|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:combustion_chamber_type
|
annular
|
|
gptkbp:combustion_efficiency
|
high
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
hydromechanical
|
|
gptkbp:cooling_system
|
gptkb:Interpol
air-cooled
|
|
gptkbp:design
|
Mikhail L. Tumansky
|
|
gptkbp:development
|
1960s
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:emissions_standard
|
moderate
|
|
gptkbp:engine
|
gptkb:fighter_aircraft
various applications
rich history
modular
mass production
Brayton cycle
ongoing development
air start
jet propulsion technology
significant legacy
R-15 family
|
|
gptkbp:engine_configuration
|
turbojet
unique characteristics
advanced design
single spool
detailed specifications
|
|
gptkbp:engine_influence
|
influential design
|
|
gptkbp:engine_power
|
high performance
various metrics
|
|
gptkbp:engine_reliability_metrics
|
various metrics
|
|
gptkbp:engine_type
|
multiple variants
R-15 B-300 P
|
|
gptkbp:first_flight
|
gptkb:1964
|
|
gptkbp:first_introduced
|
gptkb:1965
|
|
gptkbp:fuel_economy
|
2,000 kg/h
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Tumansky R-15 B-300
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
4,200 mm
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
Tumansky
|
|
gptkbp:max_speed
|
Mach 3.2
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notable_feature
|
high thrust-to-weight ratio
|
|
gptkbp:operational_history
|
gptkb:Soviet_Union
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:operational_use
|
1970s
|
|
gptkbp:propulsion
|
no
150 k N
8.0 kg/k N
|
|
gptkbp:related_aircraft
|
gptkb:Challenger
|
|
gptkbp:reliability
|
moderate
|
|
gptkbp:retirement
|
1990s
|
|
gptkbp:successor
|
R-15 B-300 M
|
|
gptkbp:turbine_type
|
axial
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-25
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Mi_G-25
gptkb:Mi_G-25_R
gptkb:Mikoyan_Mi_G-31
|
|
gptkbp:bfsLayer
|
5
|