| Weight (with propeller and battery) | 1237g±0.5g |
| Size(L*W*H, propeller included) | 457*558*143mm (Unfolded) 230*130*143mm (Folded) |
| Wheelbase | 397 mm |
| Maximum Service Ceiling Altitude | 6000 m |
| Max ascent speed | 5 m/s（automatic flight） 8 m/s（manual control） |
| Max descent speed | 4 m/s (Ludicrous) |
| Max horizontal flight speed | 20m/s (Ludicrous) |
| Max tilt angle | 33° (Ludicrous) |
| Max angular velocity | 120°/s |
| Max flight time | 36 min |
| Operating temperature range | -10℃ ~ 40℃ |
| Maximum resistance to wind | Level 8 |
| Operating frequency | non-Japan：2.400 GHz - 2.4835 GHz；5.725 - 5.850 GHz Japan：2.400 GHz - 2.4835 GHz；5.650 - 5.755 GHz |
| Transmission power | 2.4G FCC/ ISED：≤27dBm SRRC/CE/MIC/RCM：≤20dBm 5.8G (non-Japan) ; 5.7G (Japan) FCC/ISED/SRRC/MIC：≤27dBm CE/ RCM：≤14dBm |
| Hovering accuracy | When RTK is enabled and working normally: Vertical: ±0.1 m; Horizontal: ±0.1 m |
| RTK is not enabled: vertical: ±0.1 m (when the visual positioning is working normally); ±0.5 m (when GNSS positioning works normally) Level: ±0.3 m (when the visual positioning is working normally); ±1.5 m (when GNSS positioning works normally) |
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| Image position compensation | The position of the camera center relative to the phase center of the airborne A-RTK antenna, under the body axis system: (-2.63, 0.31, 83.5) mm, and the photo EXIF coordinates have been compensated. The positive XYZ axis of the body axis system points to the front, right, and bottom of the aircraft respectively. |
