Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Pilatus_PC-24
gptkb:Hawker_400XP gptkb:Beechcraft_Premier_I gptkb:Cessna_CitationJet |
| gptkbp:bypassRatio |
2.58:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
two-stage fan, mixed-flow, axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
18.36 in
|
| gptkbp:family |
gptkb:Williams_FJ44
|
| gptkbp:firstRun |
1992
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Williams FJ44-2A turbofan
|
| gptkbp:intendedUse |
business jet
|
| gptkbp:length |
47.2 in
|
| gptkbp:manufacturer |
gptkb:Williams_International
|
| gptkbp:thrust |
2300 lbf
|
| gptkbp:turbineType |
two-stage low-pressure, one-stage high-pressure
|
| gptkbp:weight |
452 lb
|
| gptkbp:bfsParent |
gptkb:Beechcraft_Premier_I
|
| gptkbp:bfsLayer |
7
|