Rolls-Royce AE 3009

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instanceOf turbofan engine
gptkbp:aircraft military jets
compatible with various military aircraft
gptkbp:application military aircraft
gptkbp:climate high operating temperature
gptkbp:controls gptkb:full_authority_digital_engine_control_(FADEC)
digital engine control
gptkbp:coolingSystem advanced cooling technology
gptkbp:customerService comprehensive customer support
gptkbp:design high bypass ratio
gptkbp:design_feature modular design
gptkbp:developer gptkb:Rolls-Royce_AE_3007
gptkbp:diameter approximately 60 inches
gptkbp:electrification turbofan powerplant
gptkbp:emissionsStandard low emissions
gptkbp:engine approximately 3 feet
approximately 12 feet
gptkbp:engineType axial compressor
high-pressure turbine
multiple variants available
turbofan engine type
gptkbp:firstFlight 1990
gptkbp:fuel_capacity high fuel efficiency
low fuel consumption
gptkbp:fuelType gptkb:Jet_A-1
annular combustor
gptkbp:future_plans future developments planned
gptkbp:global_presence global market presence
gptkbp:hasArea extensive testing conducted
https://www.w3.org/2000/01/rdf-schema#label Rolls-Royce AE 3009
gptkbp:innovation engine innovation
gptkbp:inspiration reduce operational costs
gptkbp:maintenance long maintenance intervals
gptkbp:manufacturer gptkb:Rolls-Royce
gptkbp:market_segment military aviation
gptkbp:noise_level low noise
gptkbp:notableUsers gptkb:Boeing_737_AEW&C
gptkbp:operationalRange military operations
gptkbp:partnerships strategic partnerships established
gptkbp:performances optimized performance
gptkbp:productionYears 1980s to 1990s
gptkbp:propulsion high thrust-to-weight ratio
approximately 20,000 lbf
gptkbp:related_engine gptkb:Rolls-Royce_AE_3007
gptkb:AE_family
Brayton_cycle
gptkbp:reliability high reliability
gptkbp:service_ceiling high service ceiling
gptkbp:setting twin-spool
gptkbp:sustainability focus on sustainability
gptkbp:team Rolls-Royce_design_team
gptkbp:weight approximately 3,000 lb