Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:aircraft |
gptkb:Cessna_Citation_series
|
| gptkbp:application |
business jets
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
approximately 2.5 ft
|
| gptkbp:emissionsStandard |
Stage 4
|
| gptkbp:engineType |
axial compressor
two-spool turbine |
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuel_capacity |
0.5 lb/hp/hr
|
| gptkbp:fuelType |
Jet A
|
| https://www.w3.org/2000/01/rdf-schema#label |
TFE731-40T
|
| gptkbp:length |
approximately 4.5 ft
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Honeywell
|
| gptkbp:noise_level |
low noise
|
| gptkbp:number_of_stages |
8 stages
|
| gptkbp:propulsion |
4000 lbf
|
| gptkbp:related_engine |
Brayton_cycle
|
| gptkbp:weight |
approximately 800 lb
|