Statements (71)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
manual.
|
| gptkbp:cooling_system |
air-cooled.
uses air cooling. |
| gptkbp:country_of_origin |
gptkb:Soviet_Union
|
| gptkbp:design_features |
simple design.
|
| gptkbp:development |
derived from the VK-1 engine.
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:engine |
1947-1955.
Brayton cycle. developed during the early Cold War. done in factories in the Soviet Union. in various military aircraft. included in later models. influenced future Soviet jet engine designs. ongoing after initial production. reflected in later models. |
| gptkbp:engine_configuration |
straight-through
detailed in technical manuals. focus on simplicity and reliability. inline. led by Mikhail Klimov. |
| gptkbp:engine_design_characteristics |
noted for its compact size.
|
| gptkbp:engine_design_iterations |
led to enhanced performance.
|
| gptkbp:engine_design_legacy |
influenced future jet engine designs.
|
| gptkbp:engine_historical_documentation |
preserved in military archives.
|
| gptkbp:engine_historical_impact |
significant in aviation history.
|
| gptkbp:engine_operational_challenges |
faced during its service life.
|
| gptkbp:engine_operational_history_documentation |
recorded in military history.
|
| gptkbp:engine_performance_improvements |
achieved through iterative design.
|
| gptkbp:engine_power |
approximately 1000 hours.
evaluated during flight tests. improved over predecessors. |
| gptkbp:engine_production_challenges |
overcame during its manufacturing.
|
| gptkbp:engine_production_facilities |
located in the Soviet Union.
|
| gptkbp:engine_specifications_documentation |
compiled for engineers.
|
| gptkbp:engine_technical_documentation |
available in archives.
|
| gptkbp:engine_testing_phase |
completed in 1946.
|
| gptkbp:engine_testing_results |
published in aviation journals.
|
| gptkbp:engine_type |
VK-48 A, VK-48 B.
|
| gptkbp:first_flight |
1947
|
| gptkbp:fuel_economy |
average.
0.85 kg/kgf·h. |
| gptkbp:fuel_type |
kerosene
|
| gptkbp:historical_significance |
paved the way for future jet engines.
|
| https://www.w3.org/2000/01/rdf-schema#label |
Klimov VK-48 engine
|
| gptkbp:ignition_system |
spark ignition.
|
| gptkbp:is_tested_for |
Moscow.
conducted in the late 1940s. |
| gptkbp:length |
4.1 m
|
| gptkbp:maintenance |
short.
|
| gptkbp:manufacturer |
Klimov
|
| gptkbp:max_speed |
Mach 0.9.
|
| gptkbp:noise_level |
high.
|
| gptkbp:notable_users |
Soviet Air Force.
|
| gptkbp:operational_history |
used in various aircraft during the 1950s.
|
| gptkbp:operational_range |
limited to subsonic speeds.
|
| gptkbp:propulsion |
3.0.
2400 kgf |
| gptkbp:related_aircraft |
compatible with several Soviet aircraft.
|
| gptkbp:reliability |
moderate.
|
| gptkbp:successor |
gptkb:Klimov_VK-1
|
| gptkbp:turbine_type |
single-stage
|
| gptkbp:type |
turbojet
|
| gptkbp:used_in |
gptkb:Mikoyan-Gurevich_Mi_G-15
|
| gptkbp:weight |
800 kg
|
| gptkbp:bfsParent |
gptkb:Klimov_design_bureau
|
| gptkbp:bfsLayer |
7
|