|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:9
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country
|
gptkb:China
|
|
gptkbp:design_features
|
advanced aerodynamics
|
|
gptkbp:development
|
1990s
|
|
gptkbp:development_cost
|
high
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
air start
WS-15 engine
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
|
|
gptkbp:engine_power
|
4,000 hours
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:exported_to
|
gptkb:none
|
|
gptkbp:first_flight
|
gptkb:2000
|
|
gptkbp:fuel_economy
|
0.85 kg/k N/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
WS-10 engine
|
|
gptkbp:integration
|
easy with airframes
|
|
gptkbp:is_tested_for
|
extensive
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Shenyang_Aircraft_Corporation
|
|
gptkbp:max_speed
|
Mach 2.0
|
|
gptkbp:military_technology
|
gptkb:none
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:performance
|
superior
|
|
gptkbp:project
|
planned improvements
|
|
gptkbp:propulsion
|
no
8.67
130 k N
|
|
gptkbp:related_aircraft
|
gptkb:Sukhoi_Su-27_family
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:2005
|
|
gptkbp:successor
|
WS-15 engine
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:upgrades
|
ongoing
|
|
gptkbp:used_in
|
gptkb:Chengdu_J-10
gptkb:Shenyang_J-11
|
|
gptkbp:weight
|
about 1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:WS-20_turbofan_engine
|
|
gptkbp:bfsLayer
|
7
|