A.System Architecture

1.radar warning system

Large vertical take-off fixed-wing UAVs carry active phased array radars and perform long-range early warning missions in the air

2.Interceptor launcher

Catapult launch: can be launched immediately, no runway required

Compatible with vehicle-mounted/fixed-position dual-mode deployment.

3.Interceptor flight platform

1)turbojet engine

●Maximum thrust 80kg

●Maximum flight speed 700km/h

●Minimum flight speed 150km/h

●Range: AWACS: 4 hours, strike aircraft: 1 hour

2)Flying wing configuration

●Variable fixed wing

●Wingspan 2.8 meters

●Intelligent skin: (thermal control and anti-icing capabilities)

3)Operating temperature

40℃~60℃

4)Payload

●Maximum take-off weight 120 kg

●Payload 50 kg, 400 rounds, more than 10 rounds to shoot down a Shahid urban attack drone within 50 km

5)Navigation method

●Inertial/GNSS/terrain matching, triple redundancy

●GNSS-denied environment (without satellite positioning system)

●Positioning error ≤ 100 meters

●Can return home autonomously

4.Electro-optical composite guidance module (on interceptor aircraft)

1)Build a closed loop of "reconnaissance-control-strike-evaluation": (autonomous reconnaissance, lock control, strike, and evaluation complete the closed loop)

2)Infrared band: Refrigerated infrared detection: (15-20 times longer than ordinary infrared detection distance) 15-20 kilometers

3)Interceptor laser ranging: 1500 meters accuracy ±0.5 meters

4)Visible light tracking: 4K@120fps Intelligent recognition algorithm: (AI algorithm for high-definition video)

5)Multi-source fusion: target classification and threat assessment completed in 0.2 seconds

5.Airborne weapon systems

1)Universal adapter: can be equipped with various mainstream machine guns, 5.8 or 5.56mm small caliber bullets are recommended. Buyers are required to provide the gun model for configuration

2)Intelligent stabilization system: six-axis gyro platform compensates for flight attitude disturbances

3)Ballistic computer: Real-time calculation of wind speed, altitude, and relative speed variables

4)Designed for autonomous decision-making: autonomously select the launch time based on the target lock situation

6.Covering area:

1)A medium-sized system can defend a city, 

2)and a large system can defend an entire country's borders (1 AWACS + 4 interceptors, covering an area of 3,000 square kilometers).

B.Operational Process

1.Radar warning trigger

1)The radar on the AWACS (large vertical take-off fixed-wing drones equipped with active phased array radars, used for long-range early warning missions in the air) can identify drones or swarms from up to 50 kilometers away and generate an intercept plan. It can be launched manually or automatically.

2)Moreover, we don't need our early warning aircraft. If others report an early warning, we can also fly over to intercept it.

2.Lightning Strike

The catapult pushes the interceptor to its operating speed, and the turbojet engine takes over to accelerate, achieving the longest possible interception.

3.Intelligent Hunting

1)Conventional target precision fire mode:

for medium and low speed single targets: medium-sized fixed-wing suicide drones such as Shahid 136

2)Airborne weapon system configuration:

●Real-time calculation of trajectory by computer:

- Wind speed vector (0-15 m/s compensation)

-Relative speed (0-400 km/s difference)

- Altitude difference (0-2000m trajectory correction)

●The six-axis stabilization platform is activated to offset the vibration of the body

●Ammunition Selection:

●Small caliber general-purpose machine gun ammunition

●Three-round test firing → calibration firing → full-automatic rapid firing

4.Damage Assessment

The airborne optoelectronic system transmits the strike effect in real time and automatically triggers a secondary attack if the target is not destroyed.

5.Autonomous return to home

To start energy saving mode after completing a task:

●Navigate to the recovery area for parachute landing/roll landing

●Landing accuracy circle radius ≤ 30 meters

C.Major technological breakthroughs

1.Miniaturization of turbojet engines

It uses a 3D printed combustion chamber, with a thrust-to-weight ratio of 8:1 and a life cycle of 200 hours.

2.Aerial Shooting Stabilization Technology

Microsecond-level posture prediction algorithm.

Dispersion at 200 meters ≤ 2 milliradians

3.Smart Energy Management

Power distribution in combat mode and return mode:

1)Interception phase: Thrust reaches 90%, reaching the target area at high speed

2)Return phase: Thrust reaches 40% , maintain cruising, and return at low speed

4.Anti-interference communication

Frequency hopping/spread spectrum/microwave three-mode data link with the ground command center (anti-interference communication means) maintains >98% communication reliability in strong electromagnetic interference environment.

D.Delivery time: 

3 months, including testing. Freight charter or rail