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Z-9 Harbin (WZ-9) Chinese Medium Multi-Role Helicopter

Z-9

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Basic Information
Name
Z-9 Harbin (WZ-9) Chinese Medium Multi-Role Helicopter
Designation
Z-9
Alternate Designation
Equipment Type
Manufacturer
Harbin
Date of Introduction
1981
Description

Despite statements from some sources, WZ-9 is too lightly protected to be an "Attack helicopter". The Z-9 was designed to be adaptable for a variety of roles, including transport, direct air support, escort, security, reconnaissance, ambulance, anti-submarine warfare, IW, airborne C2, search and rescue, antiship, and anti-submarine warfare. Each fuselage side has one pylon allowing for a single pod or missile rack. An expected upgrade for WZ-9/Z-9g is the red arrow 9 laser-beam rider/MMW guided ATGM, with 1,200 mm penetration and a 5 km range. The first Z-9 flew in 1981 and was built in China from components supplied by Aérospatiale as part of a production patent bought on 15 October 1980. On 16 January 1992, the indigenous variant Z-9B, constructed with 70% Chinese-made parts, flew successfully. The flight test was completed in November 1992 and the design was finalized a month later. Z-9B production began in 1993 and entered PLA service in 1994. The Z-9B features an 11-blade Fenestron faired-in tail rotor with wider-chord, all-composite blades replacing the 13-blade used in the original AS365N. As a light tactical troop transport, the Z-9 has the capacity to transport 10 fully armed soldiers. Generally, the Z-9 is identical to the AS365N Dauphin, though later variants of the Z-9 incorporate more composite materials to increase structural strength and lower radar signature. The helicopter has a four-blade main rotor, with two turboshaft engines mounted side by side on top of the cabin with an engine layout identical to the AS365N. The Z-9 teardrop-shaped body features a tapered boom to the tail fin, with a rounded nose and stepped-up cockpit, retractable gear, and all flat bottom. In 2002, Harbin obtained Chinese certification for the new H410A variant of the Z-9, which features more powerful Turbomeca Arriel 2C turboshaft engines; Eurocopter issued official objections to Harbin's decision to continue production in spite of the license-production agreement having expired, leading to a period of highly sensitive international negotiations to resolve the dispute.

