Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:business_jet
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
2.5 ft
|
| gptkbp:elevation |
FL410
|
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:exhaust_system |
mixed flow
|
| 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 |
TFE731-40 R
|
| gptkbp:length |
4.5 ft
|
| gptkbp:manufacturer |
gptkb:Honeywell
|
| gptkbp:noise_level |
Stage 3
|
| gptkbp:number_of_stages |
gptkb:14
|
| gptkbp:propulsion |
4000 lbf
|
| gptkbp:weight |
800 lb
|
| gptkbp:bfsParent |
gptkb:Learjet_60
gptkb:Hawker_750 |
| gptkbp:bfsLayer |
6
|