Product overview
The Times Starlight TIM-W60 is a powered cargo UAV for urban logistics, plateau and mountain supply delivery, relief operations, and agricultural and forestry transport. Its integrally molded carbon-fiber body combines a 2000mm wheelbase with a 14S power system and a stated maximum payload of 40kg. The aircraft incorporates the manufacturer's military-grade flight controller and an AI module supporting obstacle avoidance, positioning, landing, navigation and following. Redundant safety protections, 360° autonomous obstacle avoidance and planned-route autonomous flight extend its transport role.
The standard configuration specifies a 15 km data link under unobstructed, interference-free conditions. With the standard three-sensor gimbal, specified endurance is 40min and range is 40km. Maximum speed is 23m/s, maximum flight height is 2000m, and maximum takeoff altitude is 5000 m. Environmental specifications cover Force 6 wind, moderate rain and -20 ℃ to 60℃ operation. Procurement-relevant discrepancies remain: maximum takeoff weight is listed as both 40 kg and 80kg, while a separate gimbal-equipped endurance claim reaches 60 minutes. Cloud-platform and industry-application integration supports remote-sensing workflows.
Specifications
| Specification | Value & conditions |
|---|---|
| Product identity and purpose | Times Starlight TIM-W60 intelligent cargo UAV. |
| Airframe construction | Integrally molded carbon-fiber body described as lightweight, strong and corrosion-resistant. |
| Power system | 14S power system. |
| Intended transport applications | Urban logistics, plateau and mountain supply delivery, relief-supply delivery, and agricultural and forestry transport. |
| Flight control and intelligent functions | Manufacturer-developed military-grade flight control combined with an AI module for obstacle avoidance, precise positioning and landing, intelligent navigation, and following. |
| Autonomous flight and safety | Multiple redundant safety protections, 360° autonomous obstacle avoidance, and autonomous flight along planned routes. |
| Application integration | UAV, cloud-platform and industry-application integration for low-altitude remote sensing. |
| Wheelbase | 2000mm. |
| Maximum takeoff weight | 80kg in the performance description; 40 kg in the technical specifications. |
| Technical-table maximum takeoff weight | 40 kg; conflicts with the 80kg performance-description figure. |
| Maximum payload | 40kg. |
| Endurance | 40min.Standard three-sensor gimbal. |
| Performance-description endurance | Up to 60 minutes; differs from the 40min technical specification for the standard three-sensor gimbal.Three-sensor gimbal fitted. |
| Flight range | 40km.Standard three-sensor gimbal. |
| Data-link distance | 15 km.Standard configuration; unobstructed line of sight without interference. |
| Maximum flight height | 2000m. |
| Maximum takeoff altitude | 5000 m. |
| Maximum flight speed | 23m/s. |
| Wind resistance | Force 6. |
| Weather protection | Moderate rain. |
| Operating temperature | -20 ℃ ~ 60℃. |
| Environmental operating capability | Flight-task capability described at 4500 m altitude and in Force 6 wind and moderate rain.4500 m altitude, Force 6 wind and moderate rain. |
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