| Z-10 | |
| Type: | Attack helicopter |
| Manufacturer: | Changhe Aircraft Industries Corporation (CAIC) |
| Unit Cost: | US$ 17 million [1] |
| Design Group: | 602nd Aircraft Design Institute Kamov Design Bureau |
| First Flight: | 29 April 2003[2] |
| Introduction: | 2009 |
| Status: | In service[3] |
| Produced: | 2003-present |
The Changhe Z-10 (Chinese: s=直-10|p=Zhí-Shí|l=helicopter-10) is a Chinese medium-weight, twin-turboshaft attack helicopter built by the Changhe Aircraft Industries Corporation for the People's Liberation Army Ground Force. Designed by 602nd Aircraft Design Institute of Aviation Industry Corporation of China (AVIC) and Kamov Design Bureau, the aircraft is intended primarily for anti-tank warfare missions with secondary air-to-air combat capability.
The plan to develop a medium-weight helicopter program was initiated in 1994 with the attack helicopter program formally beginning in 1998. The preliminary design of the aircraft was provided by Kamov, while prototyping was conducted by the 602nd Aircraft Design Institute of Aviation Industry Corporation of China (AVIC).[4] [5] [6] [7] The Z-10 first flew on 29 April 2003[2] and entered Chinese Army Aviation service in 2009.
Nicknames of characters in the Chinese classic novel Water Margin have been used to name Z-10 and its light-weight counterpart, the Harbin Z-19 by Chinese Army Aviation Corps; Z-10 is called Fierce Thunderbolt (Pi Li Huo, 霹雳火), the nickname of Qin Ming, while Z-19 is called Black Whirlwind (Hei Xuan Feng, 黑旋风), the nickname of Li Kui.[8] [9] [10]
The People's Liberation Army Ground Force (PLAGF) established its army aviation units in January 1988. The unit used helicopters transferred from People's Liberation Army Air Force (PLAAF), including Mil Mi-4, Harbin Z-5, Mil Mi-8, and Aérospatiale Gazelle. By the mid-1980s, the Chinese decided to field dedicated attack helicopters. The brief honeymoon period between China and the West provided China opportunities to evaluate Agusta A129 Mangusta, AH-1 Cobra, and BGM-71 TOW missiles. However, the 1989 Tiananmen Square protests and massacre and the proceeding arms embargo prevented many deals from going through. Nevertheless, China successfully imported or licensed aircraft types such as Changhe Z-8, Harbin Z-9, Sikorsky S-70, Mi-17, and Aerospatiale AS332 Super Puma.[11]
There was also debate in China about whether the PLAGF or PLAAF should operate attack helicopters. Eventually, the PLAGF won and began to induct armed helicopters based on the Harbin Z-9 design. The use of the Z-9WA modification helped China realize the requirement for a dedicated attack helicopter platform.
A preprimary plan to develop an attack helicopter in China began in 1992.[12] [13] China began to develop the 6-ton class China Helicopter Medium (CHM) program in 1994, headed by the 602nd and 608th Research Institutes.[14] This program was later developed into Harbin Z-20. In 1995, China commissioned Kamov to develop a preliminary design for the 6-ton helicopter, known as Project 941 internally. Project 941 was a large departure from traditional Soviet design, focusing entirely on the Chinese requirement. The concept was then handed to China for further development, which Kamov did not participate in. Based on the concept, Chinese engineers developed prototypes and iterate designs based on the testing results. The changes include modification on the airframe shapes to optimize radar cross section (RCS), changes on the engine bay shape to accommodate domestic engines, and the engine nozzle layout.[15]
China also secured assistance from Eurocopter France for the rotor system and AgustaWestland in 1997 for the transmission system in 1998. Pratt & Whitney Canada and Hamilton Sundstrand secretly provided PT6C-67C engines and digital engine control systems to aid the programs, leading to them receiving investigations and penalties from the United States government.[6] [7] [16]
In 1998, the 602nd Research Institute proposed the Special Armed Project to develop the final design, which was designated the Z-10.[17] Initially, the Z-10 project was planned to share its propulsion system with the CHM program, however, the two programs were separated and the Z-10 was prioritized to be completed first.[8] During the development in 2000, Denel also provided technical assistance to the project in the area of flight stability.[5] After the US government cut off engine sources from Pratt & Whitney, China turned to domestic replacements with lower thrust-rating, leading to further weight-saving design changes.[6] The replacement engine was the indigenous WZ-9 turboshaft.
