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CASC Rainbow

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CASC Rainbow (Cai Hong, abbreviated as CH) is the name of a series Chinese UAVs developed by China Academy of Aerospace Aerodynamics of China Aerospace Science and Technology Corporation (CASC), also known as the 11th Academy of CASC, or 701st Research Institute.

Contents

CH-1

CH-1 is the first member of the Rainbow (CH) series UAV. The general designer was Mr. Shi Wen (石文), who is also the general designer of CH-2, the successor of CH-1, CASC PW-1, the derivative of CH-1, and CASC PW-2, the derivative of CH-2. CH-1 program first begun in 2000, and the success of CH-1 resulted in the establishment of UAV program which eventually led to other designs that followed. CH-1 is mainly intended for reconnaissance and surveillance missions. Specification:

  • Wingspan (m): 4.4
  • Length (m): 3.75
  • Height (m): 0.87
  • Weight (kg): 40
  • Payload (kg): 4.5
  • Fuel (kg): 26
  • Max speed (km/h): 170
  • Cruise speed (km/h): 120 – 150
  • Normal radius (km): > 100
  • Normal operating altitude (km): 1 – 3
  • Ceiling (km): 4.6
  • Max range (km): 740 @ 1 km altitude and 124 km/h speed
  • Endurance (h): 6
  • Rate of climb (m/s): 4.3
  • Turn radius (m): 290
  • g overload: - 1.5 to 3
  • Launch: rocket assisted + catapult mounted on vehicle
  • Recovery: parachute
  • Max wind scale allowed for operation: 5
  • CH-2

    CH-2 is second member of Rainbow (CH) series UAV and it is a development of earlier CH-1, with identical twin-boom layout. As with its predecessor CH-1, propulsion of CH-2 is also provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage, and the UAV is launched via vehicle mounted catapult with rocketed assisted take-off. CH-2 is mainly intended for reconnaissance and surveillance missions.

    CH-3

    CH-3 is a fixed wing UCAV of the Rainbow series. CH-3 adopts the unusual canard layout, similar to the Jetcruzer 450 and the Rutan VariEze. This means that the CH-3 lacks centrally located vertical tail, but has large winglets and canards. Propulsion is provided by a three-blade propeller driven by a pusher engine mounted on empennage. The main landing wheels of the tricycle landing gear has fairing to reduce drag.

    In January, 2015, a CH-3 drone was reported to have crashed in the north of Nigeria. It is believed the drone was involved in Nigeria's struggle against the Islamic militant group, Boko Haram. China supplied the CH-3 to Nigeria government prior to 2014, along with YC-200 guided bombs and AR-1 air-to-ground missile.

    Specification:

  • Wingspan (m): 8
  • Range (km): 960
  • Endurance (h): 12
  • Payload (kg): 60 – 80
  • Ceiling (km): 4
  • CH-3A

    CH-3A is the development of CH-3 and share the identical layout. Improvement of CH-3A over CH-3 includes that the maximum payload is increased to more than 100 kg, and satellite data link is also incorporated. CH3A is a miltipurpose UAV which can also carry AR 1 laser guided rocket for attacking role.Bangladesh Armed Forces operates these drones as of 2015. It is also widely rumoured that Myanmar Air Force operates them,and some images have been found,but theres no confirmation.Specification:

  • Payload (kg): 180 maximum
  • Endurance (h): 6 with maximum payload
  • Ceiling (Km): 4
  • Max Range (km): 960
  • CH-4

    CH-4 is the largest fixed wing UCAV of the Rainbow series (as of end of 2013). Externally, CH-4 looks almost identical to General Atomics MQ-9 Reaper, and the only distinct visual difference between two UAVs is that the ventral fin below the V-tail on MQ-9 is absent on CH-4. There are two versions, the CH-4A and CH-4B. The CH-4A is a reconnaissance drone (capable of a 3500–5000 km range and a 30- to 40-hour endurance) while the CH-4B is a mixed attack and reconnaissance system with provisions for 6 weapons and a payload of up to 250 to 345 kg.

    CH-4 is capable of firing air-to-ground missile from altitude of 5,000 meters, therefore the aircraft can stay outside of effective range of most anti-aircraft guns. It also allow CH-4 to be able to fire from a position that provides wider viewing area.

    Vasiliy Kashin, a China specialist at Moscow's Centre for Analysis of Strategies and Technologies, said that The CH-4B UCAV has been exported to Egypt, Saudi Arabia and Iraq.

    CH-5

    Latest UCAV of the Rainbow series, with a payload of 1000 kg, a maximum takeoff weight of over 3 tons, a service ceiling of 10 km, and an endurance up to 60 hours with range of 6500 km. Thanks to shared data link it can cooperate with CH-3 and CH-4 drones. It conducted its maiden flight in August 2015. The drone can carry up to 24 missiles at a single time. There are also plans to extend its endurance and range to 120 hours and 20000 km, respectively.

    CH-91

    CH-91 is a fixed-wing UAV in twin-boom layout with inverted v-tail and a pair of skids as landing gear. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage. CH-91 is mainly intended for reconnaissance and surveillance missions. It's also called as BZK-008.Used by Bangladesh Armed Forces for reconnaissance duties.

    CH-92

    CH-92 is a fixed-wing UAV in conventional layout with V-tail and tricycle landing gear. Propulsion is provided by a propeller driven by a pusher engine mounted at the empennage. CH-92 is mainly intended for reconnaissance and surveillance missions.

    CH-802

    CH-802 is a fixed wing micro air vehicle (MAV) in conventional layout with elevated high-wing configuration and V-tail. CH-802 has a cylindrical fuselage and propulsion is provided by a two-blade propeller driven by a tractor brushless electric motor atop of the fuselage. CH-803 is mainly intended for reconnaissance and surveillance missions. CH-802 program begun in 2007 and was completed in 2008. Specification:

  • Wingspan (m): 3
  • Length (m): 1.8
  • Weight (kg): 6.5
  • Payload (kg): 1
  • Radius (km): 30
  • Normal operating altitude (km): 0.3 – 1
  • Normal radius (km): 30 – 50
  • Cruise speed (km/h): 60
  • Endurance (h): 2.5
  • Ceiling (km): 4
  • Launch: by hand
  • CH-803

    CH-803 is a fixed-wing UAV with a cylindrical fuselage and canards, but without tailplane. Propulsion is provided by two-blade propeller driven by a tractor engine mounted in the nose. Another unique feature of CH-803 is that it adopts forward-swept wing. CH-803 is mainly intended for reconnaissance and surveillance missions. CH-803 program begun in 2008 and was completed in 2011. Specification:

  • Wingspan (m): 3
  • Length (m): 1.8
  • Weight (kg): 18
  • Payload (kg): 3.5
  • Radius (km): 30
  • Normal operating altitude (km): 0.5 – 1.5
  • Normal radius (km): 50 – 80
  • Cruise speed (km/h): 80 – 110
  • Endurance (h): 5
  • Ceiling (km): 3.5
  • Launch: catapult
  • Recovery: parachute
  • CH-901

    CH-901 is a fixed-wing UAV in conventional layout with cylindrical fuselage and high-wing configuration. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the end of empennage. CH-901 is designed as an UCAV.

    Operators

     Egypt
  • Egyptian Air Force: CH-4B
  •  Iraq
  • Iraqi Army: CH-4B
  •  Nigeria
  • Nigerian Army: 2 CH-3
  •  Turkmenistan
  • Turkmen Air Force: CH-3
  • References

    CASC Rainbow Wikipedia


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