CASC Rainbow
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CASC Rainbow (''Cai Hong'', abbreviated as CH) is a series of
unmanned aerial vehicle An unmanned aerial vehicle (UAV), commonly known as a drone, is an aircraft without any human pilot, crew, or passengers on board. UAVs are a component of an unmanned aircraft system (UAS), which includes adding a ground-based controll ...
s (UAVs) developed by the
China Academy of Aerospace Aerodynamics China Academy of Aerospace Aerodynamics or CAAA (in Chinese: 中国航天空气动力技术研究院) is a research and manufacturing organization for rockets, missiles and unmanned aerial vehicles (UAVs). Headquartered in Beijing, China, it is a ...
, an entity under the
China Aerospace Science and Technology Corporation The China Aerospace Science and Technology Corporation, or CASC, is the main contractor for the Chinese space program. It is state-owned and has subsidiaries which design, develop and manufacture a range of spacecraft, launch vehicles, strategi ...
(CASC). The China Academy of Aerospace Aerodynamics is also known as the 11th Academy of CASC, or 701st Research Institute.


Variants


CH-1

CH-1 is the first of the Rainbow (CH) series UAVs. 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. The CH-1 program began in 2000, and its success resulted in the establishment of the UAV program that led to other designs that followed. The 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 the second of the Rainbow (CH) series UAVs and is a development of the earlier CH-1, with identical
twin-boom A twin-boom aircraft is characterised by two longitudinal booms (extended nacelle-like bodies). The booms may contain ancillary items such as fuel tanks and/or provide a supporting structure for other items. Typically, twin tailbooms support ...
layout. As for the CH-1, propulsion is provided by a two-blade propeller driven by a
pusher engine A bank engine (United Kingdom/Australia) (colloquially a banker), banking engine, helper engine or pusher engine (North America) is a railway locomotive that temporarily assists a train that requires additional power or traction to climb a grad ...
mounted at the rear end of the fuselage, and the UAV is launched via vehicle mounted catapult with rocketed assisted take-off. The CH-2 is mainly intended for reconnaissance and surveillance missions.


CH-3

CH-3 is a fixed wing
unmanned combat aerial vehicle An unmanned combat aerial vehicle (UCAV), also known as a combat drone, colloquially shortened as drone or battlefield UAV, is an unmanned aerial vehicle (UAV) that is used for intelligence, surveillance, target acquisition, and reconnaissance ...
(UCAV) of the Rainbow series. The CH-3 adopts an unusual canard layout, similar to the
Jetcruzer 450 The AASI Jetcruzer was an American single turboprop light civil transport made by Advanced Aerodynamics and Structures Inc. The Jetcruzer had an unusual configuration, with a single turboprop engine driving a pusher propeller, a prominent canard ...
and the
Rutan VariEze The Rutan VariEze is a composite, canard aircraft designed by Burt Rutan. It is a high-performance homebuilt aircraft, hundreds of which have been constructed. The design later evolved into the Long-EZ and other, larger cabin canard aircraf ...
. This means that the CH-3 lacks centrally located vertical tail, but has large
winglet Wingtip devices are intended to improve the efficiency of fixed-wing aircraft by reducing drag. Although there are several types of wing tip devices which function in different manners, their intended effect is always to reduce an aircraft' ...
s and canards. Propulsion is provided by a three-blade propeller driven by a pusher engine mounted on
empennage The empennage ( or ), also known as the tail or tail assembly, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an arrow.Crane, Dale: ''Dictionary of Aeronautical Terms, third e ...
. 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 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. In February, 2016, Nigeria announced a successful drone strike in its ongoing war against Boko Haram. China delivered 12 CH-3 to Myanmar in 2014-2015 to fight rebels.
NESCOM Burraq The Burraq ( ur, ) is an unmanned combat aerial vehicle (UCAV) jointly developed and built by the National Engineering and Scientific Commission (NESCOM) and the Pakistan Air Force (PAF). Development Since 2004, the United States (US) has be ...
is thought to be mostly influenced by CH-3. 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 multipurpose UAV which can also carry AR 1 laser guided rocket for attacking role. It is also widely rumoured that Myanmar Air Force operates them, and some images have been found. Specification: *Payload (kg): 180 maximum *Endurance (h): 6 with maximum payload *Ceiling (Km): 4 *Max Range (km): 960


