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Y-9 transport aircraft???

houshanghai

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The first Y-9 prototype (#941) is shown here parked at CFTE airfield. The design was first unveiled at the 11th Beijing Airshow in September 2005. Y-9 is the next generation medium-size and medium-range transport aircraft to replace the obsolete Y-8 series transport aircraft. It appears to have superceded the earlier Y-8-X project (initially dubbed Y-8U?). The aircraft features a spacious cargo cabin which can quickly load/unload maximum 20t containerized cargo, or airdrop 13.2t equipment or 98 paratroopers. It also has a 4-crew cockpit featuring 6 color MFDs and EFIS. The aircraft is equipped with advanced communication, navigation, radar, EGWPS, collision avoidance systems to ensure safe flight under all weather conditions. The aircraft will be powered by 4 WJ-6C turboprops (rated @ 5,100ehp each) with JL-4 6-blade propellers made of composite materials, which improve its high temperature and high altitude performance. Some specifications: max TO weight 65t, max payload 20t or 106 paratroopers, 15t payload range 2,200km, max range 5,000km, max level speed 650km/h, cruise speed 550km/h, service ceiling 10,100m, cruise altitude 8,000m. The development of Y-9 started officially in October 2005 and the construction of the first prototype (tail and head sections) started in 2006. However the project appeared to have been halted in 2007 due to shifting the production to the high priority High New series as well as Y-8C transport aircraft. The developement of Y-9 resumed in late 2008 after the two year delay and the first prototype was rumored to have made its maiden flight on November 5, 2010.


Chinese Military Aviation | China Air Force
 
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Yun-9 Multipurpose Transport Aircraft


At the September 2005 International Aviation Expo held in Beijing, Shaanxi Aircraft Industry (Group) Co. Ltd unveiled its Y-9 multi-purpose transport aircraft design. A substantial redesign of the Shaanxi Y-8 (Chinese copy of the An-12 Cub), the aircraft was initially revealed to the public at the 2002 Zhuhai Air Show under the name of Y-8X concept transport. It is said to be comparable to the U.S. Lockheed Martin C-130J transport in general performance.

The development of the Y-8X began in 2001 to meet the requirements of the PLA Air Force for a capable and advanced medium-size tactical transport aircraft to replace the ageing Y-8. The project aims to develop a multi-purpose turboprop transport aircraft that approaches or in some aspects exceeds the performance of the U.S. C-130J. The development is believed to have been assisted by The Ukraine-based Antonov Aeronautical Scientific-technical Complex (ASTC) aircraft company.

During the 2005 Beijing International Aviation Expo, Shaanxi revealed more details about the Y-8X, now re-designated Y-9. Compared to the Y-8, the new aircraft features a more spacious cargo cabin, fast loading/uploading system, improved WJ-6C turboprop engines, six-blade propellers, and a “glass cockpit”. The aircraft can be used for both military and civil flights.

The Y-9 ’s wings are high-mounted with four turboprop engines mounted under the wings’ leading edges. The aircraft utilises six-blade JL-4 propellers made of composite materials. The rear cargo door, which also serves as a ramp, allows cargo to be quickly loaded/unloaded. The tail flats and fin are mounted high. The aircraft has a two-wheel nose landing gear and two four-wheel main landing gears.

The payload requirement of the Y-9 includes a range of military vehicles, helicopters, cargo containers, pallets, and paratroopers. The Y-9 can air-drop paratroops and equipment either by parachute or gravity extraction. It can perform wither single or multiple airdrops of paratroopers and cargo. The aircraft can carry nine international standard pallets of 108'' X 88'' or eight 125'' X 96'', or 132 armed paratroopers.

Specifications

Flight crew: 4
Cargo cabin size: (length/width/height) 16.2m/3.2m/2.35m
Empty weight: 39,000kg
Maximum take-off weight: 77,000kg
Overloading take-off weight: 81,000kg
Payload: Normal 25,000kg; Maximum 30,000kg; or 132 armed paratroopers; or vehicles and weapons
Cruising speed: 600~650km/h
Cruising altitude: 9,000m
Range: Ferry range with max payload 7,800km
Flight endurance: 12 hours

Last update: 25 April 2007


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Yun-9 (Y-9) Multipurpose Transport Aircraft - SinoDefence.com
 
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Y-8F600

The Y-8F600 is the latest development variant of the Y-8. The aircraft was developed under the assistance of Ukraine-based Antonov Aeronautical Scientific-Technical Complex (ASTC) and Pratt and Whitney Canada. The Y-8F600 configured to provide an aerial platform for airborne early warning aircraft and other special purposes is referred to as “Category-III Platform”. The aircraft made its first flight on 14 January 2005.



KJ-200 AEW&C aircraft based on the Y-8F600 airframe (Chinese Internet)

Based on the successful Shaanxi Y-8 series transport aircraft, the Y-8F600 has been extensively modified and upgraded with Western technologies including turboprop engine and avionics. The development programme began in 1999, with two foreign partners Ukraine-based Antonov Aeronautical Scientific-Technical Complex (ASTC) and Pratt and Whitney Canada joining the programme in 2000~2002. Under the contract signed in 2002, Shaanxi and Antonov shall jointly design, assemble prototypes, certify and put into series the new Y-8F600 transport, while P&W was responsible for providing its PW150B engine to power the aircraft.

A risks-sharing partner under the programme, Antonov provided Shaanxi with the results of rigidity and aerodynamic research, as well as documents on aircraft maintainability and service life. It also designed the new wing with fuel tanks and developed technology to build it. Antonov would also share its technical data and experience with Shaanxi, and was involved in the test of the aircraft. The first flight of the Y-8F600 was made successfully on 14 January 2005.

The Y-8F600 is also referred to by Shaanxi and the PLA as “Category-III Platform”, which would provide an advanced aerial platform for special purposes such as airborne early warning (AEW/AWACS), electronic warfare and intelligence (EW/ELINT), maritime patrol, etc. The terms of Category-I and -II platforms are used to refer to the aerial platforms developed from the Y-8 basic variant and Y-8C fully-pressurised variant respectively. The successful development of the Y-8F600 was seen as a significant achievement for Shaanxi.

The Y-8F600 features an advanced two-man ‘glass’ cockpit. As well as basic flight avionics, the aircraft is equipped with datalink, flight management and control, and near ground warning system.

The Y-8F600 is powered by four P&W PB150B turboprop engines. The all-composite six-blade R-408 propeller system was developed by British Dodi company. This arrangement offers improved take-off performance at "hot and high" airports and high altitude cruise performance, extended engine service lives, and lower engine operating and maintenance costs. In addition, noise levels will be reduced and meet stringent airport noise restrictions. The aircraft maximum take-off weight is increased to 65t


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KJ-200 AEW&C aircraft based on the Y-8F600 airframe (Chinese Internet)


Yun-8 (Y-8 Cub) Turboprop Transport Aircraft - SinoDefence.com
 
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This is going to be the poor man's C-130 :lol:

Really look forward to this baby and the Y-20.
 
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