Product overview
The V135 IPE V2.0 is offered in a 55KV configuration for eVTOL drone applications.
MAD describes the motor as designed to carry a payload of 25–30kg per rotor with a 40-inch carbon propeller.
For coaxial installations, Allow for a total thrust loss of 25%.
Specifications
| Specification | Value & conditions |
|---|---|
| Motor model | MAD V135 IPE V2.0Model identified in motor data. |
| KV option | 55KVListed product option. |
| Design payload per rotor | 25–30kgWith a 40-inch carbon propeller; described as a design payload, not a verified aircraft payload rating. |
| Coaxial thrust allowance | 25% total thrust lossFor a coaxial configuration. |
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