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A long-endurance delta-wing fixed-wing UAV with 13h endurance, 50 kg payload capacity, 180 kg maximum takeoff weight, 5000 m maximum flight altitude, and Level 7 wind resistance for target simulation, electronic countermeasure support, and multi-payload mission applications.





The HY180 Long-Endurance Delta-Wing Fixed-Wing UAV is a mission-focused unmanned aircraft platform designed for target simulation, electronic countermeasure support, payload integration, and specialized field operation scenarios. Its delta-wing fixed-wing configuration provides stable flight performance, strong payload adaptability, and reliable endurance for professional B2B applications. With a fuselage length of 2850 mm, wingspan of 2600 mm, maximum takeoff weight of 180 kg, and maximum payload capacity of 50 kg, the HY180 offers a practical balance between payload capability, endurance, speed, and deployment flexibility. The platform supports up to 13 hours of endurance, 50 m/s cruise speed, 62 m/s maximum level speed, 5000 m maximum flight altitude, and Level 7 wind resistance. It can support rocket-assisted launch or pneumatic launcher deployment, with parachute recovery for mission completion.
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The HY180 Long-Endurance Delta-Wing Fixed-Wing UAV is designed for professional B2B customers who need a long-endurance fixed-wing UAV platform with strong payload adaptability and reliable mission performance. It is suitable for target simulation, electronic countermeasure support, payload testing, training support, mission equipment integration, and specialized field operation scenarios. With 13h maximum endurance, 50 kg payload capacity, 5000 m maximum flight altitude, and Level 7 wind resistance, the HY180 is suitable for projects that require longer flight time, stable fixed-wing performance, and flexible payload configuration.
The HY180 supports a maximum payload capacity of 50 kg, making it suitable for different mission modules and customer-specific payload systems. Payload configuration can be customized according to the project requirements. Customers may integrate mission equipment, test modules, electronic systems, communication devices, or other specialized payloads. For accurate evaluation, we recommend providing payload weight, dimensions, mounting method, power requirements, and expected mission profile before quotation.
The HY180 supports up to 13 hours of maximum endurance, depending on payload weight, fuel configuration, flight altitude, cruise speed, wind conditions, and mission profile. For long-duration missions, actual flight time should be evaluated together with payload type, required route distance, operating altitude, and safety reserve. Our team can help review the mission requirements and recommend a suitable configuration for your project.
The HY180 has an overall length of 2850 mm, a wingspan of 2600 mm, and a height of 608 mm. It supports a 180 kg maximum takeoff weight and 50 kg maximum payload capacity. Its key flight performance includes 50 m/s cruise speed, 62 m/s maximum level speed, 5 m/s climb rate, 13h maximum endurance, 5000 m maximum flight altitude, and Level 7 wind resistance. The platform uses a piston aviation engine and is designed for long-duration fixed-wing UAV missions.
The HY180 supports rocket-assisted launch or pneumatic launcher deployment, depending on customer requirements and mission conditions. For recovery, the platform supports parachute recovery, which helps reduce dependence on runway infrastructure and improves deployment flexibility in field environments. This launch and recovery method is useful for customers who need a fixed-wing UAV platform that can operate in areas where runway access is limited.
Yes. The HY180 can be customized according to B2B project requirements. Customization may include payload mounting interface, onboard power supply, communication configuration, ground control system setup, launch support equipment, recovery system configuration, airframe finish, documentation, spare parts package, and training support. Final customization depends on payload type, mission requirements, quantity, destination country, operating environment, and applicable compliance procedures.
To provide an accurate quotation and configuration proposal, please provide the following information: Required quantity; Destination country or region; Intended application; Payload type, size, weight, and power requirements; Expected endurance, speed, altitude, and mission distance; Launch and recovery requirements; Communication and ground control requirements; Spare parts, training, and technical support needs; Customization requirements; Expected delivery schedule. This information helps us evaluate the suitable HY180 configuration, payload integration plan, lead time, and delivery arrangement.
For international B2B orders, we currently support FOB and CIF trade terms only. FOB means the buyer arranges international freight after the goods are delivered to the agreed port of shipment. CIF means we arrange freight and insurance to the agreed destination port. At this stage, we do not support DDP, DAP, EXW, or door-to-door delivery terms. For an accurate quotation, please provide your destination port, order quantity, required configuration, payload requirements, and any customization needs.