|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
gptkb:Mikoyan_MiG-31
|
|
gptkbp:application
|
military aviation
|
|
gptkbp:commissioningDate
|
1958
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:coolingSystem
|
air-cooled
advanced cooling system
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:emissionsStandard
|
Stage 3
|
|
gptkbp:engine
|
modular
interceptor aircraft
Soviet_design
|
|
gptkbp:engineConfiguration
|
mass production
single-spool
state-funded project
|
|
gptkbp:engineType
|
turbojet
axial
afterburner
multiple variants developed
R-29-300
|
|
gptkbp:firstFlight
|
1964
|
|
gptkbp:fuel_capacity
|
high
0.85 kg/kN·h
|
|
gptkbp:fuelType
|
annular
kerosene
|
|
gptkbp:hasArea
|
gptkb:Moscow
ground testing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Tumansky R-29
|
|
gptkbp:introduced
|
1965
|
|
gptkbp:is_used_in
|
gptkb:Mikoyan_MiG-25
|
|
gptkbp:length
|
4.1 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
Tumansky
|
|
gptkbp:maximum_speed
|
gptkb:Mach_3.2
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notableUsers
|
gptkb:Soviet_Union
|
|
gptkbp:operational_status
|
gptkb:Soviet_Air_Force
|
|
gptkbp:operationalHistory
|
part_of_Soviet_aviation_history.
|
|
gptkbp:operationalRange
|
2000 km
|
|
gptkbp:performances
|
classified
1000 hours
high performance
high reliability
major overhaul required every 500 hours
|
|
gptkbp:productionYears
|
6 years
|
|
gptkbp:propulsion
|
not equipped
150 kN
0.1875
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:reliability
|
0.95
|
|
gptkbp:successor
|
gptkb:Tumansky_R-33
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:updates
|
upgraded versions available
|
|
gptkbp:weight
|
800 kg
|