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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:check_in_time
|
optional
|
|
gptkbp:compression_ratio
|
6:1
|
|
gptkbp:control_system
|
automatic
digital
fly-by-wire
|
|
gptkbp:cooling_system
|
air
air-cooled
|
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gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:development
|
1945-1949
|
|
gptkbp:diameter
|
2.5 ft
|
|
gptkbp:elevation
|
up to 40,000 ft
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
Brayton cycle
air-start
|
|
gptkbp:engine_configuration
|
twin-engine
axial-flow
pylon-mounted
|
|
gptkbp:engine_power
|
1500 hours
1780 k W
|
|
gptkbp:engine_type
|
single-spool
|
|
gptkbp:exhaust_nozzle
|
convergent-divergent
|
|
gptkbp:exhaust_system
|
subsonic
|
|
gptkbp:first_flight
|
gptkb:1949
|
|
gptkbp:fuel_capacity
|
0.76 m
1.07 m
272 kg
|
|
gptkbp:fuel_economy
|
moderate
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
kerosene
hydromechanical
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-21 engine
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
gptkb:electronic
|
|
gptkbp:length
|
3.5 ft
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
low
85 d B
|
|
gptkbp:number_of_rooms
|
annular
|
|
gptkbp:operational_history
|
used in Korean War
|
|
gptkbp:propulsion
|
no
4.0
2400 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
45,000 ft
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:weight
|
600 lb
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|