CASC Rainbow
CASC Rainbow (Chinese:
Variants
[edit]This section contains promotional content. (October 2022) |
CH-1
[edit]The CH-1 is the first of the Rainbow (CH) series UAVs. The general designer was Mr. Shi Wen (
Specifications:[3]
- 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, and catapult mounted on vehicle
- Recovery: parachute
- Max wind scale allowed for operation: 5
CH-2
[edit]The CH-2 is the second of the Rainbow (CH) series UAVs and is a development of the earlier CH-1, with identical twin-boom layout. Like the CH-1, propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage. The UAV is launched via a vehicle mounted catapult with rocket-assisted take-off.[4][5] The CH-2 is mainly intended for reconnaissance and surveillance missions.[2]
CH-3
[edit]The CH-3 is a fixed wing unmanned combat aerial vehicle (UCAV) of the Rainbow series. The CH-3 adopts an unusual canard layout, similar to the Jetcruzer 450 and the Rutan VariEze. This means that the CH-3 lacks a centrally located vertical tail, with large winglets and canards instead. Propulsion is provided by a three-blade propeller driven by a pusher engine mounted on the empennage. The main landing wheels of the tricycle landing gear has a fairing to reduce drag.[6]
In January, 2015, a CH-3 drone was reported to have crashed in northern Nigeria.[7] It is believed that the drone was involved in Nigeria's struggle against the Boko Haram militant group.[8] China supplied the CH-3 to Nigeria government prior to 2014, along with YC-200 guided bombs and AR-1 air-to-ground missiles.[9] In February of 2016, Nigeria announced a successful drone strike in its ongoing war against Boko Haram.[10]
China delivered 12 CH-3s to Myanmar in 2014-2015 to fight rebels.[11] NESCOM Burraq is thought to be mostly influenced by the CH-3 design.[12]
Specifications:[6]
- Wingspan (m): 8
- Range (km): 960
- Endurance (h): 12
- Payload (kg): 60 – 80
- Ceiling (km): 4
CH-3A
[edit]The CH-3A is a development of the earlier CH-3, with both sharing an identical layout. Improvements of the CH-3A over the CH-3, includes the maximum payload increasing to more than 100 kg and a satellite data link being incorporated. The CH3A is a multipurpose UAV which can also carry AR 1 laser guided rockets for an attacking role. It is also widely rumored that the Myanmar Air Force operates them, and some images have been found.[13]
Specification:[14]
- Payload (kg): 180 maximum
- Endurance (h): 6 with maximum payload
- Ceiling (Km): 4
- Max Range (km): 960
CH-4
[edit]Externally, the CH-4 looks almost identical to the General Atomics MQ-9 Reaper, with the only distinct visual difference between the two UAVs being the ventral fin below the V-tail on MQ-9 which is absent on the CH-4.[15][16][17] 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 life) 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 missiles from an altitude of 5,000 meters (~16,400 feet), meaning the aircraft is capable of staying outside the effective range of most anti-aircraft guns. It also allows the CH-4 to be able to fire from a position that provides a wider area of view.[18]
Vasiliy Kashin, a Chinese specialist at Moscow's Centre for Analysis of Strategies and Technologies, said that the CH-4B UCAV has been exported to Myanmar,[19][20] Pakistan, Egypt, Saudi Arabia, Algeria, and Iraq.[21][22] Myanmar is also producing a CH-4 UAV under license with an agreed transfer of technology.[23]
Iraq received an unknown number of CH-4B models in early 2015, enabling numerous battlefield reversals in conflicts surrounding Mosul and Ramadi against ISIL.[24]
Saqr-1 is thought to be mostly influenced by the CH-4.[25]
Specifications:[26]
- Length: 8.5 m (28 ft)
- Wing Span: 18 m (59 ft)
- Max Take Off Weight: 1,300 kg (2,900 lb)
- Payload: 345 kg (761 lb)
- Endurance: 40 hours
- Powerplant: 1 x 100 Hp engine
- Maximum Speed: 235 knots (435 km/h)
- Cruise Speed: 180 knots (330 km/h)
- Communications range: >1,000 km (620 mi) with SatCom (1,500-2,000 km for CH-4B),[27] ~150 km (93 mi) from Ground Control Station (GCS)
- Armaments: AR-1 missile, AR-2 missile (20 kg, 5 kg armour-piercing warhead, inertial guidance system with terminal semi-active laser (SAL) seeker, maximum range 8 km),[28] AKD-10 air-to-surface anti-tank missile, BRMI-90 90mm guided rocket, FT-7/130 130 kg glide bombs, FT-9/50 50 kg bomb, FT-10/25 25 kg bomb, GB-7/50 50 kg precision-guided munition (PGM), GB-4/100 PGM.[29]
CH-5
[edit]The CH-5 is a large UAV with a wingspan of 21 metres, a payload of 1,000 kg, a maximum takeoff weight of over 3 tonnes, a service ceiling of 9 km, an endurance life of up to 60 hours,[30] and a range of 10,000 km. Thanks to a shared data link system, it can cooperate with CH-3 and CH-4 drones. It conducted its maiden flight in August 2015[31] at its first airshow flight (in northern Hebei province) in July 2017.[30] The drone can carry a maximum of 16 missiles at a single time. There were also plans to extend its range up to 20,000 km.[32] Chinese officials claimed the CH-5 Rainbow was similar in performance to the US MQ-9 Reaper and "may come in at less than half the price". Compared to the Garrett TPE331 turboprop engine mounted on the Reaper, the CH-5 is equipped with an unidentified turbo-charged piston engine with less than half the horsepower. This design consideration limits the maximum altitude of the CH-5 to 9 km compared to the 12–15 km of the Reaper, but it also extends CH-5's endurance life to 60 hours compared to the Reaper's 14 hours.
