|
gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:aircraft
|
gptkb:Chengdu_J-20
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:climate
|
1,600 K
|
|
gptkbp:construction_cost
|
high
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
1,100 mm
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:engineType
|
2
3
WS-10A-1
WS-10A-2
WS-10A-3
|
|
gptkbp:exportedTo
|
gptkb:Bangladesh
gptkb:Egypt
gptkb:Iran
gptkb:Myanmar
gptkb:Pakistan
|
|
gptkbp:firstFlight
|
2000
|
|
gptkbp:firstRace
|
1996
|
|
gptkbp:fuel_capacity
|
high
0.85 kg/kN·h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:future_plans
|
completed in 1999
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
WS-10A Taihang
|
|
gptkbp:inspiration
|
gptkb:Russian_AL-31F
indigenous engine development
|
|
gptkbp:is_designed_to
|
gptkb:Shenyang_Liming_Aircraft_Engine_Company
|
|
gptkbp:is_used_in
|
gptkb:Chengdu_J-10
gptkb:Shenyang_J-11
gptkb:Shenyang_FC-31
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:market
|
gptkb:Chinese_military_aviation
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_feature
|
thrust vectoring
|
|
gptkbp:operational_status
|
in production
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:performance
|
superior to WS-6
|
|
gptkbp:produces
|
1980s
|
|
gptkbp:propulsion
|
8.67
13,000 lbf
|
|
gptkbp:related_engine
|
WS family
Brayton_cycle
|
|
gptkbp:replacedBy
|
WS-15 engine
|
|
gptkbp:successor
|
WS-6 engine
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:weight
|
1,500 kg
|