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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.〔(CY-01 )〕 Specification:〔(CY-01H )〕 *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 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Chunyi CY-01」の詳細全文を読む スポンサード リンク
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