SNECMA Atar 9 B

URI: https://gptkb.org/entity/SNECMA_Atar_9_B
GPTKB entity
Statements (33)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:compressor_type 8
gptkbp:cooling_system air-cooled
gptkbp:design gptkb:SNECMA
gptkbp:development 1950s to 1960s
gptkbp:diameter 0.9 m
gptkbp:engine gptkb:Rolls-Royce_Avon
Brayton cycle
gptkbp:engine_configuration turbojet
single-spool
gptkbp:first_flight gptkb:1956
gptkbp:fuel_economy 0.85 kg/k N·h
gptkbp:fuel_type kerosene
https://www.w3.org/2000/01/rdf-schema#label SNECMA Atar 9 B
gptkbp:ignition_system gptkb:spark_plug
gptkbp:intended_use gptkb:military_aircraft
gptkbp:length 4.1 m
gptkbp:manufacturer gptkb:SNECMA
gptkbp:max_speed Mach 2.2
gptkbp:number_of_rooms annular
gptkbp:operational_history gptkb:French_Air_Force
gptkbp:operational_use 1960s
gptkbp:propulsion 7.5:1
around 9,000 lbf
gptkbp:related_aircraft Mirage family
gptkbp:successor gptkb:SNECMA_M53
gptkbp:turbine_type 2
gptkbp:type afterburning turbojet
gptkbp:used_in gptkb:Dassault_Mirage_III
gptkbp:variant Atar 9 C
gptkbp:weight 1,200 kg
gptkbp:bfsParent gptkb:Dassault_Mirage_3
gptkbp:bfsLayer 5