Shaanxi Y-9

Chinese medium military transport aircraft From Wikipedia, the free encyclopedia

The Shaanxi Y-9 (Chinese: 运-9; pinyin: Yùn-9) is a Chinese medium utility/military transport aircraft produced by Shaanxi Aircraft Company for the People's Liberation Army.[1][2] It is a lengthened and upgraded development of the Shaanxi Y-8F.[3]

National originChina
StatusIn service
Quick facts Y-9, General information ...
Y-9
Shaanxi Y-9 landing
General information
TypeTransport aircraft
National originChina
ManufacturerShaanxi Aircraft Company
StatusIn service
Primary usersPeople's Liberation Army Air Force
History
Manufactured2010–present
Introduction date2012
First flightNovember 2010
Developed fromShaanxi Y-8
VariantsShaanxi KJ-500
Shaanxi Y-9JZ
Shaanxi KQ-200
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Development

Development of the Y-9 may have begun as early as 2002 as the Y-8X program. The program was a collaborative effort with Antonov – the designers of the An-12 that it was ultimately derived from – and was aimed at competing with the Lockheed Martin C-130J Super Hercules. By September 2005, the Y-9 designation was being used.[4] The Y-9 received design features originally intended for the Y-8F600,[4] which was cancelled in 2008.[5]

Shaanxi had hoped to conduct the first flight as early as 2006, but it was delayed. Design changes were made in 2006,[3] with the design being frozen by January 2010. After the design freeze, it was suggested that the first flight would depend on securing a launch customer; construction had also not yet commenced.[5] The aircraft finally flew in November 2010.[6]

The Y-9 entered People's Liberation Army Air Force (PLAAF) service in 2012,[1] with full operating capability being announced in December 2017.[2]

Design

The Y-9 is powered by four WoJiang WJ-6C turboprop engines. The propellers are six-bladed and made with Chinese JL-4 composites. The WJ-6C is replaced by the Pratt & Whitney Canada PW150B in the Y-9E export variant.[4]

The cruise speed is 300 knots (560 km/h; 350 mph) with an endurance of around 10.5 hours.[7]

Cargo capacity

The cargo bay has an internal volume of 155 m3 and is fitted with cargo handling rollers and tie-down rings. The rear entrance to the cargo bay also functions as a ramp.[1][8]

Variants

KQ-200 anti-submarine warfare aircraft
Y-9
Base variant
Y-9E
Export designation of Y-9[6]
Y-8Q / KQ-200 (GX-6)
Anti-submarine aircraft[9]
Y-9JZ (GX-8)
Electronic intelligence variant[10][11][1]
Y-9XZ (GX-9)
Psychological warfare aircraft[12]
Y-9W / KJ-500 (GX-10)
Airborne early warning and control variant. Five hour endurance, and fitted with lighter version of KJ-2000 AESA radar.[13]
Y-9W (KJ-500) airborne early warning aircraft
Y-9G (GX-11)
Electronic warfare (ECM) variant[7]
Y-9G Electronic warfare aircraft
Y-9X (GX-12)
Electronic intelligence (ELINT) aircraft[12]
Y-9LG (GX-13)
New ECM variant[14]
Y-9Q anti-submarine warfare aircraft
Y-9Q / Y-9FQ (GX-15)
Anti-submarine aircraft
KJ-700 (GX-16)
Aerial early warning variant[15]
Y-9DZ (GX-17)
Speculated to be a new EW variant[citation needed]

Operators

Y-9JB electronic intelligence aircraft
 China
Myanmar
Namibia

Specifications (Y-9)

Data from Jane's All the World's Aircraft 2010-11 [20]

General characteristics

  • Crew: 4
  • Capacity: 20,000 kg (44,092 lb) cargo / 106 paratroopers / 72 medevac +3 attendants
  • Length: 36.065 m (118 ft 4 in)
  • Wingspan: 38 m (124 ft 8 in)
  • Height: 11.3 m (37 ft 1 in)
  • Wing area: 121.9 m2 (1,312 sq ft)
  • Airfoil: root: C-5-18; tip: C-3-14[21]
  • Max takeoff weight: 65,000 kg (143,300 lb) (and MLW)
  • Fuel capacity: 23,000 kg (50,706 lb)
  • Powerplant: 4 × WoJiang WJ-6C turboprop engines, 3,800 kW (5,100 shp) each [4]
  • Propellers: 6-bladed JL-4 composite constant-speed fully-feathering reversible propellers

Performance

  • Maximum speed: 660 km/h (410 mph, 360 kn)
  • Cruise speed: 560 km/h (350 mph, 300 kn)
  • Range: 2,200 km (1,400 mi, 1,200 nmi) with 15,000 kg (33,069 lb) payload
  • Ferry range: 5,700 km (3,500 mi, 3,100 nmi) with maximum fuel
  • Service ceiling: 10,400 m (34,100 ft)
  • Maximum operating altitude: 8,000 m (26,000 ft)
  • Power/mass: 0.234 kW/kg (0.142 hp/lb)

See also

References

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