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gptkbp:instance_of
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gptkb:jet_engine
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|
gptkbp:application
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gptkb:military_aircraft
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|
gptkbp:certification
|
military certification
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|
gptkbp:combustor_type
|
annular
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|
gptkbp:compressor_type
|
axial
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|
gptkbp:control_system
|
gptkb:manual
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_date
|
1945
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:elevation
|
up to 12,000 m
|
|
gptkbp:emissions_standard
|
gptkb:standard
|
|
gptkbp:engine
|
fighter jets
modular
periodic
Brayton cycle
advanced for its time
modernization projects
air start
influenced future designs
influenced future designs.
limited series
1947-1950
early jet technology
pioneering jet engine
|
|
gptkbp:engine_configuration
|
gptkb:Klimov_design_bureau
classified
inline
robust design
|
|
gptkbp:engine_operational_challenges
|
high maintenance needs
|
|
gptkbp:engine_power
|
high thrust
1,000 hours
evaluated by military
|
|
gptkbp:engine_type
|
gptkb:VK-7_F
gptkb:VK-7_M
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_economy
|
moderate
0.85 lb/hp·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:history
|
derived from VK-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-7 engine
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:noise_level
|
moderate
|
|
gptkbp:notable_users
|
gptkb:Soviet_Union
|
|
gptkbp:operational_history
|
gptkb:Soviet_Air_Force
|
|
gptkbp:operational_use
|
gptkb:Korean_War
|
|
gptkbp:propulsion
|
5.83
7,000 lbf
5.83 lbf/lb
|
|
gptkbp:reliability
|
high
|
|
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
|