Tumansky R-11

URI: https://gptkb.org/entity/Tumansky_R-11

GPTKB entity

Predicate	Object
gptkbp:instance_of	gptkb:jet_engine
gptkbp:application	gptkb:military_aircraft
gptkbp:average_temperature	900 ° C
gptkbp:compressor_type	axial compressor
gptkbp:designed_by	Tumansky
gptkbp:diameter	0.9 m
gptkbp:engine	Brayton cycle
gptkbp:engine_configuration	turbojet
gptkbp:first_flight	1947
gptkbp:fuel_economy	0.85 kg/k N·h
gptkbp:fuel_type	kerosene
https://www.w3.org/2000/01/rdf-schema#label	Tumansky R-11
gptkbp:introduced	1950
gptkbp:length	3.5 m
gptkbp:notable_users	gptkb:Soviet_Air_Force gptkb:Polish_Air_Force gptkb:Czechoslovak_Air_Force
gptkbp:produced_by	gptkb:Soviet_Union
gptkbp:propulsion	50 k N
gptkbp:replaced_by	gptkb:Tumansky_R-25
gptkbp:retired	1970s
gptkbp:successor	gptkb:Tumansky_R-25
gptkbp:turbine_type	single-stage turbine
gptkbp:type	gptkb:turbofan_engine
gptkbp:used_in	gptkb:Mikoyan-Gurevich_Mi_G-17 gptkb:Mikoyan-Gurevich_Mi_G-15 gptkb:Mikoyan-Gurevich_Mi_G-19
gptkbp:weight	400 kg
gptkbp:bfsParent	gptkb:Mikoyan_Mi_G-21 gptkb:Mi_G-21 gptkb:Mi_G-21_F-13 gptkb:Mi_G-21bis
gptkbp:bfsLayer	5