|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:La-17_fighter_aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:Tupolev_Tu-16
bombers
|
|
gptkbp:average_temperature
|
1,000 ° C
|
|
gptkbp:controls
|
manual control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:decommissioned
|
1960s
|
|
gptkbp:design
|
simple design
Mikulin design bureau
|
|
gptkbp:developer
|
Mikulin RD-500 A
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:engine
|
gptkb:RD-500_A
turbojet
Brayton cycle
inline engine
air start
RD-500-1
|
|
gptkbp:engine_type
|
axial compressor
single-stage turbine
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_capacity
|
moderate
0.8 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
annular combustion chamber
|
|
gptkbp:historical_significance
|
first Soviet turbojet engine
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mikulin RD-500
|
|
gptkbp:influenced_by
|
German turbojet technology
|
|
gptkbp:inspired_by
|
gptkb:Whittle_engine
|
|
gptkbp:legacy
|
influenced future Soviet jet engines
|
|
gptkbp:length
|
4,200 mm
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Mikulin
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notable_feature
|
afterburner
|
|
gptkbp:notable_users
|
gptkb:Soviet_Air_Force
|
|
gptkbp:operational_area
|
1950s
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:production_years
|
1947-1955
|
|
gptkbp:propulsion
|
0.24
4.17
50 k N
|
|
gptkbp:replaced_by
|
KRD-500 engine
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:successor
|
gptkb:KRD-500
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Tupolev_Tu-4
|
|
gptkbp:weight
|
1,200 kg
|