Unmaned Surface Vehicles
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Total Stations
Electronic Theodolites
Digital Levels
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Prisms/Tripods/Poles/Staffs...
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SLAM LiDAR
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Pipe & Cable Locator
VR Simulated Surveying Training Systems
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Track Geometry Measuring Trolley Systems
Automated Tunnel Scanning & Inspection Systems

Model: MF2500
Features
Specification

| Aircraft System | aircraft type | VTOL (vertical takeoff and landing) |
| wingspan | 250 cm | |
| take-off weight | 11 kg | |
| power supply | lithium polymer battery | |
| battery power |
38500 mAh*1 (fixed wing) 3700 mAh*2 (rotor) |
|
| body material | kevlar fiber material | |
| Flight Performance | take-off method | vertical take-off |
| landing method | vertical landing | |
| maximum ceiling | 5500 m | |
| working height | -- | |
| cruising speed* | typical 21 m/s (75 km/h) | |
| endurance | best up to 150 minutes | |
| single flight range* | maximum 180 km | |
| single flight coverage* | maximum 46 sq.km/GSD 10 cm | |
| landing space | vertical landing within 1 m | |
| Operation Performance | base observations | autopilot |
| radio datalink | -- | |
| control frequency | 1-2W | |
| radio communication range | 3-20 km | |
| weather limit | beaufort scale 6 (10.8-13.8 m/s) | |
| operating temperature | -10℃ to 45℃ | |
| Ground Control | auto return | upon indications of low battery, airspeed anomaly, abnormal attitude |
| drone tracking | manually controlled, one-key operation |
Note: all information above is subject to change without any prior notice.
9598