Defense and tactical UAVs in flight above a rugged field environment during reconnaissance mission operations

HY180 Long-Endurance Delta-Wing Fixed-Wing UAV

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.

HY180 long-endurance delta-wing fixed-wing UAV main product image
HY180 delta-wing UAV engine and propeller detail
HY180 delta-wing UAV nose and fuselage detail
HY180 delta-wing UAV tail wing and control surface detail
HY180 delta-wing UAV wing structure detail

Key Features

  • Long-endurance delta-wing fixed-wing UAV for professional mission applications
  • 50 kg maximum payload capacity for multi-payload integration
  • 180 kg maximum takeoff weight for medium-size UAV missions
  • 13h maximum endurance for extended field operation scenarios
  • 5000 m maximum flight altitude for wider operational coverage
  • 50 m/s cruise speed and 62 m/s maximum level speed
  • 5 m/s climb rate for stable altitude gain
  • Level 7 wind resistance for stronger outdoor adaptability
  • Piston aviation engine for reliable long-duration operation
  • Supports rocket-assisted launch, pneumatic launcher deployment, and parachute recovery
  • Suitable for target simulation, electronic countermeasure support, payload testing, and specialized mission deployment

Product Overview

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.

Technical Specifications

Core Specifications
Model
HY180
UAV Type
Long-Endurance Delta-Wing Fixed-Wing UAV
Overall Length
2850 mm
Wingspan
2600 mm
Height
608 mm
Propulsion System
Piston aviation engine
Launch Method
Rocket-assisted launch or pneumatic launcher
Recovery Method
Parachute recovery
Maximum Payload Capacity
50 kg
Cruise Speed
50 m/s
Maximum Level Speed
62 m/s
Climb Rate
5 m/s
Maximum Takeoff Weight
180 kg
Maximum Endurance
13 h
Maximum Flight Altitude
5000 m
Wind Resistance
Level 7
Typical Applications
Target simulation, electronic countermeasure support, payload integration

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Frequently Asked Questions

What missions is the HY180 Long-Endurance Delta-Wing Fixed-Wing UAV suitable for?

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.

What is the payload capacity of the HY180 UAV?

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.

How long can the HY180 UAV stay in the air?

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.

What are the key performance specifications of the HY180?

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.

How does the HY180 UAV take off and recover?

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.

Can the HY180 be customized for different payloads or mission requirements?

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.

What information should I provide before requesting a quotation?

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.

What trade terms do you support for international orders?

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.