A more recent engine variant, with a 300kW piston engine from Anhui Hangrui Co., will increase the service ceiling to 12 km and the endurance life to 120 hours.[33]
Armaments: AR-1 missile, AR-2 missile (20 kg, 5 kg armour-piercing warhead, inertial guidance system with terminal semi-active laser (SAL) seeker, maximum range 8 km)[28]
CH-6
[edit]The CH-6 is a large UAV with a MTOW of 7800 kg with two variants: a strike variant with an 18-hour endurance life and a 450 kg payload; a reconnaissance variant with a 21-hour endurance life and a 120 kg payload. It was in development in 2021.[34]
CH-7
[edit]The CH-7 is a stealth, flying wing UCAV similar to the X-47B, with a 22m wingspan and a 10m length. It can fly at 920 km/h and an altitude of 13,000m. The endurance life is around 15 hours with an operational radius of 2000 km.[35] It can carry antiradiation missiles and standoff weapons.[36][37][38] According to its chief designer, "the CH-7 can intercept radar electronic signals, and simultaneously detect, verify and monitor high-value targets, such as hostile command stations, missile launch sites, and naval vessels". It was planned to make its maiden flight in 2019 and commence production from 2022.[35]
CH-10
[edit]The CH-10 is a tiltrotor UAV.[39]
CH-91
[edit]The CH-91 is a fixed-wing UAV with a twin-boom layout and an inverted v-tail with a pair of skids acting as the landing gear. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage.[40][41] The CH-91 is mainly intended for reconnaissance and surveillance missions.[2] It is also known as the BZK-008.
CH-92
[edit]CH-92 is a fixed-wing UAV in the conventional V-tail layout with a tricycle landing gear. Propulsion is provided by a propeller driven by a pusher engine mounted at the empennage. The CH-92 is mainly intended for reconnaissance, surveillance, and attack missions.[2][42]
CH-802
[edit]The CH-802 is a fixed-wing micro air vehicle (MAV) in the conventional layout with an elevated high-wing configuration and V-tail. The CH-802 has a cylindrical fuselage with propulsion being provided by a two-blade propeller driven by a tractor brushless electric motor atop the fuselage.[43][44] The CH-803 is mainly intended for reconnaissance and surveillance missions.[2] The CH-802 program began in 2007 and was completed in 2008.
- 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
[edit]The CH-803 is a fixed-wing UAV with a cylindrical fuselage and canards, but without the tailplane. Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose. Another unique feature of the CH-803 is that it adopts a forward-swept wing.[45] The CH-803 is mainly intended for reconnaissance and surveillance missions.[2] The CH-803 program began in 2008 and was completed in 2011.
