|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
MiG-15
MiG-17
|
|
gptkbp:application
|
military aviation
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
derived_from_Rolls-Royce_Nene
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
modular design
influenced future designs
single shaft
turbojet layout
aluminum alloys
|
|
gptkbp:engineConfiguration
|
mass production
single-spool
centrifugal compressor
|
|
gptkbp:engineType
|
turbojet
afterburning turbojet
axial compressor
several variants developed
|
|
gptkbp:firstFlight
|
1949
|
|
gptkbp:firstRace
|
1947
|
|
gptkbp:fuel_capacity
|
0.85 lb/hp/hr
|
|
gptkbp:fuelType
|
kerosene
annular combustor
|
|
gptkbp:hasArea
|
military certification
ground testing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Tumansky RD-500
|
|
gptkbp:is_designed_to
|
Tumansky
|
|
gptkbp:is_used_in
|
gptkb:Mikoyan-Gurevich_MiG-15
gptkb:Mikoyan-Gurevich_MiG-17
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:notableUsers
|
gptkb:Soviet_Air_Force
gptkb:Korean_People's_Air_Force
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:operational_status
|
1950s
|
|
gptkbp:operationalHistory
|
part_of_Cold_War_aviation_history
|
|
gptkbp:origin
|
gptkb:Soviet_Union
|
|
gptkbp:performances
|
high reliability
high thrust-to-weight ratio
low maintenance requirements
detailed specifications available.
|
|
gptkbp:propulsion
|
5,000 lbf
|
|
gptkbp:related_engine
|
gptkb:Tumansky_engines
Brayton_cycle
|
|
gptkbp:replacedBy
|
gptkb:Tumansky_R-11F-300
|
|
gptkbp:successor
|
gptkb:Tumansky_R-11
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:updates
|
upgraded versions available
|
|
gptkbp:weight
|
1,200 lb
|