The system encompasses the overall assembly, commissioning, and testing of light armor, ground vehicles, radar antennas, shelters, and personnel, and can be delivered in conjunction with artillery systems or independently. The system also includes the research and development and production of supporting equipment and ground support equipment for the MQ-55 loitering munition.
The special-purpose UAV and loitering munition product is the 55kg-class loitering munition 3-piece (MQ-55 loitering munition). This munition is an integrated design combining an infrared/image-guided precision-guided reconnaissance and strike UAV launched by artillery and a multi-functional warhead, with gas-powered catapult launch. The loitering munition achieves integrated reconnaissance and strike capabilities through mission allocation, route planning, and autonomous coordination. The primary objective is to develop customized special-purpose drones and loitering munitions. These are custom-made products, and other similar products on the market cannot be used on specific artillery models, possessing uniqueness and exclusivity. The loitering munition's technical solutions were developed and validated by the company's R&D department, achieving comprehensive optimization of the munition's overall structure, aerodynamics, strength, shape, and flight control. The company is responsible for the entire munition. The MQ55 loitering munition is a core subsystem of the swarm warfare system (gun, drone, and munition) used with the SR5 howitzer. The SR5 howitzer has been finalized and is being mass-produced and deployed domestically. Additionally, the company.
| An unmanned aerial vehicle (UAV) system consists of an airborne segment and a ground segment. | |
| The airborne segment comprises the UAV platform, onboard avionics, onboard data link, and mission payload. The ground segment consists of ground telemetry, tracking, and command (TT&C) equipment, ground control terminals, and launching devices. |
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| Flight Control Unit | Firepower control unit |
| Flight Control: Takeoff, Cruise, Return, Landing; Motor Control: Attitude Control; Integrated Navigation: Position Calculation, Attitude Calculation; Safety Assurance: Link Breakage Return, Parachute Recovery, Fault Detection; Data Management: Communicating with data links and sensors, data storage, evaluation and analysis. |
Generalized load control Optical equipment control Multi-mode warhead control |
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| Power Unit | Integrated Data Link for Image and Data Communication |
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| Ground Command and Control System | Optoelectronic pod |
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| Multi-mode warhead technical parameters: | |
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Launch system parameters | |||||||||
| No. | Parameter Item | Parameter Value | ||||||||
| 1 | Launcher front support dimensions | 1300*1300*1500 (mm) | ||||||||
| 2 | Large launcher support dimensions | 1500*1000*1000 (mm) | ||||||||
| 3 | Launch tube dimensions | 4200*340*340 (mm) | ||||||||
| 4 | Inner diameter | 240 (mm) | ||||||||
| 5 | Launch weight | >60kg | ||||||||
| 6 | Launch method | Gas launch | ||||||||
| 7 | Operating air pressure | >2.5Mpa | ||||||||
| 8 | Launch elevation angle | 10° | ||||||||
| 9 | Total weight (excluding gas booster) | >300kg | ||||||||
| 10 | UAV exit velocity | <40m/s | ||||||||
  
  
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| No. | Project | Indicators | ||||||||
| 1 | Operational Area | Wide-area search, identification, and destruction of various ground cluster targets within a 30 square kilometer operational area | ||||||||
| 2 | Launch Method | SR5 storage and launch container gas-propelled bomb launch, zero-field launch, helicopter delivery, etc. | ||||||||
| 3 | Mission Radius | 50km (forward flight range: not less than 30km) | ||||||||
| 4 | Attack Strategy | Scenario-based (personnel bypass, mission can be re-injected) collaborative network attack | ||||||||
| 5 | Network Scale | Mission leader ground control, mission leader and 31 follower missiles Network Configuration | ||||||||
| 6 | Ejection Launch Capacity | Catapult takeoff weight ≤ 55kg | ||||||||
| 7 | Endurance | Endurance k1h | ||||||||
| 8 | Cruise Speed | 140km/h–180km/h | ||||||||
| 9 | Power | Battery + Motor + Propeller | ||||||||
| 10 | Mission Payload | Maximum payload 15kg (multi-mode warhead 8.8kg, three-light seeker, etc., warhead explosive charge < 5kg)6000m (altitude) | ||||||||
| 11 | Service Ceiling | 6000m (altitude) | ||||||||
| 12 | Environmental Adaptability |
1) Wind resistance: Level 5 (surface wind speed) for catapult launch, Level 6 for flight phase;
2) Operating temperature: -40°C to +60°C (onboard equipment), -20°C to +40°C (ground equipment); 3) Storage temperature: -40°C to +65°C; 4) Relative humidity: ≤95% (+25°C). |
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