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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Dassault_Mirage_5
gptkb:Mirage_III
gptkb:Dassault_Mirage_F1
gptkb:Dassault_Mirage_4
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|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:controls
|
gptkb:football_match
|
|
gptkbp:cooling_system
|
air-cooled
air-cooled system
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|
gptkbp:developer
|
1960s to 1970s
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissions_standard
|
gptkb:Euro_I
convergent nozzle
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:advanced_technology
gptkb:SNECMA_Atar_9_K-50_R
gptkb:battle
high performance
mass production
high reliability
Brayton cycle
twin-spool
subsonic inlet
Atar family
SNECMA design
used in multiple aircraft.
|
|
gptkbp:engine_type
|
gptkb:Atar_9_K-50_R
turbojet
axial compressor
single-stage turbine
|
|
gptkbp:first_flight
|
gptkb:1978
|
|
gptkbp:first_introduced
|
gptkb:Dassault_Mirage_F1
|
|
gptkbp:fuel_capacity
|
0.9 m
1,200 kg
3.8 m
2,000 kg/h
0.85 kg/k N/h
|
|
gptkbp:fuel_type
|
gptkb:Company
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SNECMA Atar 9 K-50
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:SNECMA
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
afterburner
|
|
gptkbp:operational_area
|
gptkb:1980s
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
gptkb:battle
4.2
50 k N
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:successor
|
gptkb:SNECMA_M88
|
|
gptkbp:used_in
|
gptkb:Dassault_Mirage_2000
|
|
gptkbp:weight
|
approximately 1,200 kg
|