Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:business_jet
|
| gptkbp:bypass_ratio |
3.5:1
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
2.5 ft
|
| gptkbp:first_flight |
gptkb:1996
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Williams International FJ44
|
| gptkbp:length |
4.5 ft
|
| gptkbp:manufacturer |
gptkb:Williams_International
|
| gptkbp:notable_users |
gptkb:Embraer_Phenom_300
gptkb:Hawker_4000 gptkb:Cessna_Citation_X |
| gptkbp:propulsion |
3,400 lbf
|
| gptkbp:turbine_type |
single-stage high-pressure turbine
|
| gptkbp:weight |
600 lb
|
| gptkbp:bfsParent |
gptkb:T-7_A_Red_Hawk
|
| gptkbp:bfsLayer |
5
|