SV-S supports area surveying, patrol and data collection, with configuration around the mission payload and the customer's workflow.
SV-S lists a 1 kg rated payload, a 2.8 kg airframe and a folding structure for camera or inspection-payload integration. Survey deliverable quality also depends on the camera, positioning method, image overlap and ground-control plan; aircraft specifications alone do not establish mapping accuracy.
Final configuration depends on operating conditions and the agreed specification.
A mission platform combines the airframe, propulsion, flight control, communications and payload. Surveying emphasizes imaging and positioning; inspection emphasizes viewing geometry and coverage; transport emphasizes restraint and centre of gravity. Product specifications define initial limits, while mission results require complete-system validation.
Prepare payload mass, dimensions, power and interfaces, plus route length, duration, take-off space and wind conditions. Interpret nominal endurance with load, energy reserve and environment. Control range and ceiling are not operating permissions. Record acceptance criteria in the project configuration.
Remove propellers before parameter changes or firmware updates. Check airframe heading, controller and positioning-module orientation, propeller rotation and electrical connections. Use the fitted controller’s version-specific procedure for calibration, mode switching and failsafe verification. After loading, check balance and camera obstruction before controlled flight tests.
Inspect propellers, fasteners, battery or fuel system and communications before and after flight. Log payload configuration, flight time and anomalies to track wear. Abnormal vibration, energy warnings, unstable positioning or severe weather call for aborting under the validated contingency procedure and inspecting the aircraft.
Final configuration depends on operating conditions and the agreed specification.
| Model | SV-S |
|---|---|
| Category | Industrial drones |
| Motor-to-motor diagonal | 710 mm |
| Unfolded / working dimensions | 570 × 620 × 220 mm |
| Folded / storage dimensions | 510 × 270 × 130 mm |
| Product mass | 2.8 kg |
| Number of motors | 4 |
| Maximum output per motor | 430 W |
| Maximum thrust per motor | 2.5 kg |
| Rated payload | 1 kg |
| ESC rated voltage | 24 V DC |
| ESC rated current | 6 A |
| Propeller diameter × pitch | 15 × 5.5 in |
| Propeller material | Carbon-fibre composite |
Documentation covers dimensions, performance data and operating requirements. Contact Mr. Liu for selection advice or after-sales support.
Final configuration depends on operating conditions and the agreed specification.
