Ne-20 turbojet engine

URI: https://gptkb.org/entity/Ne-20_turbojet_engine

GPTKB entity

Statements (57)

Predicate	Object
gptkbp:instance_of	gptkb:engine
gptkbp:bfsLayer	6
gptkbp:bfsParent	gptkb:Mitsubishi_J8_M
gptkbp:application	gptkb:aircraft
gptkbp:average_temperature	up to 900 ° C
gptkbp:controls	manual control
gptkbp:cooling_system	air-cooled intercooling
gptkbp:developer	1950s
gptkbp:diameter	0.9 m
gptkbp:emissions_standard	low emissions
gptkbp:engine	annular combustion chamber
gptkbp:engine_type	axial compressor single-stage turbine
gptkbp:first_flight	gptkb:1955
gptkbp:fuel_capacity	moderate efficiency 0.8 kg/k N·h
gptkbp:fuel_type	kerosene
https://www.w3.org/2000/01/rdf-schema#label	Ne-20 turbojet engine
gptkbp:length	3.2 m
gptkbp:maintenance	100 hours
gptkbp:manufacturer	gptkb:NPO_Saturn
gptkbp:noise_level	low noise
gptkbp:operational_range	high altitude
gptkbp:propulsion	20 k N
gptkbp:reliability	high reliability
gptkbp:services	2000 hours
gptkbp:successor	gptkb:AL-7_engine
gptkbp:used_in	gptkb:Tupolev_Tu-95 gptkb:Sukhoi_Su-9 gptkb:Sukhoi_Su-24 gptkb:Sukhoi_Su-25 gptkb:Tupolev_Tu-16 gptkb:Sukhoi_Su-34 gptkb:Antonov_An-70 gptkb:Mikoyan-Gurevich_Mi_G-17 gptkb:Ilyushin_Il-114 gptkb:Ilyushin_Il-28 gptkb:Mikoyan-Gurevich_Mi_G-21 gptkb:Mikoyan-Gurevich_Mi_G-23 gptkb:Mikoyan-Gurevich_Mi_G-25 gptkb:Mikoyan-Gurevich_Mi_G-31 gptkb:Mikoyan-Gurevich_Mi_G-15 gptkb:Tupolev_Tu-214 gptkb:Mikoyan-Gurevich_Mi_G-19 gptkb:Sukhoi_Su-57 gptkb:Sukhoi_Su-7 gptkb:Antonov_An-225 gptkb:Ilyushin_Il-76 gptkb:Sukhoi_Su-11 gptkb:Tupolev_Tu-4 gptkb:Tupolev_Tu-160 gptkb:Sukhoi_Su-15 gptkb:Antonov_An-124 gptkb:Tupolev_Tu-16_K gptkb:Yakolev_Yak-25
gptkbp:weight	150 kg