Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
business jet
|
| gptkbp:bypassRatio |
5.2:1
|
| gptkbp:certification |
gptkb:Transport_Canada
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
two-spool
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
0.97 m
|
| gptkbp:family |
PW300 series
|
| gptkbp:firstRun |
2001
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW307
|
| gptkbp:introducedIn |
2005
|
| gptkbp:length |
1.7 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfStages |
2
3 axial, 1 centrifugal |
| gptkbp:thrust |
6,400 lbf
|
| gptkbp:usedIn |
gptkb:Dassault_Falcon_8X
gptkb:Dassault_Falcon_7X |
| gptkbp:weight |
650 kg
|
| gptkbp:bfsParent |
gptkb:PW300
|
| gptkbp:bfsLayer |
8
|