SV-V15 combines flexible vertical take-off and landing with fixed-wing area coverage for surveying, patrol and data collection.
SV-V15 combines vertical take-off and landing with a 5 m-span fixed-wing platform for wider-area inspection. Visible and thermal gimbal specifications support an early review of imaging, mass and interfaces. The 16-hour endurance entry explicitly concerns a heavy-fuel engine and must not be assumed for the gasoline configuration.
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-V15 |
|---|---|
| Category | Industrial drones |
| Airframe material | Carbon fibre and glass fibre |
| Wingspan | 5000 mm |
| Rated payload | ≥10 kg |
| Maximum payload | 15 kg |
| Maximum take-off mass | 55 kg |
| Fuel | No. 92 gasoline (source designation) |
| Service ceiling | 4500 m |
| Nominal operating / flight time | 16 h (heavy-fuel engine configuration) |
| Cruise speed | 60 km/h |
| Climb rate | 5 m/s |
| Control radius | 30 km |
| Wind resistance (source) | Force 6 |
| Optical zoom | 30× |
| Optical spectral range | 0.4-0.9 μm |
| Focal length | 4.3-129 mm |
| Video output | HD-SDI, 1080P, 30 Hz |
| Thermal imager type | Uncooled long-wave infrared |
| Infrared spectral range | 8-14 μm |
| Infrared detector pixels | 640 × 512 |
| Noise-equivalent temperature difference | 50 mK |
| Gimbal dimensions | 120 × 183 mm |
| Gimbal mass | 860 g |
| Gimbal operating temperature | -20 ~ 60 °C |
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.
