Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular combustion chamber
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
manual control
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:country_of_origin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engine |
Brayton cycle
extensive documentation exists air start innovative design features produced in large numbers subject of research studies influenced future jet engine designs faced technical challenges during development developed in 1940s widely used in Soviet aircraft influenced future jet engine research part of Soviet aviation history recognized in aviation community |
| gptkbp:engine_awards |
received awards for design excellence
|
| gptkbp:engine_collaborations |
collaborated with various aerospace companies
|
| gptkbp:engine_configuration |
pylon-mounted
detailed specifications available turbojet engine configuration |
| gptkbp:engine_exhibitions |
exhibited in aviation museums
|
| gptkbp:engine_power |
high performance for its time
reliable engine |
| gptkbp:engine_publications |
featured in aviation publications
|
| gptkbp:engine_type |
gptkb:VK-1_engine_variant
|
| gptkbp:first_flight |
1947
|
| gptkbp:fuel_economy |
0.8 kg/s
|
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Klimov VK-32 engine
|
| gptkbp:ignition_system |
spark plug ignition
|
| gptkbp:impact |
significant impact on jet propulsion technology
|
| gptkbp:is_tested_for |
ground testing required
|
| gptkbp:length |
3.5 m
|
| gptkbp:maintenance |
moderate maintenance required
|
| gptkbp:manufacturer |
Klimov
|
| gptkbp:max_speed |
Mach 0.9
|
| gptkbp:noise_level |
high noise level
|
| gptkbp:operational_history |
used in Korean War
|
| gptkbp:propulsion |
8.0
3200 lbf |
| gptkbp:related_aircraft |
gptkb:Mikoyan-Gurevich_Mi_G-17
|
| gptkbp:service_ceiling |
12000 m
|
| 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 |
400 kg
|
| gptkbp:bfsParent |
gptkb:Klimov_design_bureau
|
| gptkbp:bfsLayer |
7
|