Specifications:[46]
- 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-817
[edit]VTOL micro-surveillance and attack UAV with a top speed of 64.8 km/h and an endurance of 15 minutes.[47]
CH-901
[edit]The CH-901 is a fixed-wing UAV in the conventional layout with a cylindrical fuselage and a high-wing configuration. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the end of empennage.[48] The CH-901 is designed as a UCAV.[2][49]
CH-902
[edit]Fixed-wing cylindrical UAV.[50]
Operational history
[edit]Royal Saudi Land Force
[edit]The Kingdom of Saudi Arabia have been operating the CH-4, along with the Wing Loong II drone in its military intervention in Yemen.[51]
On 12 July 2018, Houthi rebels shot down an armed Saudi Arabian CH-4 drone near Asir border.[52][53]
On 8 August 2018, Houthi rebels shot down an armed Saudi Arabian CH-4B drone near Tuwal border crossing.[54][55]
On 23 December 2018, Houthi rebels shot down a Saudi Arabian CH-4 drone.[56] in Saada province, northern Yemen, and displayed the wreckage of the drone.[57][58]
On 11 April 2019, a Saudi Arabian CH-4 drone was lost over Yemen, according to Houthi media the Saudi drone was shot down by friendly fire.[59][60]
On 7 January 2020, Houthi rebels shot down an armed Saudi Arabian CH-4B drone over Jawf province.[61][62]
On 22 December 2020, Houthi rebels shot down a Saudi Arabian CH-4B drone, serial number 20311 on the district of Madghal in Marib province.[63][64][65]
On 12 February 2021, Houthis intercepted a Saudi Arabian CASC Rainbow CH-4 drone in Meghdal, Marib Governorate, displaying footage of the CH-4 being shot down.[66][67]
On 23 March 2021, a Houthi spokesman said that Houthi forces shot down a US MQ-9 Reaper drone operating in Marib,[68] however a day later the Houthis published footage of the intercept that depicted a drone resembling the CH-4.[69][70]
On 23 May 2021, a Saudi Coalition CH-4 drone is shot down by Houthi fighters in Al-Maraziq, Al-Jawf governorate.[54][71] Later Houthi media wing released a video of the shootdown of the drone.[72]
On 6 October 2021, Houthis reported the shot down of a Saudi Arabian CASC Rainbow CH-4 drone in Juba district,[73] southern Marib province by Houthi Air Defenses, later displaying footage of the drone wreck.[74][75]
United Arab Emirates Air Force
[edit]The United Arab Emirates Air Force have been operating the CH-4, along the Wing Loong II drone in its military intervention in Yemen.[51][76]
Comparison
[edit]Model | Manufacturer | Armaments | Takeoff weight | Engine type | Maximum cruise speed | Operational endurance |
---|---|---|---|---|---|---|
CH-1 | CASC | No | 220 kg | Piston | 140 km/h | 6 hours |
CH-2 | CASC | No | 220 kg | Piston | 160 km/h | 8 hours |
CH-3 | CASC | Yes, 80 kg | 650 kg | Piston | 220 km/h | 12 hours |
CH-4 | CASC | Yes, 345 kg | 1330 kg | Piston | 180 km/h | 30 hours for recon / 12 hours for strike |
CH-5 | CASC | Yes, 1000 kg | 3300 kg | Turboprop | 220 km/h | 60 hours for recon / 30 hours with 8 AR-1 missiles |
GJ-1 (Wing Loong 1) | Chengdu | Yes, 200 kg | 1100 kg | Piston | 280 km/h | 20 hours |
GJ-2 (Wing Loong 2)[78] | Chengdu | Yes, 480 kg | 4200 kg | Turboprop | 370 km/h | 32 hours / 20 hours at max speed |
Wing Loong 3[79] | Chengdu | Yes, 2300 kg | 6200 kg | Turboprop | Unknown | 40 hours |
Chengdu WZ-10 | Chengdu | Yes, 400 kg | 3200 kg | Turbojet | 370 km/h | 32 hours |
WJ-700[80] | CASIC | Yes | 3500 kg | Turbofan | Unknown | 20 hours |
WJ-600 A/D[81] | CASIC | Yes | Unknown | Turbofan | 850 km/h | 5 hours |
TB-001A[82] | Tengdeng | Yes, 1200 kg | 3200 kg | Turboprop | Unknown | 35 hours at 1000 kg payload |
Operators
[edit]- Algerian People's National Armed Forces: CH-3 and CH-4[83]
- People's Liberation Army Ground Force: KVD002, a reconnaissance and precision strike drone based on the CH-4.[84]
- Indonesian Armed Forces: six CH-4Bs[28][88][27]
- Myanmar Air Force: Acquired 12 CH-3As and some CH-4s for precision airstrike mission.[94][95][87][96] Myanmar is also producing the CH-4 model with the transfer of technology under license.[97]
- Nigerian Air Force: CH-3[9] and CH-4
- Pakistan Armed Forces: Known to use the CH-3 inspired UCAVs like the GIDS Shahpar since 2012.[98] Procured 12-24 CH-4A/B UCAVs in late January 2021.[99][100]
- Serbian Air Force and Air Defence: CH-92A and CH-95[101]
- Turkmen Air Force: CH-3[102]
- United Arab Emirates Armed Forces: CH-4 [87]
See also
[edit]Related lists
References
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