Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:aircraft_operated |
gptkb:Cessna_Citation_III
gptkb:Gulfstream_G150 gptkb:Bombardier_Learjet_60 |
| gptkbp:application |
gptkb:business_jet
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
approximately 2.5 ft
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:engine_configuration |
twin-engine
|
| gptkbp:first_flight |
gptkb:1980
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell TFE731-40 R
|
| gptkbp:length |
approximately 4.5 ft
|
| gptkbp:maintenance |
4000 hours
|
| gptkbp:manufacturer |
gptkb:Honeywell
|
| gptkbp:max_speed |
Mach 0.80
|
| gptkbp:noise_level |
Stage 3 compliant
|
| gptkbp:propulsion |
4000 lbf
|
| gptkbp:service_ceiling |
41,000 ft
|
| gptkbp:turbine_type |
two-spool turbine
|
| gptkbp:weight |
approximately 600 lb
|
| gptkbp:bfsParent |
gptkb:Hawker_750_XP
gptkb:Bombardier_Learjet_60 |
| gptkbp:bfsLayer |
6
|