CH-4

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 Pelvic fins or ventral fins are paired fins located on the ventral surface of fish. The paired pelvic fins are homologous to the hindlimbs of tetrapods. Structure and function Structure In actinopterygians, the pelvic fin consists of two ...
below the
V-tail The V-tail or ''Vee-tail'' (sometimes called a butterfly tail or Rudlicki's V-tailGudmundsson S. (2013). "General Aviation Aircraft Design: Applied Methods and Procedures" (Reprint). Butterworth-Heinemann. p. 489. , 9780123973290) of an aircraft ...
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 (~16,400 feet), therefore the aircraft can stay outside of effective range of most anti-aircraft guns. It also allows 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 Myanmar, Pakistan, Egypt, Saudi Arabia, Algeria and Iraq.
Myanmar Myanmar, ; UK pronunciations: US pronunciations incl. . Note: Wikipedia's IPA conventions require indicating /r/ even in British English although only some British English speakers pronounce r at the end of syllables. As John Wells explai ...
is also producing CH-4 UAV under license with the transfer of technology. Iraq has received an unknown number of CH-4B in early 2015, spurred on battlefield reversals in
Mosul Mosul ( ar, الموصل, al-Mawṣil, ku, مووسڵ, translit=Mûsil, Turkish: ''Musul'', syr, ܡܘܨܠ, Māwṣil) is a major city in northern Iraq, serving as the capital of Nineveh Governorate. The city is considered the second larg ...
and
Ramadi Ramadi ( ar, ٱلرَّمَادِي ''Ar-Ramādī''; also formerly rendered as ''Rumadiyah'' or ''Rumadiya'') is a city in central Iraq, about west of Baghdad and west of Fallujah. It is the capital and largest city of Al Anbar Governorate w ...
to
ISIL An Islamic state is a state that has a form of government based on Islamic law (sharia). As a term, it has been used to describe various historical polities and theories of governance in the Islamic world. As a translation of the Arabic term ...
. Saqr-1 is thought to be mostly influenced by CH-4. Specification: * Length: * Wing Span: * Max Take Off Weight: * Payload: * Endurance: 40 hours * Powerplant: 1 x 1000 Hp engine * Maximum Speed: * Cruise Speed: * Communications range: > with SatCom (1,500-2,000 km for CH-4B), ~ 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), 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.


CH-5

The CH-5 is the latest UCAV of the Rainbow series, with a wingspan of 21 metres, a payload of 1,000 kg, a
maximum takeoff weight The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits. The analogous ...
of over 3 tonnes, a service ceiling of 9 km, an endurance of up to 60 hours and a range of 10,000 km. Thanks to shared data link it can cooperate with CH-3 and CH-4 drones. It conducted its maiden flight in August 2015 and its first airshow flight (in northern
Hebei province Hebei or , (; alternately Hopeh) is a northern province of China. Hebei is China's sixth most populous province, with over 75 million people. Shijiazhuang is the capital city. The province is 96% Han Chinese, 3% Manchu, 0.8% Hui, and 0 ...
) in July 2017. The drone can carry 16 missiles at a single time. There were also plans to extend its range up to 20,000 km. 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 The Honeywell TPE331 (military designation: T76) is a turboprop engine. It was originally designed in the 1950s by Garrett AiResearch, and produced since 1999 by Honeywell Aerospace. The engine's power output ranges from . Design and developm ...
turboprop A turboprop is a turbine engine that drives an aircraft propeller. A turboprop consists of an intake, reduction gearbox, compressor, combustor, turbine, and a propelling nozzle. Air enters the intake and is compressed by the compressor. ...
engine mounted on the Reaper, CH-5 is equipped with an unidentified turbo-charged piston engine, with less than half the
horsepower Horsepower (hp) is a unit of measurement of power, or the rate at which work is done, usually in reference to the output of engines or motors. There are many different standards and types of horsepower. Two common definitions used today are t ...
. This choice 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 to 60 hours compared to 14 hour of the Reaper's. A newer variant with a 300kW piston engine from Anhui Hangrui Co. will increase the service ceiling to 12 km and endurance to 120 hours. 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)


CH-6

The CH-6 is a large UAV with a
MTOW The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits. The analogous ...
of 7800 kg with two variants: a strike variant with 18-hour endurance and 450 kg payload; a reconnaissance variant with 21-hour endurance and 120 kg payload. It was in development in 2021.


CH-7

The CH-7 is a stealthy flying wing
UCAV An unmanned combat aerial vehicle (UCAV), also known as a combat drone, colloquially shortened as drone or battlefield UAV, is an unmanned aerial vehicle (UAV) that is used for intelligence, surveillance, target acquisition, and reconnaissance ...
similar to the
X-47B The Northrop Grumman X-47B is a demonstration unmanned combat aerial vehicle (UCAV) designed for aircraft carrier-based operations. Developed by the American defense technology company Northrop Grumman, the X-47 project began as part of DARPA' ...
, with a 22m wingspan and 10m length. It can fly at 920 km/h and at an altitude of 13,000m. Endurance is about 15 hours and its operational radius is 2000 kilometers. It can carry antiradiation missiles and standoff weapons. 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 is planned to make its maiden flight in 2019 and commence production in 2022.


