Klimov RD-500

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 5
gptkbp:bfsParent gptkb:Su-25_Frogfoot
gptkb:Su-25_UTG
gptkb:Yakovlev_Yak-130
gptkb:Yak-130
gptkbp:aircraft_operated fighter jets
gptkbp:application gptkb:aircraft
gptkbp:average_temperature 1,000 ° C
gptkbp:controls manual control
gptkbp:cooling_system air-cooled
gptkbp:date 1945
gptkbp:diameter 0.9 m
gptkbp:engine turbofan
high reliability
Brayton cycle
single-spool
high thrust-to-weight ratio
various military aircraft
1,000 hours
air start
detailed specifications available
produced in large numbers
moderate efficiency
developed in post-war era
characteristics include high thrust
upgraded to RD-600
gptkbp:engine_type gptkb:RD-500_A
2
8
gptkbp:first_flight 1947
gptkbp:fuel_capacity 0.85 lb/lbf/hr
2,000 lb/hr
gptkbp:fuel_type kerosene
annular combustion chamber
https://www.w3.org/2000/01/rdf-schema#label Klimov RD-500
gptkbp:ignition_system spark plug ignition
gptkbp:is_tested_for ground testing
gptkbp:length 3.5 m
gptkbp:maintenance 500 hours
gptkbp:manufacturer Klimov
gptkbp:noise_level 85 d B
gptkbp:notable_users gptkb:Soviet_Air_Force
gptkbp:operational_history used in Korean War
gptkbp:origin gptkb:Monarch
gptkbp:propulsion 4.17
5,000 lbf
gptkbp:replaced_by gptkb:Klimov_RD-600
gptkbp:successor gptkb:Klimov_RD-600
gptkbp:type axial-flow turbojet
gptkbp:used_in gptkb:Mikoyan-Gurevich_Mi_G-15
gptkbp:weight 1,200 lb