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

HY2400 Turbojet Canard Delta-Wing UAV

A turbojet-powered canard delta-wing UAV with 600 km range, 30 kg payload capacity, 150 kg maximum takeoff weight, 2h endurance, and 300 km/h maximum level speed for defense, target simulation, electronic countermeasure support, and tactical field applications.

HY2400 turbojet canard delta-wing UAV main product image
HY2400 turbojet canard delta-wing UAV airframe structure detail
HY2400 turbojet canard delta-wing UAV canard wing detail
HY2400 turbojet canard delta-wing UAV nose detail
HY2400 turbojet canard delta-wing UAV tail propulsion detail

Key Features

  • Turbojet-powered fixed-wing UAV for high-speed tactical applications
  • Canard delta-wing aerodynamic layout for stable high-speed flight
  • 600 km maximum range for extended mission coverage
  • 30 kg effective payload capacity for mission-focused configuration
  • 150 kg maximum takeoff weight for medium-size fixed-wing UAV applications
  • 2h maximum endurance depending on payload and mission profile
  • 200 km/h cruise speed and 300 km/h maximum level speed
  • 6000 m maximum flight altitude for wider operational coverage
  • Level 7 wind resistance for stronger environmental adaptability
  • Suitable for target simulation, defense training, electronic countermeasure support, and tactical field operation scenarios

Product Overview

The HY2400 Turbojet Canard Delta-Wing UAV is a high-speed fixed-wing UAV platform designed for defense, tactical training, target simulation, electronic countermeasure support, and specialized field operation scenarios. Its canard delta-wing configuration and turbojet propulsion system provide strong speed performance, stable flight capability, and long-range mission flexibility. With a wingspan of 2.4 m, fuselage length of 2.35 m, maximum takeoff weight of 150 kg, and effective payload capacity of 30 kg, the HY2400 offers a practical balance between payload capability, speed, endurance, and operational range. The platform supports up to 2 hours of endurance, 600 km range, 6000 m maximum flight altitude, 200 km/h cruise speed, and 300 km/h maximum level speed, making it suitable for professional B2B defense and specialized UAV project requirements.

Technical Specifications

Core Specifications
Model
HY2400
UAV Type
Turbojet Canard Delta-Wing Fixed-Wing UAV
Wingspan
2.4 m
Fuselage Length
2.35 m
Maximum Flight Altitude
6000 m
Maximum Takeoff Weight
150 kg
Maximum Endurance
2 h
Effective Payload Capacity
30 kg
Cruise Speed
200 km/h
Maximum Level Speed
300 km/h
Wind Resistance
Level 7
Maximum Range
600 km
Propulsion System
Turbojet-powered

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Frequently Asked Questions

What missions is the HY2400 Turbojet Canard Delta-Wing UAV suitable for?

HY2400 is a turbojet-powered high-speed fixed-wing UAV platform designed for professional defense, tactical training, target simulation, electronic countermeasure support, and specialized field operation scenarios. With 600 km maximum range, 300 km/h maximum level speed, 30 kg effective payload capacity, and 6000 m maximum flight altitude, it is aligned with mission-focused high-speed UAV applications.

What makes HY2400 different from conventional fixed-wing UAVs?

HY2400 uses a canard delta-wing aerodynamic layout and turbojet propulsion, unlike conventional propeller-driven fixed-wing UAVs. This configuration supports higher speed, stable high-speed flight behavior, and stronger mission flexibility, making it better aligned with high-speed defense and test-related mission profiles.

What are the key performance specifications of the HY2400 UAV?

HY2400 has a 2.4 m wingspan and 2.35 m fuselage length, with 150 kg maximum takeoff weight and 30 kg effective payload capacity. Key flight performance includes up to 2 h endurance, 600 km maximum range, 200 km/h cruise speed, 300 km/h maximum level speed, 6000 m maximum flight altitude, and Level 7 wind resistance.

What payload capacity does HY2400 support?

HY2400 supports up to 30 kg effective payload capacity. Payload configuration can be customized for mission equipment, test modules, electronic systems, and other project-specific payloads. For accurate evaluation, provide payload weight, dimensions, mounting requirements, power requirements, and intended mission scenario.

Can HY2400 be customized?

Yes. HY2400 can be customized for B2B project requirements, including payload integration, communication configuration, ground control setup, launch support equipment, airframe finish, documentation, spare parts packages, and training support. Final scope depends on mission requirements, quantity, destination country, and applicable compliance procedures.

What information should I provide before requesting a quotation?

Please provide required quantity, destination country or region, intended application, required payload type and weight, expected range/speed/altitude requirements, ground control and communication requirements, launch or support equipment requirements, preferred Incoterm (FOB/CIF), spare parts and training needs, customization requirements, and expected delivery schedule. This information helps define suitable configuration, lead time, and delivery arrangement.

Do you provide technical support and training?

Yes. For B2B projects, we provide technical documentation, operation guidance, spare parts recommendations, configuration support, and training options based on project scope. Support can include operation guidance, maintenance instructions, ground control support, payload integration consultation, remote technical support, and project-based training.

What trade terms do you support for international orders?

For international B2B orders, standard trade terms are FOB and CIF. Under FOB, the buyer arranges international freight after goods are delivered to the agreed port of shipment. Under CIF, we arrange freight and insurance to the agreed destination port. DDP, DAP, EXW, and door-to-door delivery are not included in the standard scope and can be discussed case by case for specific projects.