|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
1,000 ° C
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
manual control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:design_date
|
1945
|
|
gptkbp:diameter
|
2.5 ft
|
|
gptkbp:emissions_standard
|
non-compliant
|
|
gptkbp:engine
|
gptkb:Soviet_Air_Force
gptkb:fighter_aircraft
gptkb:Klimov_engine_family
gptkb:historical_significance
Cold War era
limited production
post-war development
Brayton cycle
air start
modular assembly
influenced future designs
afterburner option
VK-1 engine replacement
VK-11 M upgrade
|
|
gptkbp:engine_configuration
|
turbine design
turbojet engine configuration
classified specifications
Klimov design team
VK-11-1
|
|
gptkbp:engine_power
|
1960s
high performance
1,000 hours
|
|
gptkbp:engine_production_year
|
1947
|
|
gptkbp:engine_testing_phase
|
prototype testing
|
|
gptkbp:engine_type
|
gptkb:VK-11_A
VK-11 B variant
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:gasoline
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-11 engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
gptkb:Moscow
ground testing
|
|
gptkbp:length
|
3.5 ft
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_history
|
used in Korean War
|
|
gptkbp:propulsion
|
1.5
not available
1,800 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Mikoyan-Gurevich_Mi_G-17
|
|
gptkbp:reliability
|
high
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1_engine
|
|
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
|