Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
regional airliner
|
| gptkbp:bypassRatio |
5.0:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
two-spool
|
| gptkbp:family |
gptkb:CF34
|
| gptkbp:firstFlight |
1995
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF34-8C5
|
| gptkbp:length |
2.62 m
|
| gptkbp:mainRotorDiameter |
137 cm
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfStages |
2
10 |
| gptkbp:thrust |
13,360 lbf
|
| gptkbp:usedIn |
gptkb:Bombardier_CRJ1000
gptkb:Bombardier_CRJ700 gptkb:Bombardier_CRJ900 |
| gptkbp:weight |
907 kg
|
| gptkbp:bfsParent |
gptkb:Bombardier_CRJ-900
gptkb:Bombardier_CRJ700_series gptkb:Bombardier_CRJ900 |
| gptkbp:bfsLayer |
7
|