CH-10

The CH-10 is a
tiltrotor A tiltrotor is an aircraft which generates lift and propulsion by way of one or more powered rotors (sometimes called ''proprotors'') mounted on rotating shafts or nacelles usually at the ends of a fixed wing. Almost all tiltrotors use a trans ...
UAV.


CH-91

CH-91 is a fixed-wing UAV in
twin-boom A twin-boom aircraft is characterised by two longitudinal booms (extended nacelle-like bodies). The booms may contain ancillary items such as fuel tanks and/or provide a supporting structure for other items. Typically, twin tailbooms support ...
layout with
inverted v-tail The V-tail or ''Vee-tail'' (sometimes called a butterfly tail or Rudlicki's V-tailGudmundsson S. (2013). "General Aviation Aircraft Design: Applied Methods and Procedures" (Reprint). Butterworth-Heinemann. p. 489. , 9780123973290) of an aircraft ...
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.


CH-92

CH-92 is a fixed-wing UAV in conventional layout with
V-tail The V-tail or ''Vee-tail'' (sometimes called a butterfly tail or Rudlicki's V-tailGudmundsson S. (2013). "General Aviation Aircraft Design: Applied Methods and Procedures" (Reprint). Butterworth-Heinemann. p. 489. , 9780123973290) of an aircraft ...
and tricycle landing gear. Propulsion is provided by a propeller driven by a pusher engine mounted at the
empennage The empennage ( or ), also known as the tail or tail assembly, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an arrow.Crane, Dale: ''Dictionary of Aeronautical Terms, third e ...
. CH-92 is mainly intended for reconnaissance, surveillance and attack missions.


CH-802

CH-802 is a fixed wing
micro air vehicle A micro air vehicle (MAV), or micro aerial vehicle, is a class of miniature UAVs that has a size restriction and may be autonomous. Modern craft can be as small as 5 centimeters. Development is driven by commercial, research, government, and mil ...
(MAV) in conventional layout with elevated high-
wing configuration The wing configuration of a fixed-wing aircraft (including both glider (aircraft), gliders and powered aeroplanes) is its arrangement of lifting and related surfaces. Aircraft designs are often classified by their wing configuration. For examp ...
and
V-tail The V-tail or ''Vee-tail'' (sometimes called a butterfly tail or Rudlicki's V-tailGudmundsson S. (2013). "General Aviation Aircraft Design: Applied Methods and Procedures" (Reprint). Butterworth-Heinemann. p. 489. , 9780123973290) of an aircraft ...
. 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 A tailplane, also known as a horizontal stabiliser, is a small lifting surface located on the tail (empennage) behind the main lifting surfaces of a fixed-wing aircraft as well as other non-fixed-wing aircraft such as helicopters and gyropla ...
. 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-817

VTOL micro-surveillance and attack UAV with a top speed of 64.8 km/hr and an endurance of 15 minutes.


CH-901

CH-901 is a fixed-wing UAV in conventional layout with cylindrical fuselage and high-
wing configuration The wing configuration of a fixed-wing aircraft (including both glider (aircraft), gliders and powered aeroplanes) is its arrangement of lifting and related surfaces. Aircraft designs are often classified by their wing configuration. For examp ...
. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the end of
empennage The empennage ( or ), also known as the tail or tail assembly, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an arrow.Crane, Dale: ''Dictionary of Aeronautical Terms, third e ...
. CH-901 is designed as an
UCAV An unmanned combat aerial vehicle (UCAV), also known as a combat drone, colloquially shortened as drone or battlefield UAV, is an unmanned aerial vehicle (UAV) that is used for intelligence, surveillance, target acquisition, and reconnaissance ...
.


CH-902

Fixed-wing cylindrical UAV.


Operational history


Royal Saudi Land Force

The Kingdom of Saudi Arabia have been operating CH-4, along the Wing Loong II drone in its military intervention in Yemen. On 12 July 2018, Houthi rebels shot down an armed Saudi Arabian CH-4 drone near Asir border. On 8 August 2018, Houthi rebels shot down an armed Saudi Arabian CH-4B drone near Tuwal border crossing. On 23 December 2018, Houthi rebels shot down a Saudi Arabian CH-4 drone. in Saada province, northern Yemen and displayed the wreckage of the drone. On 11 April 2019, a Saudi Arabian CH-4 drone is lost over Yemen, according to Houthi media the Saudi drone was shot down by friendly fire. On 7 January 2020, Houthi rebels shot down an armed Saudi Arabian a CH-4B drone over Jawf province. 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. On 12 February 2021, Houthis intercepted a Saudi Arabian CASC Rainbow CH-4 drone in Meghdal, Marib Governorate, displaying footage of the shot down. On 23 March 2021, a Houthi spokesman said that Houthi forces shot down a US MQ-9 Reaper drone operating in Marib, however a day later the Houthis published footage of the shootdown depicting a drone resembling a CH-4 drone. On 23 May 2021, a Saudi Coalition CH-4 drone is shot down by Houthi fighters in Al-Maraziq, Al-Jawf governarate. Later Houthi media wing released a video of the shotdown of the drone. On 6 October 2021, Houthis reported the shot down of a Saudi Arabian CASC Rainbow CH-4 drone in Juba district, southern Marib province by Houthi Air Defenses, later displaying footage of the drone wreck.


