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