Product overview
The Zhuhai SV Tech Co., Ltd. ME100 is a heavy-payload multirotor flight platform for industrial missions, with support for mission-payload and ground-system integration. Propulsion and payload selection depend on operating conditions, while final equipment configuration depends on agreed project specifications. Payload accommodation requires assessment of cargo dimensions, center of gravity, securing arrangements and takeoff and landing space before confirming the specific model and its flight duration under the intended load.
The available reference configuration is designated E100, whose correspondence with ME100 remains unresolved and requires confirmation before ordering. Subject to that restriction, it specifies six motors, a 3000 mm motor wheelbase, 3000 × 3000 × 1800 mm operating dimensions, 110 kg aircraft mass and 100 kg rated payload. Each motor is listed at 15 kW maximum output and 85 kg maximum thrust, with 51 × 9.5 in carbon-fiber propellers. Nominal duration is 15 min without complete test conditions; full-payload endurance and passenger-carrying authorization cannot be inferred.
Specifications
| Specification | Value & conditions |
|---|---|
| Model | ME100 |
| Product category | Industrial UAV |
| Motor wheelbase | 3000 mmE100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Dimensions | 3000 × 3000 × 1800 mmDeployed / operating dimensions in the E100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Complete aircraft mass | 110 kgE100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Nominal operating / flight time | 15 minE100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. Full-payload endurance cannot be inferred. |
| Motor count | 6E100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Maximum output power | 15 kWPer motor in the E100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Maximum thrust | 85 kgPer motor in the E100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Rated payload | 100 kgE100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Propeller diameter × pitch | 51 × 9.5 inE100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Propeller material | Carbon fiberE100 attachment reference configuration; correspondence with ME100 must be confirmed before ordering. |
| Purpose | Heavy-payload industrial missions and system integration, with propulsion and mission payload matched to operating conditions. |
| Integration scope | Mission-payload and ground-system integration. |
| Final configuration | Configuration is determined for the project.Operating conditions and mutually agreed specifications determine the final configuration. |
| Model correspondence limitation | The E100 attachment designation conflicts with ME100; correspondence must be confirmed before ordering.Parameters retained as an attachment reference configuration. |
| Payload accommodation requirements | Cargo dimensions, center of gravity, securing method and takeoff and landing area require assessment before confirming the model and flight duration for the payload.Heavy-load projects. |