Klimov VK-15 engine

GPTKB entity

Statements (53)
Predicate Object
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