NJUAV LY

LY-Z15 is a fixed-wing UAV developed by NJUAV in conventional layout with high-wing configuration. Propulsion is provided by a propeller-driven tractor engine mounted in the nose, and landing gear consists of a pair of skids. Specification:[1]

• Length: 1.8 m
• Height: 0.5 m
• Wingspan: 2.5 m
• Max Speed: 130 km/ h
• Cruising Speed: 90 km/h
• Ceiling: 2000 m
• Max Takeoff Weight: 15 kg
• Max Payload : 3 kg
• Max Fuel Capacity : 2 kg
• Endurance: 2 h
• Max Range: 20 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 2.8 kW
• Launch: Hand thrown or catapult
• Recovery: glide or parachute

LY-Z25 is a fixed-wing UAV developed by NJUAV in conventional layout with high-wing configuration and T-tail. Propulsion is provided by a propeller driven by a pusher engine mounted behind the wing, and landing gear consists of a pair of skids. Specification:[2]

• Length: 2.2 m
• Height: 0.7 m
• Wingspan: 2.8 m
• Max Speed: 130 km/ h
• Cruising Speed: 90 km/h
• Ceiling: 2000 m
• Max Takeoff Weight: 25 kg
• Max Payload : 3.5 kg
• Max Fuel Capacity : 2.5 kg
• Endurance: 2 h
• Max Range: 20 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 2.8 kW
• Launch: Vehicle assisted or catapult
• Recovery: glide or parachute

LY-Z35 is a fixed-wing UAV developed by NJUAV in twin-boom layout with high-wing configuration and twin tails. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage, and landing gear consists of a pair of skids. Specification:[3]

• Length: 2.3 m
• Height: 0.5 m
• Wingspan: 3 m
• Max Speed: 150 km/ h
• Cruising Speed: 90 km/h
• Ceiling: 2000 m
• Max Takeoff Weight: 35 kg
• Max Payload : 3 kg
• Max Fuel Capacity : 2 kg
• Endurance: 2 h
• Max Range: 20 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 3 kW
• Launch: Vehicle assisted or catapult
• Recovery: glide or parachute

LY-Z45 is a fixed-wing UAV developed by NJUAV in twin-boom layout with high-wing configuration and twin tails. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage, and landing gear consists of a pair of skids. LY-Z45 is a larger cousin of the smaller LY-Z35. Specification:[4]

• Length: 2.5 m
• Height: 0.7 m
• Wingspan: 3.6 m
• Max Speed: 160 km/ h
• Cruising Speed: 130 km/h
• Ceiling: 3000 m
• Max Takeoff Weight: 45 kg
• Max Payload : 5 kg
• Max Fuel Capacity : 6 kg
• Endurance: 3 h
• Max Range: 50 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 5 kW
• Launch: Vehicle assisted or catapult
• Recovery: glide or parachute

LY-Z65 is a fixed-wing UAV developed by NJUAV in twin-boom layout with high-wing configuration and twin tails. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage, and landing gear consists of a pair of skids. LY-Z65 is a larger cousin of the smaller LY-Z35 and LY-Z45. Specification:[5]

• Length: 2.96 m
• Height: 0.78 m
• Wingspan: 4 m
• Max Speed: 160 km/ h
• Cruising Speed: 130 km/h
• Ceiling: 3000 m
• Max Takeoff Weight: 65 kg
• Max Payload : 15 kg
• Max Fuel Capacity : 9 kg
• Endurance: 3 h
• Max Range: 50 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 11 kW
• Launch: Vehicle or rocket assisted
• Recovery: glide or parachute

LY-Z100 is a fixed-wing UAV developed by NJUAV in twin-boom layout with high-wing configuration and twin tails. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage, and landing gear consists of a pair of skids. LY-Z100 is a larger cousin of the smaller LY-Z35, LY-Z45 and LY-Z65. Specification:[6]

• Length: 3 m
• Height: 0.8 m
• Wingspan: 4 m
• Max Speed: 180 km/ h
• Cruising Speed: 130 km/h
• Ceiling: 3500 m
• Max Takeoff Weight: 100 kg
• Max Payload : 20 kg
• Max Fuel Capacity : 16 kg
• Endurance: 4 h
• Max Range: 50/100 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 16.2 kW
• Launch: Vehicle or rocket assisted
• Recovery: glide or parachute

LY-Z200 is a fixed-wing UAV developed by NJUAV in twin-boom layout with high-wing configuration and twin tails. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage, and landing gear consists of a pair of skids. LY-Z100 is a larger cousin of the smaller LY-Z35, LY-Z45, LY-Z65, and LY-Z100. Specification:[7]

• Length: 4.5 m
• Height: 1.43 m
• Wingspan: 6 m
• Max Speed: 180 km/ h
• Cruising Speed: 150 km/h
• Ceiling: 4800 m
• Max Takeoff Weight: 200 kg
• Max Payload : 50 kg
• Max Fuel Capacity : 50 kg
• Endurance: 6 – 8 h
• Max Range: 50/100 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 28 kW
• Launch: Vehicle or rocket assisted
• Recovery: glide or parachute

LY-Z270 is a fixed-wing UAV developed by NJUAV in twin-boom layout with high-wing configuration and twin tails. Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose, and landing gear consists of a pair of skids. Specification:[8]

• Length: 5.28 m
• Height: 1.53 m
• Wingspan: 7.2 m
• Max Speed: 180 km/ h
• Cruising Speed: 130 km/h
• Ceiling: 5000 m
• Max Takeoff Weight: 270 kg
• Max Payload : 70 kg
• Max Fuel Capacity : 60 kg
• Endurance: 9.6 h
• Max Range: 200 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 33 kW
• Launch: Vehicle assisted
• Recovery: glide or parachute

LY-ZY200 is a fixed-wing UAV developed by NJUAV in twin-boom layout with high-wing configuration and twin tails. Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose, and landing gear consists of a pair of skids. LY-ZY200 is the smaller cousin of the larger LY-Z270. Specification:[9]

• Length: 4.28 m
• Height: 1.28 m
• Wingspan: 6 m
• Max Speed: 180 km/ h
• Cruising Speed: 130 – 150 km/h
• Ceiling: 6500 m
• Max Takeoff Weight: 200 kg
• Max Payload : 50 kg
• Max Fuel Capacity : 50 kg
• Endurance: 6 h
• Max Range: 50/100 km
• Max Wind Scale Allowed for Operation: 5
• Engine Power: 27.9 kW
• Launch: Vehicle assisted
• Recovery: glide or parachute

List of unmanned aerial vehicles of the People's Republic of China