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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_operated
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gptkb:Dassault_Mirage_2000_D
gptkb:Dassault_Mirage_2000_N
gptkb:Dassault_Mirage_2000-5
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gptkbp:combustor_type
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annular combustor
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gptkbp:compressor_type
|
axial compressor
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gptkbp:control_system
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gptkb:FADEC
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gptkbp:development
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gptkb:Snecma_M53-P2
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gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:engine
|
gptkb:Snecma_M53-P2
gptkb:General_Electric_F404
gptkb:Pratt_&_Whitney_F119
gptkb:Rolls-Royce_RB199
gptkb:Mitsubishi_F3
Brayton cycle
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gptkbp:engine_configuration
|
twin-spool
|
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gptkbp:engine_power
|
high efficiency
reliable operation
high thrust-to-weight ratio
low noise level
good acceleration
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|
gptkbp:first_flight
|
gptkb:1978
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|
gptkbp:first_introduced
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gptkb:1980
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|
gptkbp:fuel_economy
|
0.85 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Snecma M53
|
|
gptkbp:is_tested_for
|
static test
flight test
ground test
|
|
gptkbp:length
|
approximately 3.8 m
|
|
gptkbp:maintenance
|
modular design
|
|
gptkbp:manufacturer
|
gptkb:Snecma
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:notable_users
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Egyptian_Air_Force
gptkb:Qatar_Air_Force
gptkb:Indian_Air_Force
gptkb:French_Air_Force
|
|
gptkbp:propulsion
|
7.5:1
around 9,000 lbf
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:Snecma_M88
|
|
gptkbp:turbine_type
|
axial turbine
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Dassault_Mirage_2000
|
|
gptkbp:weight
|
about 1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Dassault_Mirage_2000-9
gptkb:Mirage_2000_D
gptkb:Mirage_2000_N
gptkb:Mirage_2000-5
gptkb:Heinkel_aircraft
|
|
gptkbp:bfsLayer
|
6
|