|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
gptkb:Tupolev_aircraft
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:built
|
over 1,000
|
|
gptkbp:climate
|
1,000 °C
|
|
gptkbp:controls
|
manual control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:crew
|
1
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissionsStandard
|
non-compliant
|
|
gptkbp:engine
|
inline engine
R-15B-300
|
|
gptkbp:engineConfiguration
|
turbojet
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:exhaustSystem
|
straight exhaust
subsonic intake
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuel_capacity
|
0.8 kg/kN·h
|
|
gptkbp:fuelType
|
kerosene
spark plug ignition
annular combustion chamber
can-type combustor
fuel pump system
|
|
gptkbp:hasDepartment
|
optional
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Tumansky R-15B-300
|
|
gptkbp:introduced
|
1955
|
|
gptkbp:is_used_in
|
gptkb:Tupolev_Tu-95
|
|
gptkbp:length
|
4.2 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
Tumansky
|
|
gptkbp:maximum_speed
|
1,000 km/h
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notable_feature
|
high thrust-to-weight ratio
|
|
gptkbp:operational_status
|
gptkb:Soviet_Air_Force
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:productionYears
|
1950s
|
|
gptkbp:propulsion
|
not available
15,000 lbf
|
|
gptkbp:related_engine
|
gptkb:Tumansky_R-11F-300
Brayton_cycle
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
strategic bomber engine
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:serviceType
|
1955-1990s
|
|
gptkbp:successor
|
gptkb:Tumansky_R-15B-300M
|
|
gptkbp:team
|
gptkb:Mikhail_Tumansky
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:weight
|
1,500 kg
|