|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:aircraft_operated
|
Mirage family
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:controls
|
hydraulic control
|
|
gptkbp:cooling_system
|
air-cooled
air cooling
|
|
gptkbp:developer
|
1950s
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:SNECMA_Atar_9_K-50
low
moderate
discontinued
extensive
high performance
Brayton cycle
inline
moderate efficiency
9,000 lbf
influential in jet engine design.
turbojet design
SNECMA engineers
|
|
gptkbp:engine_type
|
axial compressor
single-stage turbine
Atar 9 K-20
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:fuel_capacity
|
2,500 kg/h
|
|
gptkbp:fuel_type
|
annular
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SNECMA Atar 9 K-30
|
|
gptkbp:ignition_system
|
gptkb:park
|
|
gptkbp:is_tested_for
|
gptkb:Monarch
ground testing
|
|
gptkbp:is_used_by
|
gptkb:French_Air_Force
|
|
gptkbp:length
|
4.1 m
|
|
gptkbp:maintenance
|
modular design
|
|
gptkbp:manufacturer
|
gptkb:SNECMA
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notable_feature
|
afterburner
|
|
gptkbp:operational_area
|
1960s
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:propulsion
|
gptkb:battle
afterburning
7.5:1
around 9,000 lbf
|
|
gptkbp:replaced_by
|
gptkb:SNECMA_M53
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:successor
|
gptkb:SNECMA_M53
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:used_in
|
gptkb:Dassault_Mirage_III
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:SNECMA_Atar_9_K-50_R
|
|
gptkbp:bfsLayer
|
7
|