Chunyi UAV

Chunyi 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 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 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

CY-02 Small White
CY-02 Small White (Xiao-Bai or Xiaobai, 小白) ) is fixed wing UAV developed by Chunyi in conventional layout with high wing configuration and tricycle landing gear. Propulsion is provided by a two-blade propeller driven tractor engine mounted in the nose. Specification:
 * Length (m): 2.08
 * Wingspan (m): 2.7
 * Wing area (m2): 0.86
 * Empty weight (kg): 5.5
 * Payload (kg): 5
 * Max take-off weight (kg): 18
 * Fuel (L): 3
 * Max speed (km/h): 140
 * Cruise speed (km/h): 90
 * Ceiling (km): 4
 * Endurance (h): 1.5–2
 * Range (km): 250
 * Remote control radius: 100 km
 * Max wind scale allowed for operation: 6
 * Launch: taxiing or catapult
 * Recovery: taxiing or parachute
 * Operating temperature (°C): -10 to 55
 * Storage temperature (°C): -40 to 65
 * Deployment time (min): < 15
 * Recover time (min): < 10
 * Mean time between failures (h): > 100
 * Mean time to repair (h): < 0.5
 * Power plant: Komatsu 3W-56 gasoline engine

CY-03 Big White
CY-03 Big White (Da-Bai or Dabai, 大白) is fixed wing UAV developed by Chunyi in conventional layout with high wing configuration and tricycle landing gear. Propulsion is provided by a two-blade propeller driven tractor engine mounted in the nose. has almost identical appearance with Iflyer Big White 3 because both share the same airframe, and the main difference between the tow UAVs in in their respective flight control systems which are totally different from each other because each company developed its own flight control system for the platform. The perform of both UAVs are also almost identical to each other. Specification:
 * Wingspan: 2.95 m
 * Length: 2.3 m
 * Max speed: 135 km/h
 * Min speed: 65 km/h
 * Empty weight: 22 kg
 * Max takeoff weight: 35 kg
 * Normal payload: 6–8 kg
 * Max payload: 16 kg
 * Fuel: 8 L
 * Cruise speed: 90–110 km/h depending on payload
 * Ceiling: 5 km
 * Endurance: 2–3 h depending on payload
 * Rate of climb: 6–8 m/s depending on payload
 * Max wind scale allowed for operation: 5
 * Launch: catapult or takeoff
 * Takeoff distance: 100 m

CY-04 Crow
CY-04 Crow (Wu-Ya or Wuya, 乌鸦) is a hand held micro air vehicle (MAV) developed by Chunyi for battlefield surveillance / reconnaissance. Constructed of composite material, CY-04 Crow is in conventional layout and high wing configuration. Propulsion is provided by a propeller driven push engine mounted behind the wing and it can be quickly assembled and disassembled in the field for rapid deployment. CY-04 Crow is similar in size with AeroVironment RQ-11 Raven and performans similar missions. Specification:
 * Length (m): 1.4
 * Wingspan (m): 2.1
 * Wing area (m2): 0.5
 * Empty weight (kg): 1.2
 * Payload (kg): 1
 * Max take-off weight (kg): 3.5
 * Power plant: lithium battery
 * Max speed (km/h): 90
 * Cruise speed (km/h): 50
 * Rate of climb (m/s): 3
 * Endurance (min): 40–60
 * Range (km): > 30
 * Max wind scale allowed for operation: 4
 * Launch: hand thrown
 * Recovery: taxiing / glide
 * Take-off speed (km/h): 20
 * Storage container size (m): 0.8 × 0.31 × 0.36
 * Stall speed (km/h): 25

CY-05 Quick Eye
CY-05 Quick Eye (Kuai-Yan or Kuaiyan, 快眼) is fixed wing UAV developed by Chunyi in twin boom layout with inverted Pelikan tail and tricycle landing gear. Propulsion is provided by a two-blade propeller driven pusher engine mounted at the rear end of the fuselage. The twin boom are not attached to the wing as in most twin boom designs, but instead, they are raised from the fuselage. CY-5 Quick Eye has almost identical appearance with PUT UAV PLT06 because both share the same airframe, and the main difference between the tow UAVs in in their respective flight control systems which are totally different from each other because each company developed its own flight control system for the platform. The perform of both UAVs are also almost identical to each other. Specification:
 * Length: 2.03 m
 * Wingspan: 2.3 m
 * Wing area: 0.8 m2
 * Height: 0.58 m
 * Max take-off weight: 18 kg
 * Empty weight: 5.5 kg
 * Payload: 5 kg
 * Fuel: 4 L
 * Max speed: 150 km/h
 * Cruise speed: 100 km/h
 * Endurance: 2.5 h
 * Range: 120 km (radius)
 * Ceiling: 5 km
 * Max wind scale allowed for operation: 6
 * Rate of climb: 5 m/s
 * Take-off: Taxiing
 * Landing: Taxiing
 * Power plant: 4 kW gasoline engine

CY-07
CY-07 is fixed wing UAV developed by Chunyi in twin boom layout with twin tails and tricycle landing gear. CY-07 is powered by two engines both of which are mounted on the fuselage, a tractor engine in the nose, and a pusher engine at the end. Both engines are equipped with two-blade propeller.

CY-08 Flying Saucer with Delta Wing
CY-08 Flying Saucer with Delta Wing is fixed wing UAV developed by Chunyi in blended wing body layout with twin tails and tricycle landing gear. Propulsion is provided by a two-blade propeller driven pusher engine mounted at the end fo empennage. A unique feature of CY-08 is that its twin tails are pointing downward instead of upward as most aircraft designs. The complete name for CY-08 is Flying Saucer with Delta Wing UAV (Fei-Die San-Jiao-Yi Wu-Ren-Ji, 飞蝶三角翼无人机).

CY-10
CY-10 is a fixed wing UAV developed by Chunyi in delta wing layout with mid wing configuration. The fuselage is constructed of composite material and it has tricycle landing gear. Propulsion is provided by a two-blade propeller driven pusher engine mounted at the end fo empennage. A unique feature of CY-10 is that its winglets are pointing downward, in stead of upward as in most cases. The complete name for CY-10 is Large Delta Wing UAV (Fei-Die San-Jiao-Yi Wu-Ren-Ji, 大三角翼无人机). Specification
 * Length (m): 2.65
 * Wingspan (m): 3.55
 * Wing area (m2): 2.1
 * Empty weight (kg): 30
 * Payload (kg): 30
 * Max take-off weight (kg): 70
 * Fuel (L): 20
 * Max speed (km/h): 180
 * Cruise speed (km/h): 120
 * Ceiling (km): 5
 * Endurance (h): 5
 * Range (km): 500
 * Max wind scale allowed for operation: 6
 * Launch: taxiing
 * Recovery: taxiing or parachute
 * Take-off distance (m): 100–200
 * Landing distance (m): 100–200
 * Stall speed (km/h): 80
 * Power plant: Komatsu 3W210/212

F-16 Simulation Drone
F-16 Simulation Drone developed by Chunyi externally resembles a scaled down version of F-16, and it is designed to provide realistic training for ground based air defense forces to positively identify F-16s visually.

F-22 Simulation Drone
F-22 Simulation Drone developed by Chunyi externally resembles a scaled down version of F-22, and it is designed to provide realistic training for ground based air defense forces to positively identify F-22s visually. Specification:
 * Length (m): 2.1
 * Wingspan (m): 1.5
 * Height (m): 0.5
 * Power plant: P-120 turbojet
 * Max take-off weight (kg): 15
 * Speed (km/h): 280