Chunyi CY-01

Chunyi CY-01 UAVs are Chinese UAVs developed by Beijing Chunyi Aviation Science and Technology Co., Ltd. (Chunyi, 北京淳一航空科技有限公司), and most of them have entered service with Chinese military governmental establishments.

CY-01H Hua Ying

CY-01H Hua Ying (Hua-Ying or Huaying, 华英) is fixed-wing UAV developed by Chunyi in twin-boom layout with twin tail and tricycle landing gear. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage.^[1] Specification:^[2]

• Length (m): 2.3
• Wingspan (m): 2.9
• Wing area (m²): 0.96
• Height: 0.66
• Empty weight (kg): 10
• Payload (kg): 5–10
• Max take-off weight (kg): 20
• Fuel (L): 3–6
• Max speed (km/h): 150
• Cruise speed (km/h): 110
• Ceiling (km): 4
• Endurance (h): 1.5–3
• Range (km): 150
• Max wind scale allowed for operation: 6
• Launch: taxiing or catapult
• Recovery: taxiing or parachute
• Storage container size (m): 1.45 × 70 × 55
• Stall speed (km/h): 80
• Power plant: 4 kW twin cylinder

CY-01V Hua Ying

CY-01V Hua Ying (Hua-Ying or Huaying, 华英) is fixed-wing UAV developed by Chunyi in twin-boom layout with inverted v-tail and tricycle landing gear. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage.^[3]

• Length (m): 2.3
• Wingspan (m): 2.9
• Wing area (m²): 0.96
• Empty weight (kg): 10
• Payload (kg): 5
• Max take-off weight (kg): 20
• Fuel (L): 3–6
• Max speed (km/h): 150
• Cruise speed (km/h): 110
• Ceiling (km): 4
• Endurance (h): 1.5
• Range (km): 150
• Max wind scale allowed for operation: 6
• Launch: taxiing or catapult
• Recovery: taxiing
• Stall speed (km/h): 80
• Power plant: 4 kW gasoline-powered piston engine

See also

• List of unmanned aerial vehicles of China
• Chunyi CY
• Chunyi CY-05
• Chunyi UAV

References