Engineering:Chunyi CY-01
| CY-01 series UAV | |
|---|---|
| Role | UAV |
| National origin | China |
| Manufacturer | Chunyi |
| Designer | Chunyi |
| First flight | 2013 |
| Introduction | 2013 |
| Status | In service |
| Primary user | China |
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
References
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