Rolls-Royce Tay 650

GPTKB entity

Statements (48)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 6
gptkbp:bfsParent gptkb:Rolls-Royce_Tay_620
gptkbp:application gptkb:engine
gptkbp:bypass_ratio 4.5:1
gptkbp:certification FAA certified
EASA certified
gptkbp:controls gptkb:football_match
gptkbp:cooling_system air-cooled
gptkbp:diameter 0.9 m
1.5 m
gptkbp:engine gptkb:dual-channel_FADEC
low emissions
advanced aerodynamics
improved performance
modular design
advanced materials
high reliability
high efficiency
twin-spool
high bypass ratio
high thrust-to-weight ratio
robust design
excellent performance
reduced fuel consumption
high bypass ratio fan
full authority digital engine control
gptkbp:engine_type turbofan
axial
gptkbp:first_flight gptkb:1990
gptkbp:fuel_capacity 0.9 m
1.5 m
0.5 lb/h/lbf
gptkbp:fuel_type gptkb:Jet_A-1
https://www.w3.org/2000/01/rdf-schema#label Rolls-Royce Tay 650
gptkbp:length 1.5 m
gptkbp:maintenance low maintenance
gptkbp:manufacturer gptkb:film_production_company
gptkbp:noise_level low noise
gptkbp:notable_users gptkb:Gulfstream_G550
gptkb:Dassault_Falcon_7_X
gptkb:Bombardier_Global_Express
gptkbp:number_of_stages gptkb:5
gptkbp:operational_area commercial aviation
gptkbp:propulsion 6500 lbf
gptkbp:successor Rolls-Royce B R710
gptkbp:weight 1500 lb
gptkbp:year_created gptkb:1990