|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:fighter_aircraft
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
6:1
|
|
gptkbp:control_system
|
manual control
|
|
gptkbp:cooling_system
|
air-cooled
air cooling
|
|
gptkbp:design_date
|
1947
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
gptkb:Klimov_VK-1_F
1950s
post-World War II
Brayton cycle
electric start
|
|
gptkbp:engine_afterburner
|
no
|
|
gptkbp:engine_configuration
|
gptkb:Klimov_design_bureau
simple design
inline
single-spool
3,000 lbf
|
|
gptkbp:engine_cooling_air_source
|
ambient air
|
|
gptkbp:engine_inlet_type
|
subsonic inlet
|
|
gptkbp:engine_operational_altitude
|
up to 12,000 m
|
|
gptkbp:engine_operational_role
|
powerplant for aircraft
|
|
gptkbp:engine_outlet_type
|
convergent nozzle
|
|
gptkbp:engine_power
|
high performance
1,000 hours
moderate efficiency
moderate reliability
|
|
gptkbp:engine_thrust_augmentation
|
gptkb:none
|
|
gptkbp:engine_weight-to-thrust_ratio
|
0.4
|
|
gptkbp:exhaust_system
|
straight exhaust
|
|
gptkbp:first_flight
|
1950
|
|
gptkbp:fuel_economy
|
0.85 lb/hp/hr
0.5 kg/s
|
|
gptkbp:fuel_type
|
kerosene
gravity feed
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-3 engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_history
|
1950s
|
|
gptkbp:operational_use
|
gptkb:Soviet_Air_Force
|
|
gptkbp:propulsion
|
no
2.5
3,000 lbf
|
|
gptkbp:successor
|
gptkb:Klimov_VK-1
|
|
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
|