gptkbp:instance_of
|
gptkb:jet_engine
|
gptkbp:application
|
gptkb:military_aircraft
|
gptkbp:combustion_chamber_type
|
annular
|
gptkbp:compressor_type
|
axial
|
gptkbp:control_system
|
manual control
|
gptkbp:cooling_system
|
air-cooled
air cooling
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
gptkbp:diameter
|
2.5 ft
|
gptkbp:engine
|
gptkb:military_aircraft
Brayton cycle
simple design
mass-produced
1949-1955
air start
influenced future designs
pioneered jet technology
developed in late 1940s
improved thrust versions
|
gptkbp:engine_configuration
|
gptkb:turbofan_engine
inline
detailed in technical manuals
mounted in fuselage
|
gptkbp:engine_power
|
high thrust-to-weight ratio
moderate efficiency
proven in service
|
gptkbp:engine_type
|
gptkb:VK-15_A
|
gptkbp:first_flight
|
gptkb:1949
|
gptkbp:fuel_capacity
|
compact design
|
gptkbp:fuel_economy
|
0.8 lb/lbf/hr
|
gptkbp:fuel_type
|
kerosene
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-15 engine
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
gptkbp:is_tested_for
|
gptkb:Moscow
ground testing conducted
|
gptkbp:length
|
3.5 ft
|
gptkbp:maintenance
|
periodic inspections
|
gptkbp:manufacturer
|
Klimov
|
gptkbp:max_speed
|
Mach 0.9
|
gptkbp:noise_level
|
moderate
|
gptkbp:notable_users
|
gptkb:Soviet_Air_Force
|
gptkbp:operational_history
|
used in Korean War
|
gptkbp:propulsion
|
not equipped
1,500 lbf
|
gptkbp:related_aircraft
|
gptkb:Mikoyan-Gurevich_Mi_G_family
|
gptkbp:service_ceiling
|
40,000 ft
|
gptkbp:successor
|
gptkb:Klimov_VK-1
|
gptkbp:turbine_type
|
single spool
|
gptkbp:type
|
turbojet
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-15
|
gptkbp:weight
|
1,200 lb
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
gptkbp:bfsLayer
|
7
|