Product overview
The Mingde HI41200 is an integrated carbon-fiber airframe for multirotor UAV construction. Its shell uses Japanese Toray 3K carbon fiber, formed through internal-pressure integral molding, with a thickness of 0.6mm. The physical dimensions comprise a 1200mm symmetrical wheelbase and a 500mm overall height. Shell weight is 1700G. These structural specifications describe the airframe and its shell; the shell-weight figure does not represent the total weight of an equipped aircraft.
For propulsion integration, the HI41200 accommodates motors up to 8-series size and propellers up to 29 inches. These dimensions set the stated upper limits for motor and propeller fitment. Unloaded flight time is 85min with two 25000mAh batteries, while maximum payload is specified as 5kg@35min. The endurance figures therefore describe two distinct load conditions: unloaded operation with the stated battery configuration, and a 35min duration associated with the maximum 5kg payload.
Specifications
| Specification | Value & conditions |
|---|---|
| Product type | Mingde HI41200 integrated carbon-fiber airframe |
| Shell material | Japanese Toray 3K carbon fiber |
| Manufacturing process | Internal-pressure integral molding |
| Shell thickness | 0.6mm |
| Symmetrical wheelbase | 1200mm |
| Overall height | 500mm |
| Shell weight | 1700G |
| Unloaded flight time | 85minUnloaded, with two 25000mAh batteries. |
| Maximum payload and associated flight time | 5kg@35minAt the maximum payload of 5kg. |
| Maximum motor size | 8-series |
| Maximum propeller size | 29 inches |
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