Trisha Shetty (Editor)

Chunyi CY 01

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First flight
  
2013

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.

Contents

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. Specification:

  • 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.

  • 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

    • References

    Chunyi CY-01 Wikipedia
    (Text) CC BY-SA


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