|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:business_jet
|
|
gptkbp:average_temperature
|
1,000 ° F
|
|
gptkbp:certification
|
FAA certified
NOx compliant
EASA certified
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_features
|
advanced aerodynamics
high reliability
low maintenance costs
modular construction
high bypass ratio
low noise design
|
|
gptkbp:diameter
|
2.5 ft
|
|
gptkbp:engine
|
gptkb:TFE731
Brayton cycle
|
|
gptkbp:engine_configuration
|
twin-engine
twin-spool
|
|
gptkbp:engine_type
|
turbojet
|
|
gptkbp:first_flight
|
gptkb:1972
|
|
gptkbp:fuel_capacity
|
54 in
1,200 lb
30 in
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Honeywell TFE731-50 R
|
|
gptkbp:launch_window
|
air start
|
|
gptkbp:length
|
4.5 ft
|
|
gptkbp:maintenance
|
3,600 hours
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_applications
|
gptkb:Cessna_Citation_VI
gptkb:Cessna_Citation_VII
gptkb:Hawker_800
gptkb:Bombardier_Learjet_60
gptkb:Gulfstream_G100
|
|
gptkbp:number_of_stages
|
gptkb:14
|
|
gptkbp:operational_range
|
1,000 nautical miles
1,150 statute miles
|
|
gptkbp:power_output
|
3,700 lbf
|
|
gptkbp:propulsion
|
3,700 lbf
|
|
gptkbp:service_ceiling
|
41,000 ft
|
|
gptkbp:turbine_type
|
single shaft
|
|
gptkbp:water_requirement
|
1,200 lb/hr
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Hawker_900_XP_Elite
gptkb:Hawker_900_XP
|
|
gptkbp:bfsLayer
|
6
|