Statements (53)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:aircraft_operated |
compatible with multiple fighter jets
integrated into multiple aircraft models |
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:controls |
manual control system
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design |
designed by Klimov design bureau
|
| gptkbp:developer |
1950s
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:elevation |
effective at high altitudes
|
| gptkbp:emissions_standard |
high emissions
|
| gptkbp:engine |
Brayton cycle
turbojet engine configuration limited operational life mounted on aircraft fuselage requires external starter |
| gptkbp:engine_type |
axial compressor
single-stage turbine several variants developed |
| gptkbp:exported_to |
gptkb:various_countries
|
| gptkbp:features |
simple design features
|
| gptkbp:first_flight |
gptkb:1955
|
| gptkbp:fuel_capacity |
moderate fuel efficiency
high fuel consumption rate |
| gptkbp:fuel_type |
kerosene
annular combustion chamber |
| gptkbp:historical_event |
used in Cold War era aircraft.
|
| gptkbp:historical_significance |
important in Soviet aviation history
|
| https://www.w3.org/2000/01/rdf-schema#label |
Klimov VK-28 engine
|
| gptkbp:influenced_by |
earlier Soviet jet engines
|
| gptkbp:is_tested_for |
extensively tested before deployment
tested in various conditions |
| gptkbp:legacy |
influenced future jet engine designs
|
| gptkbp:length |
3.5 m
|
| gptkbp:maintenance |
requires regular maintenance
|
| gptkbp:manufacturer |
Klimov
|
| gptkbp:material |
made from high-strength alloys
|
| gptkbp:noise_level |
high noise level
|
| gptkbp:operational_history |
used in various Soviet aircraft
|
| gptkbp:origin |
gptkb:Monarch
|
| gptkbp:performance |
high thrust-to-weight ratio
|
| gptkbp:production_years |
produced from 1955 to 1970
|
| gptkbp:propulsion |
no thrust vectoring
2800 lbf |
| gptkbp:reliability |
reliable engine
|
| gptkbp:replaced_by |
gptkb:Klimov_VK-30_engine
|
| gptkbp:specifies |
detailed technical specifications available
|
| gptkbp:successor |
gptkb:Klimov_VK-30
|
| gptkbp:type |
turbojet
|
| gptkbp:used_in |
gptkb:Mikoyan_Mi_G-21
|
| gptkbp:weight |
400 kg
|
| gptkbp:bfsParent |
gptkb:Klimov_design_bureau
|
| gptkbp:bfsLayer |
7
|