United Arab Emirates Air Force

The United Arab Emirates Air Force have been operating CH-4, along the Wing Loong II drone in its military intervention in Yemen.


Comparison


Operators

; *
Algerian People's National Armed Forces french: Armée nationale populaire , image = ANP.png , alt = , caption = People's National Army emblem , image2 = , alt2 = , caption2 = , motto = ...
: CH-3 and CH-4 ; *
Ethiopian National Defense Force The Ethiopian National Defense Force (ENDF) ( am, የኢፌዲሪ መከላከያ ሠራዊት, Ye’īfēdērī mekelakeya šerawīt, lit=FDRE Defense Force) is the military force of Ethiopia. Civilian control of the military is carried out t ...
: CH-4 ; *
Indonesian Armed Forces , founded = as the ('People's Security Forces') , current_form = , disbanded = , branches = , headquarters = Cilangkap, Jakarta , website = , commander-in-chief = Joko Widodo , ...
: six CH-4Bs ; *
Iraqi Armed Forces The Iraqi Armed Forces ( ar, القوات المسلحة العراقية romanized: ''Al-Quwwat Al-Musallahah Al-Iraqiyyah'') ( Kurdish: هێزە چەکدارەکانی عێراق) are the military forces of the Republic of Iraq. They consist ...
: 14 CH-4B ; *
Myanmar Air Force The Myanmar Air Force ( my, တပ်မတော် (လေ), ), known until 1989 as the Burmese Air Force, is the aerial branch of Myanmar's armed forces, the Tatmadaw. The primary mission of the Myanmar Air Force (MAF) since its inception h ...
: Acquired 12 CH-3As and some CH-4s for precision airstrike mission. Myanmar is also producing CH-4 with the transfer of technology under license. ; *
Nigerian Air Force The Nigerian Air Force (NAF) is the air branch of the Nigerian Armed Forces. It is the youngest branch of the Nigerian Armed Forces. It is one of the largest in Africa, consisting of about 15,000 personnel and aircraft including eight Chinese ...
: CH-3 ; *
Pakistan Armed Forces The Pakistan Armed Forces (; ) are the military forces of Pakistan. It is the world's sixth-largest military measured by active military personnel and consist of three formally uniformed services—the Army, Navy, and the Air Force, which are ...
: Known to use CH-3 inspired UCAVs like the
GIDS Shahpar The GIDS Shahpar is an unmanned aerial vehicle (UAV) built by Global Industrial Defence Solutions of Pakistan and used by the Pakistani military. It is currently in production following the completion of a test and qualification phase. Develop ...
since 2012. Procured 12-24 CH-4A/B
UCAV An unmanned combat aerial vehicle (UCAV), also known as a combat drone, colloquially shortened as drone or battlefield UAV, is an unmanned aerial vehicle (UAV) that is used for intelligence, surveillance, target acquisition, and reconnaissance ...
s in late January 2021. ; *
Serbian Air Force and Air Defence The Serbian Air Force and Air Defence ( sr-Cyrl, Ратно ваздухопловство и противваздухопловна одбрана Војске Србије, Ratno vazduhoplovstvo i protivvazduhoplovna odbrana Vojske Srbije, Wa ...
: 6 CH-92A ; *
Turkmen Air Force The Turkmen Air Force ( tk, Türkmen Howa Güýçleri) is the air force branch of the Armed Forces of Turkmenistan. It was formed from former Soviet Air Forces units within that region of the Turkestan Military District. The Turkmen Air Force in ...
: 3 3 CH-3 ; *
Zambian Defence Force The Zambian Defence Force is the military of Zambia. It consists of the Zambian Army, the Zambian Air Force, and the Zambia National Service. The defence forces were formed at Zambian independence on 24 October 1964, from constituent units of the ...
: CH-4 * United Arab Emirates Armed Forces: CH-4


See also


References


External links


Article detailing the CH family development
{{Chinese Military Aircraft Unmanned military aircraft of China Unmanned stealth aircraft