|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:air_support
|
40 kg/s
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
1,000 ° C
|
|
gptkbp:check_in_time
|
no
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
6:1
|
|
gptkbp:compressor_type
|
multi-stage
|
|
gptkbp:control_system
|
gptkb:manual
hydraulic
|
|
gptkbp:cooling_system
|
air-cooled
air cooling
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
Brayton cycle
air-start
|
|
gptkbp:engine_configuration
|
gptkb:turbofan_engine
single-spool
pylon-mounted
|
|
gptkbp:engine_lubrication_system
|
wet sump
|
|
gptkbp:engine_max_altitude
|
12,000 m
|
|
gptkbp:engine_max_range
|
1,500 km
|
|
gptkbp:engine_max_service_ceiling
|
12,000 m
|
|
gptkbp:engine_max_thrust
|
23 k N
|
|
gptkbp:engine_max_thrust_to_weight_ratio
|
0.077
|
|
gptkbp:engine_production_year
|
1948
|
|
gptkbp:engine_type
|
axial-flow
|
|
gptkbp:exhaust_system
|
gptkb:straight
|
|
gptkbp:first_flight
|
gptkb:1949
|
|
gptkbp:fuel_capacity
|
0.9 m
3.2 m
300 kg
|
|
gptkbp:fuel_economy
|
0.5 kg/s
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
gptkb:gasoline
kerosene
gravity feed
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-23 engine
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:is_tested_for
|
gptkb:Klimov_Design_Bureau
|
|
gptkbp:length
|
3.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:predecessor
|
gptkb:Klimov_VK-1_F
|
|
gptkbp:propulsion
|
no
0.077
23 k N
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1
|
|
gptkbp:turbine_type
|
single-stage
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:weight
|
300 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|