David Donald of Aviation International News claimed the Z-10 had a universal engine bay capable of fitting various types of engines, including Ukrainian Motor Sich TV3-117. However, Chinese sources indicated the TV3-117 is incompatible with the Z-10's engine bay due to the driveshaft shape and prototypes were fitted with either Pratt & Whitney PT6C-67C or Chinese-built Turbomeca Makila turboshaft engines, whereas the final version uses WZ-9 turboshaft engines due to its fully indigenous origin.
The Z-10 took its maiden flight on 29 April 2003.[2] The Z-10 entered PLA service in 2009[12] [13] [17] or 2010.
In March 2014, the Z-10 helicopter began deck trials with a People's Liberation Army Navy Type 072A-class landing ship. The purpose may be to qualify the helicopter on ships to provide air support for landing parties launched from the ship. Type 072A-class ships have a helipad but no hangar or support facilities for the aircraft on board. The Z-10 may also be qualified on the larger Type 071 amphibious transport dock.[18]
The Z-10 was one of the contenders to replace Pakistan's Bell AH-1F Cobra attack helicopters. In 2015, Pakistan acquired three Z-10s for trials,[19] but ultimately rejected the offer due to the inadequate WZ-9 engine. After the failed bid, Chinese engineers began to upgrade to the Z-10 platform to improve its competitiveness. A new prototype, designated Z-10ME, emerged in 2018 with a larger ammunition magazine size, new intake filtration systems, and new missile approach warning system (MAWS). In the same year, more equipment was added to the prototype, such as a more powerful WZ-9C turboshaft with power, new infrared signature-reducing engine exhaust nozzle, appliqué graphene-based armor plates, etc.
The PLAGF's domestic Z-10 fleet were upgraded to the Z-10ME standard with the engines, armor plates, and infrared suppresion nozzles. The Pakistan Army eventually purchased the Z-10ME as well.
The Z-10 features a tandem cockpit compartment at the front section. The airframe bulges below the cockpit, extending backward and merging with the stub wings and tail boom, creating a distinctive ridge dividing the top and bottom half of the blended fuselage, which are both canted inward, creating a hexagon-shaped frontal profile.[13] [20] This slim, rhombic configuration ensures structural strength, increases internal volumes for equipment, and reduces the frontal projected area and overall radar cross section (RCS).[20] [21] The radar-absorbent material is applied to the fuselage, further reducing the radar reflection and providing a certain degree of low observability.
The rotor system consists of a single semirigid five-blade main rotor at the top and a four-blade tail rotor at the aft section.[20] The airfoil of the primary 95KT rotor blade features a significant camber with swept tips, designed to reduce the blade length, vibration, and acoustic signature. The tail rotor consists of two sets of dual composite blades (four blades in total) mounted in an angled, non-orthogonal (scissor) arrangement[22] designed to reduce noise generated by the wingtip vortices. All blades are made with carbon fiber-wrapped spars with layered honeycomb composite for the skin, capable of sustaining damage against rounds.[20] The deicing device is fitted to the blades to increase flight safety in adverse weather.[20]
The fuselage is primarily made of aluminum alloy, with 30 percent of the mass being composite materials.[2] The cockpit compartment is wrapped inside carbon fibers, while the canopy is protected by bulletproof glasses of in thickness. Additional protection layers made of aluminum alloy and kevlar are applied to the bottom of the cockpit, side of the engine bays, and around the self-sealing fuel tank.[20] The honeycomb composite layer is applied to the fuselage bottom, while the pilot seats, landing gears, and fuel tank are reinforced for improved crashworthiness.[20] [21] The early model of Z-10 prioritizes protection in critical areas for weight reduction without sacrificing structural integrity, range, and payload. In later serial production, graphene armor plates are mounted on the side of the cockpit and engine housing to further improve the protection level.[20] [23]
The Z-10's engine air intake is protected by a metal mesh to prevent foreign objects from being sucked in. Newer variants can be installed with integrated inlet particle separators (IPS) for engine intake filtration, preventing harmful solid particulates such as sand and dust to damage the critical propulsion components. The Z-10's engine system is fitted with the Hover Infrared Suppression System (HIRSS), mixing in the engine exhaust with cold air to reduce the helicopter's infrared characteristic.[20] Later serial production of Z-10 modified the engine nozzle from sideway-facing to the upward-facing direction, further reducing the signature from heat radiation. The upward-facing exhaust nozzle, albeit beneficial for suppressing the infrared signature, would lead to additional drag, To resolve this, the engine on the Z-10 was upgraded to from to to make up the loss.[24]
The Z-10 prototype was powered by two Pratt & Whitney Canada PT6C-67C turboshaft engines, which is equipped with Full Authority Digital Engine Control (FADEC) system and sports a maximum continuous power of .[25] The early batches of Z-10 was powered by domestic Zhuzhou WZ-9 or WZ-9A turboshaft engine, providing of power.[20] [26] The reduced performance of WZ-9 turboshaft engines prevented Z-10 to carry its maximum payload of 16 anti-tank guided missiles.
