The commercial SV-T30 is a heavy-lift multirotor platform for industrial work and mission-system integration. Configure it around payload, endurance and environmental needs, using the product documentation for structural details and recommended setups.
The commercial version lists a 30 kg rated payload, a 36 kg airframe and eight motors, with documentation for a 30 kW ground station. It differs from the 34 kg SV-T30 tethered configuration. Specify the airframe, propeller and ground-power versions together.
Final configuration depends on operating conditions and the agreed specification.
A tethered system keeps its main power equipment on the ground and supplies the aircraft through a cable. It can support assessment of sustained lighting, observation and communications over a fixed area. The ground station, airborne power unit, backup supply, tether and reel must be matched as one system.
Confirm payload mass and power, station-keeping time, target height and site supply. Then assess tether mass, voltage drop and wind loading. Cable length is not usable vertical height: angle, sag, ground routing and obstacles consume length. Ground-station ratings from different versions are not interchangeable.
Before deployment, inspect connector locks, cable insulation, strain relief, cooling and protective grounding. Make connections with power isolated. Follow the fitted controller’s instructions for startup, voltage and backup power. Controlled commissioning should verify reel operation and responses to communication or primary-power loss.
Monitor voltage, current, payout and reel behavior during operation; keep the tether clear of people and obstacles. Afterwards inspect wear, bends, connectors and abnormal heating. Return-to-home or landing behavior must suit the tethered operating envelope and be validated on the fitted system, rather than copied from free flight.
Geometry follows the source. Verify the actual model and approved drawing before installation.
Final configuration depends on operating conditions and the agreed specification.
| Model | SV-T30 |
|---|---|
| Category | Industrial drones |
| Motor-to-motor diagonal | 2050 mm |
| Unfolded / working dimensions | 1570 × 1570 × 715 mm |
| Folded / storage dimensions | 845 × 860 × 775 mm |
| Product mass | 36 kg |
| Number of motors | 8 |
| Maximum output per motor | 6000 W |
| Rated thrust per motor | 16 kg |
| Rated payload | 30 kg |
| ESC rated voltage | 500 V DC |
| ESC rated current | 10 A |
| Propeller diameter × pitch | 32 × 12 in |
| Propeller material | Carbon-fibre composite |
| Ground-station model | W30 |
| Ground-station mass | 70 kg |
| Ground-station dimensions | 600 × 600 × 600 mm |
| Ground-power input | 380 V AC, 50-60 Hz |
| Ground-power output voltage | 500 V DC |
| Rated ground-power output | 30 kW |
| Tether length | 100 m |
| Automatic reel speed | 1 m/s |
| Nominal generator-powered flight duration | 8 h |
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.
SV TECH / PRODUCT ENGINEERING
Existing selection guides are retained; complete operating chapters are added. Chinese and English controller procedures differ; use the procedure confirmed for the fitted controller.
Chinese rated thrust of 16 kg and English maximum thrust of 25 kg are different definitions, not one common rating.
A changeover system supports different power and mission modes; signal switching coordinates control sources. Confirm these functions with the flight controller, onboard power and mission configuration.
Documents and engineering resources ↗ · All recognition and source images ↗
