|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:SNECMA_Atar_9_K-50
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:controls
|
gptkb:football_match
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissions_standard
|
gptkb:Eurofighter_standard
|
|
gptkbp:engine
|
gptkb:SNECMA_M53
high performance
modular design
high reliability
twin-engine
dual-spool
M88-2 upgrade
M88-3 upgrade
M88-4 upgrade
|
|
gptkbp:engine_type
|
gptkb:M88-3
gptkb:M88-2
axial compressor
high-pressure turbine
M88-10
M88-4
M88-5
M88-6
M88-7
M88-8
M88-9
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:fuel_capacity
|
high efficiency
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:has_programs
|
gptkb:Rafale_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SNECMA M88
|
|
gptkbp:is_tested_for
|
flight testing
ground testing
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Snecma
|
|
gptkbp:max_speed
|
Mach 1.8
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
digital engine control system
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
6.25
50 k N
75 k N
|
|
gptkbp:services
|
gptkb:2001
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Dassault_Rafale
|
|
gptkbp:weight
|
1,200 kg
|