|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Dassault_Rafale_B
gptkb:Dassault_Rafale_C
gptkb:Dassault_Rafale_M
|
|
gptkbp:certification
|
certified by French authorities
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:design
|
gptkb:Snecma
|
|
gptkbp:development
|
gptkb:Snecma_M88-3
gptkb:Snecma_M88-2
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_RB199
gptkb:General_Electric_F414
gptkb:Eurojet_EJ200
possible
Brayton cycle
air start
|
|
gptkbp:engine_configuration
|
twin-engine
pylon-mounted
|
|
gptkbp:engine_power
|
high performance
high reliability
|
|
gptkbp:engine_type
|
military turbofan
M88-2, M88-3
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:fuel_economy
|
0.85 kg/k N/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Snecma M88
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:Snecma
|
|
gptkbp:military_technology
|
gptkb:none
gptkb:French_Navy
gptkb:French_Air_Force
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:produced_by
|
gptkb:Snecma
|
|
gptkbp:propulsion
|
50 k N
75 k N with afterburner
|
|
gptkbp:service_entry
|
gptkb:2001
|
|
gptkbp:turbine_type
|
high-pressure turbine
low-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:type_of
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Dassault_Rafale
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Dassault_Rafale
|
|
gptkbp:bfsLayer
|
4
|