|
gptkbp:instanceOf
|
aircraft engine
|
|
gptkbp:aircraft
|
gptkb:Shenyang_J-8
300 kg/m²
|
|
gptkbp:application
|
military aviation
|
|
gptkbp:built
|
over 1000
|
|
gptkbp:climate
|
900 °C
|
|
gptkbp:compressionRatio
|
8:1
|
|
gptkbp:controls
|
mechanical control
|
|
gptkbp:coolingSystem
|
15°
air cooling
|
|
gptkbp:design
|
gptkb:Shenyang_Aircraft_Corporation
2000 hours
|
|
gptkbp:developer
|
Sino-Soviet_collaboration
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
CAA
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
axial turbine
|
|
gptkbp:exhaustSystem
|
straight exhaust
subsonic intake
|
|
gptkbp:fanBase
|
centrifugal fan
|
|
gptkbp:firstFlight
|
1956
|
|
gptkbp:frequency
|
20°/s
|
|
gptkbp:fuel_capacity
|
0.8 kg/kN/h
|
|
gptkbp:fuelType
|
direct fuel injection
annular combustor
aviation kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shenyang WP-6A
|
|
gptkbp:inspiration
|
Soviet_designs
|
|
gptkbp:is_used_in
|
gptkb:Shenyang_J-6
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Shenyang_Aircraft_Corporation
|
|
gptkbp:maximum_speed
|
gptkb:Mach_1.1
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notableUsers
|
gptkb:China
|
|
gptkbp:operationalHistory
|
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:operationalRange
|
2000 km
|
|
gptkbp:productionYears
|
1950s to 1960s
|
|
gptkbp:proportions
|
6:1
|
|
gptkbp:propulsion
|
50 kN
125 kN/kg
|
|
gptkbp:rateOfFire
|
15°/s
|
|
gptkbp:related_engine
|
gptkb:Tumansky_R-11
Brayton_cycle
|
|
gptkbp:retirementYear
|
1990s
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:serviceType
|
1958
|
|
gptkbp:speed
|
120 km/h
|
|
gptkbp:succeededBy
|
30°/s
|
|
gptkbp:successor
|
WP-7
|
|
gptkbp:technology
|
jet propulsion
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:weight
|
400 kg
|