Multiple engines were developed to upgrade the propulsion of the Z-10. China and European partners reportedly developed WZ-16.[20] WZ-9 was upgraded to WZ-9C with of maximum power. The engine was originally designed for export, but subsequently used to upgrade early Z-10s batches. The WZ-9C provides 30% more power than the original version, providing the Z-10 with enough lift for a variety of payloads.
The Z-10 emphasizes extended-range operation. The WZ-9A turboshaft engine allows the aircraft to fly at a maximum speed of and cruise speed of . The internal tank supports a range of .[20]
The Z-10 features a comprehensive self-defense suite. The YH-96 electronic warfare system includes a set of infrared missile approach warning system (MAWS),[21] radar warning receivers (RWR) and laser warning receivers (LWR), both are connected with the 6×4 countermeasure dispensers (two on each side, four in total) to release flare and chaff when incoming missiles are detected.[20] The system was upgraded on later variants with a different avionics layout, replacing previously mounted radar and electro-optical sensors with integrated countermeasure suite, indicated by several active electronically scanned array (AESA) radar panels around the fuselage and two electro-optical suites mounted on the stub wings. The radar panels are capable of passive signal detection, target searching, and active jamming, which also replace the function of missile approach warning system. The electro-optical suites include new laser,[27] infrared, ultraviolet warning receivers, and directional infrared countermeasure systems (DIRCM) to defend against infrared homing (IR) missiles.
The primary sensor suite of Z-10 is the WXG1006 electro-optical (EO) package located at the nose section. The ball-shaped package contains a forward-looking infrared sensor, a TV camera, a laser rangefinder, and a laser designator.[28] The development of the primary electro-optical fire control systems (FCS) was influenced by French and Israeli systems but with locally programmed software. The YH millimeter-wave radar was also developed for Z-10 to detect longer-range targets, and targets behind flog, smoke, and dust.[20] The mmWave radar can be installed on top of the main rotor mast.
The stepped tandem cockpit houses two pilots. The front pilot primarily controls the flight maneuver, while the back pilot handles the weapon system.[29] [30] Both pilots have identical flight instrumentation, serving as backups to each other, and both are capable of flight control and weapons operation.[21] Inside the cockpit is the digital flight instrument,[20] [21] with the fly-by-wire Hands-On Collective And Stick (HOCAS) flight control. Each pilot has two LCD multi-function displays (MFD) and multiple small displays for other information.[20] [21] [31] An additional holographic heads-up display (HUD) is provided for the front pilot.
Each pilot also wears a helmet-mounted sight (HMS), similar to the Integrated Helmet and Display Sighting System (IHADSS) on the AH-64 Apache. The helmet sight is fully integrated with FCS to control guided and unguided munitions and display onboard navigation information. The pilots can slave the sensor suite and autocannon to their helmets, controlling the sensors and autocannon direction by turning their heads.[20] For all-weather operation, the helmet visor can be attached with a binocular-like night vision goggles (NVG),[32] which was later replaced with integrated NVGs that can display night-vision image directly inside the visor.[29] [33]
Other navigation instruments of Z-10 include laser gyrocompass, radio altimeter, Doppler radar, inertial navigation, satellite navigation, and identification friend or foe (IFF) systems.[21] [34]
The Z-10 has a modular weapon system. The system uses the GJV289A standard, the Chinese equivalent of the MIL-STD-1553B databus architecture, which enables weaponry of Chinese, Soviet, and Western origin to be adopted by the Z-10. Offensive weaponry consists of machine guns, cannons, rockets, and missiles. Internal armament consists of a gun mount installed on the chin of the aircraft with 180° of horizontal traverse.[20] Two stub wings provide attachment points for external ordnance or gun pods.[21] [35] Each stub wings have two hardpoints,[21] for a total of four, and each hardpoint can carry up to 4 missiles, for a total of 16 missiles.
