The Shaanxi Y-9 (Chinese: 运-9; pinyin: Yùn-9) is a medium military transport aircraft produced by Shaanxi Aircraft Company in China.[1][2] It is a stretched and upgraded development of the Shaanxi Y-8F.[3]

Quick Facts Y-9, Role ...
Y-9
Thumb
Shaanxi Y-9 landing
Role Transport aircraft
National origin China
Manufacturer Shaanxi Aircraft Company
First flight November 2010
Introduction 2012
Status In service
Primary users People's Liberation Army Air Force
Myanmar Air Force
Namibian Air Force
Produced 2010–present
Developed from Shaanxi Y-8
Variants Shaanxi KJ-500
Shaanxi Y-9JZ
Shaanxi KQ-200
Close

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, and closely resemble the Dowty R406. 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 Y-9 is designed for 25 tons of cargo but can carry up to 30 tons in overload configuration. The cargo area has a length of 16.2 m (53 ft), a width of 3.2 m (10 ft), and a height of 2.35 m (7.7 ft). The aircraft can fit up to 106 passengers, 132 paratroopers, or 72 stretchers. For vehicles, it can carry two para-droppable ZBD-03 airborne combat vehicles as well as various other military equipment such as light trucks, cargo containers, or pallets.[8]

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][9]

Some special purpose variants such as the Y-9G (GX-11) have the rear ramp door removed.[10]

Variants

Thumb
Y-9Q 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[11]
Y-9JZ (GX-8)
Electronic intelligence variant[12][13][1]
Y-9XZ (GX-9)
Psychological warfare aircraft[14]
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.[15]
Thumb
Y-9W (KJ-500) airborne early warning aircraft
Y-9G (GX-11)
Electronic warfare (ECM) variant[7]
Y-9X (GX-12)
Electronic intelligence (ELINT) aircraft[14]
Y-9LG (GX-13)
New ECM variant[16]
Y-9T (GX-14)
Communications relay variant[citation needed]
Y-9Q (GX-15)
New anti-submarine variant[citation needed]
KJ-700 (GX-16)
Aerial early warning variant[17]
Y-9DZ (GX-17)
Speculated to be a new EW variant[citation needed]

Operators

Thumb
Y-9JB electronic intelligence aircraft
 People's Republic of China
 Myanmar
 Namibia

Specifications (Y-9)

Data from Jane's All the World's Aircraft 2010-11 [22]

General characteristics

  • Crew: 4
  • Capacity: 25,000 kg (55,116 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[23]
  • 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 [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

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Wikiwand in your browser!

Seamless Wikipedia browsing. On steroids.

Every time you click a link to Wikipedia, Wiktionary or Wikiquote in your browser's search results, it will show the modern Wikiwand interface.

Wikiwand extension is a five stars, simple, with minimum permission required to keep your browsing private, safe and transparent.