Air & Air Defense Specifications
Crew 1
Engine 2 x Zhuzhou Aeroengine Factory WZ-8A Turbo shaft Engines (650 hp)
Max Speed 305.0 km/h
Range 1000.0 km
Endurance 5.00 hrs
Service Ceiling 4500 m
Variants
Z-9A Military production version with some upgrades, such as Arriel 1C2 engine, upgrade instrument panel, and 150-kg payload increase.
Z-9A 100 Prototypes for domestic market versions with WZ8A engines. First flight 16 January 1992, approved 30 December 1992.
Z-9B Current production version for multi-role use, based on Dauphin 2 designs. Changes include 11-blade tail rotor.
Z-9C Naval version for ASW and SSM, with Sinatra HS-12 dipping sonar and torpedo. It has a datalink to support targeting for YJ-82 SSM. An expected near-term upgrade is the C-701 TV guided air-to-surface missile.
WZ-9 Light attack version of Z-9B (see ARMAMENT, left). Poss aka Z-9W. Export version is Z-9G.
Z-9Z Reconnaissance prototype.
Z-9EC ASW variant produced for the Pakistan Naval Air Arm. Configured with pulse-compression radar, low-frequency dipping sonar, radar warning receiver, and doppler navigation system, it is also armed with torpedoes for use aboard Pakistan Navy's Zulfiquar-class frigates.
Z-9EH Transport, emergency and/or passenger variant.
Z-9W (WZ-9) Armed version with optional pylon-mounted armament, gyro stabilization, and roof-mounted optical sight. Export designation Z-9G, roof-mounted sight optional. First flown in 1987, with the first weapons tests in 1989.
Z-9WA A newer night-capable version has been built with nose-mounted FLIR. In July 2011, Xinhua News Agency released a photo of Z-9WA firing ADK10 air-to-ground missile. Incorporates a domestic Chinese helmet-mounted sight that is compatible with anti-tank missiles such as HJ-8/9/10, as well as light anti-ship missiles such as C-701/703 and TL-1/10 when they are used as air-to-surface missiles, air-to-air missiles such as TY-90, and other MANPAD missiles for self-defense.
H410A Version with 635 kW WZ8C turbo-shaft engines. First flight September 2001, CAAC certification 10 July 2002. One is currently being fitted with a new Mast-Mounted Sighting (MMS) system.
H425 Newest VIP version of the H410A, that has upgraded 635 kW WZ8C turbo-shaft engines and a new Mast-Mounted Sighting (MMS) system.
H450 Projected development.
WZ-19 Attack helicopter development with tandem seats. The WZ-19 shares the same power plant as the WZ-9WA.
System
Alternative Designations Z-9 Harbin; WZ-9
Crew 1 for Z-9, 2 for WZ-9. Transports 9-12 troops, 4-8 litters or cargo.
Passengers 10 (4,189 lb)
Primary Function Medium Multi-role Helicopter
Blades – Main Rotor 4 ea
Blades Tail Rotor 11 ea
Tail rotor 13 Z-9A, 11 Z-9B/WZ-9
All Weather Capable Yes
Day/Night Capable Yes
Vertical Clime Rate 246 m/s
Cruise 260 kkm/h
Hover (out of ground effect) 1,020 m Z-9A 1,600 m Z-9B
Hover (in ground effect) 1,950 m Z-9A 2,600 m Z-9B
Speed: Max 305 km/h
Ferry Range 1,000 km
Under-Nose Low-Light TV Yes
Infrared Observing and Tracking Yes
Roof Mounted Optical Sight Yes
Number of Hard Points 2 ea
Dimensions
Length (fuselage) 12.11 m
Main Rotor Diameter 13.7 m
Main Rotor Area 11.98 m2
Height 4.01 m
Weight, Combat 4,100 kg
Weight, Empty 2,050 kg
External Fuel Tank 180 kg
Normal Fuel Load 860 kg
With Auz Fuel 1,000 kg
Automotive
Engine Type 2 x Zhuzhou Aeroengine Factory WZ-8A Turbo shaft Engines
Engine Type Turbo shaft Engines
Engine Power 650 hp each
Cruising Range 1,000 km
Speed, Maximum 305 km/hh
Speed, Average Cross 260 km/h
Climb Rate 549 mps
Ceiling 4,500 m
Ferry Range 1,000 km
Endurance 5 hours
Service Ceiling 4,500 m
Hovering Ceiling in Ground Effect 2,600 m
Hovering Ceiling out of Ground Effect 1,600 m
Communications
BG-06 Radio Altimeter Yes
Type 150 Single-Sideband Radio Yes
INS/GPS Transponder Yes
KTR-908 VHF Command Radio Set Available
TB-31 Intercom System Available
Armament
Description 2 x fixed 23-mm guns or 12.7-mm MGs. Two pylons permit mounting up to 8 ATGMs, or 4 plus 2 rocket pods.
Most Probable Armament Combat versions (WZ-9 and Z-9G) have Twin 23-mm gun, four Red Arrow-8F ATGMs, 2x 7-round 90-mm rocket pods, and 2 TY 90 IR-homing AAMs.
HJ-8 or HJ-8E ATMs
Location Wing Mounted
Function Wire-Guided Anti-Tank Missile System
Caliber/Length 1,566 mm
Diameter 120 mm
Muzzle Velocity 200 m/s
Operational Range 3,000-4,000 m
Guidance System SACLOS Wire Guidance
Armor Penetration Yes
Number of Rounds 8 ea
Single Twin Barrel GSh-23L Autocannon
Location Chin
Caliber/Length 23 x 115 mm
Maximum Effective Range 2 km
Cyclic Rate of Fire 3,000 rpm
Muzzle Velocity 690 m/s
Armor Penetration Yes
Number of Rounds 1,000 ea
Fire Control
Fire Control System Type INA
Fire Control Radar Yes
Digital Cockpit Yes
Direct Fire Control Yes
Laser Designator Yes
Automated Helmet Yes
Sensor Suite(s) Available INA
Position Location System Yes
X-Band KLC-1 Search Radar Available
Protection
Fuselage INA
Anti-Armor Yes
Cockpit Glass Yes
Stealth Properties No
Heat Signature Reduction Yes
Add on Armor INA
NBC Protection Yes
EW Yes
Chaff Flare Dispensers Yes
EW Counter Measures/CCM Yes
Details
Country of Origin China
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
Z
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
12.11 m
Width
Height
4.01 m
Weight
4100 kg
Operators (12)
China
Pakistan
Bolivia
Cambodia
Cameroon
Ghana
Kenya
Laos
Mali
Mauritania
Namibia
Zambia
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