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gptkbp:instance_of
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gptkb:jet_engine
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|
gptkbp:aircraft_type
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gptkb:fighter_aircraft
|
|
gptkbp:application
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gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
up to 1500 K
|
|
gptkbp:check_in_time
|
optional
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|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:cooling_system
|
air-cooled
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gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:design_date
|
1950s
|
|
gptkbp:designed_by
|
gptkb:Mikoyan
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:Tumansky_R-25
gptkb:Klimov_RD-500
|
|
gptkbp:engine_configuration
|
single-spool
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_economy
|
average
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
D-30 engine
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:noise_level
|
moderate
|
|
gptkbp:notable_users
|
gptkb:Afghan_Air_Force
gptkb:Algerian_Air_Force
gptkb:Egyptian_Air_Force
gptkb:Soviet_Air_Force
gptkb:Syrian_Air_Force
gptkb:Indian_Air_Force
gptkb:Polish_Air_Force
gptkb:Angolan_Air_Force
gptkb:Kazakh_Air_Force
gptkb:Vietnamese_Air_Force
gptkb:Yugoslav_Air_Force
gptkb:Belarusian_Air_Force
gptkb:Iraqi_Air_Force
gptkb:Ukrainian_Air_Force
gptkb:Hungarian_Air_Force
gptkb:Czechoslovak_Air_Force
gptkb:Libyan_Air_Force
gptkb:Bangladeshi_Air_Force
gptkb:North_Korean_Air_Force
|
|
gptkbp:number_of_rooms
|
annular combustion chamber
|
|
gptkbp:produces
|
over 10,000 units
|
|
gptkbp:production_years
|
1955-1980
|
|
gptkbp:propulsion
|
0.1
80 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:specific_impulse
|
250 s
|
|
gptkbp:successor
|
D-30 F2
|
|
gptkbp:turbine_type
|
single-stage turbine
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Mikoyan_Mi_G-23
gptkb:Mikoyan_Mi_G-21
|
|
gptkbp:variant
|
D-30 KP
D-30 F
|
|
gptkbp:weight
|
about 800 kg
|
|
gptkbp:bfsParent
|
gptkb:Aviadvigatel
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|