The autocannon on the serial production Z-10 is the PX-10A automatic chain gun,[20] [36] but the aircraft can also mount,, and autocannons,[21] with some of them marketed for export customers.
The air-to-surface missiles deployed by the Z-10 include HJ-8, HJ-9, HJ-10, AKD-9, and AKD-10 anti-tank missiles.[28] Early AKD-10 utilizes semi-active laser (SAL) guidance, while later variants reportedly incorporate millimeter wave (MMW) seekers.[28] The Z-10 can also fire BA-21 long-range anti-tank missiles with a millimeter wave/semi-active laser dual model guidance seeker.[28] The missile can be fired from Z-10 and data-linked by millimeter-wave radar mounted on friendly platforms.[37] Aside from anti-tank missiles, the Z-10 can also carry SW6 air-launched drones, CM-501GA none-line-of-sight air-to-surface missiles CM-502KG anti-tank missiles,[24] CM-501XA loitering munitions, ET60 lightweight torpedo, with the last one providing Z-10 with useful, albeit limited, naval warfare capabilities. The helicopter is compatible with GB25 and GB50 guided bombs.
The main air-to-air missile deployed by the Z-10 is the TY-90,[28] a missile specifically designed for use by helicopters in aerial combat.[20] The TY-90 is much heavier than the MANPAD missiles usually carried by helicopters, providing better lethality and range.[38]
The Z-10 can launch a great variety of unguided and guided rockets. Under the stub wings, a total of four rocket pods can be mounted on the hardpoints. Options include the 19-tube rocket pod,[39] 7-tube Fire Snake rocket pod[40] with FS70A (GR-5) guided rocket or FS70B air burst fragmentation rocket,[41] [42] or 19-tube unguided rocket pod with anti-infantry fragmentation rockets. 7-tube rocket pod is also available,[43] capable of firing the larger FS90A guided rocket or Tianjian rocket.[44] Aside from the common calibers, the helicopter can support rockets from to .
For other types of payloads, the Z-10 can carry a KG300G self-defense electronic warfare (EW) pod, providing organic survivability for frontline ELINT and ESM defense.[45] The EW pod features a stealth enclosure, and is capable of providing multi-target jamming, spectrum searching, and digital radio frequency memory (DRFM) signal processing.[46] External fuel tanks be attached to further its operational and ferry ranges.[47] The helicopter can also underslung all-terrain vehicles (ATV) for special operation insertion support. The Z-10 can underslung around 3 tonnes.
In 2011, the Z-10 can be observed operating at PLAGF bases.[48] In September 2016, the PLA announced that all of its army aviation units had been equipped with the Z-10.[49] The helicopter is stationed in frontline regions, such as the Tibet plateau,[50] and Taiwan Strait.[47]
The Z-10 was one of the contenders to replace Pakistan's Bell AH-1F Cobra attack helicopters. In 2015, Pakistan acquired three Z-10s for trials,[51] but they rejected the offer due to the inadequate WZ-9 engine. Pakistan then chose Turkey's AH-1Z; however, contracts to acquire the AH-1Z and then the TAI/AgustaWestland T129 ATAK (which uses the American LHTEC CTS800–4A engine) fell through because of worsening relations with the United States.[52] In January 2022, negotiations to acquire the Z-10ME were underway;[53] the Z-10ME had been identified as a fallback option by February 2020.[52] In June 2022, Pakistan's deal with T129 ATAK was reportedly canceled, and the Pakistan government was seeking the acquisition of Z-10ME.[54] Pakistan military reportedly received the first batch of Z-10ME in 2023.
According to Boneham of Janes Information Services, the advantages of the Z-10ME were its capabilities and affordability, when compared with similar Western platforms. The helicopter is suitable for countries without access to Western and Russian hardware.[27] Malcolm Davis of the Australian Strategic Policy Institute believed the Z-10ME offered the capability gap of operating air-launched UAVs, and potential candidates included Laos, Cambodia, Myanmar, etc. However, Davis believed the demand for advanced helicopters was quite small in these economies.[55]
In June 2012, the United States charged United Technologies and two of its subsidiaries, Pratt & Whitney Canada and Hamilton Sundstrand, of selling engine control software to China which aided in the development of the Changhe Z-10.[56] While the Chinese defense ministry denied that China bought or used the software, Pratt & Whitney Canada and Hamilton Sundstrand agreed to pay more than $75 million to the U.S. government to settle the charges.[57]
Islamic Republic of Pakistan