Product overview
The Yifei Zhineng X900 carries mission payloads on a quadrotor architecture with a carbon-fiber composite body and folding arms. Its 850mm wheelbase accompanies a maximum payload of 7kg and maximum takeoff weight of 12kg. Empty aircraft weight is 3.5kg excluding the battery. Folding the arms reduces storage volume and supports transport and deployment. Maximum endurance reaches 80 minutes unloaded. Cruise speed is 15m/s, with maximum horizontal speed of 22m/s, ascent speed of 5m/s and descent speed of 3m/s.
The standard flight platform package includes an X900 frame, remote controller, one propulsion battery, charging equipment, four motors and four propellers. Installation tools, a custom onboard wiring harness, documentation and a custom packaging box complete the supplied configuration. Multi-constellation satellite positioning provides horizontal hovering accuracy of ±0.3m under good satellite positioning conditions. Environmental limits include Force 6 wind resistance, IP54 protection and operation from -20°C to 50°C. Maximum takeoff altitude is 4000m above sea level. Parameters can be customized, with the delivery contract governing the delivered specification.
Specifications
| Specification | Value & conditions |
|---|---|
| Aircraft configuration | Quadrotor |
| Wheelbase | 850mm |
| Unfolded dimensions | 690*690*460Excluding propellers. |
| Folded dimensions | 450*450*460Excluding propellers. |
| Body material | Carbon-fiber composite |
| Maximum endurance | 80minUnloaded. |
| Empty aircraft weight | 3.5kgExcluding battery. |
| Maximum payload | 7kg |
| Maximum takeoff weight | 12kg |
| Cruise speed | 15m/s |
| Maximum horizontal flight speed | 22m/s |
| Maximum ascent speed | 5m/s |
| Maximum descent speed | 3m/s |
| Maximum flight radius | 15km |
| Maximum takeoff altitude above sea level | 4000m |
| Wind resistance | Force 6 |
| Ingress protection | IP54 |
| Operating ambient temperature | -20°C to 50°C |
| Maximum tilt angle | 30° |
| Horizontal hovering accuracy | ±0.3mGood satellite positioning conditions. |
| Arm architecture | Folding arms for compact storage and convenient transport and deployment |
| Positioning system | Multi-constellation satellite positioning |
| Parameter customization | Aircraft parameters can be customizedDelivered parameters are governed by the delivery contract. |
| Frame | 1 X900 frame setStandard supplied configuration. |
| Remote controller | 1 remote controllerStandard supplied configuration. |
| Battery and charging equipment | 1 propulsion battery and 1 charging unitStandard supplied configuration. |
| Motors and propellers | 4 EF Motor motors and 4 EF Propeller propellersStandard supplied configuration; CW/CCW components. |
| Installation tools and wiring | 1 installation tool kit and 1 custom onboard wiring harness setStandard supplied configuration. |
| Product documentation | 1 documentation set comprising a conformity certificate and operating instructionsStandard supplied configuration. |
| Packaging box | 1 custom packaging boxStandard supplied configuration. |
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