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gptkbp:instance_of
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gptkb:helicopter
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:climb_rate
|
8 m/s
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:communication_system
|
secure communication system
|
|
gptkbp:countermeasures
|
infrared countermeasures
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
twin-engine design
|
|
gptkbp:diameter
|
fenestron tail rotor
five-blade main rotor
|
|
gptkbp:engine
|
WZ-8 A
|
|
gptkbp:exported_to
|
gptkb:Bangladesh
gptkb:Angola
gptkb:Nigeria
gptkb:Pakistan
gptkb:Thailand
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:fuel_capacity
|
1,200 L
|
|
gptkbp:height
|
3.6 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Z-9 helicopter
|
|
gptkbp:is_monitored_by
|
electro-optical system
|
|
gptkbp:length
|
13.8 m
|
|
gptkbp:manufacturer
|
gptkb:Harbin_Aircraft_Manufacturing_Corporation
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
4,200 kg
|
|
gptkbp:members
|
10°/s
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:operational_range
|
500 km
|
|
gptkbp:passenger_capacity
|
gptkb:6
|
|
gptkbp:production_location
|
gptkb:China
|
|
gptkbp:production_years
|
gptkb:1986
present
|
|
gptkbp:range
|
700 km
|
|
gptkbp:related_to
|
gptkb:Z-10_helicopter
gptkb:Z-11_helicopter
gptkb:Z-15_helicopter
gptkb:Z-19_helicopter
gptkb:Eurocopter_AS365_Dauphin
|
|
gptkbp:role
|
gptkb:transportation
gptkb:search_and_rescue
gptkb:helicopter
reconnaissance
anti-submarine warfare
medical evacuation
|
|
gptkbp:roll_rate
|
30°/s
|
|
gptkbp:service_ceiling
|
5,000 m
|
|
gptkbp:strikeouts
|
20°/s
|
|
gptkbp:successor
|
gptkb:Z-20_helicopter
|
|
gptkbp:used_by
|
gptkb:People's_Liberation_Army
|
|
gptkbp:variant
|
Z-9 A
Z-9 EC
Z-9 P
Z-9 W
|
|
gptkbp:weight
|
2,800 kg
|
|
gptkbp:wingspan
|
11.0 m
|
|
gptkbp:bfsParent
|
gptkb:AVIC_Harbin_Aircraft_Industry_Group
gptkb:Harbin_Aircraft_Manufacturing_Corporation
|
|
gptkbp:bfsLayer
|
7
|