Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:regional_airliner
|
| gptkbp:bypassRatio |
5.3:1
|
| gptkbp:compressor_stages |
14
|
| gptkbp:configuration |
two-shaft turbofan
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.97 m
|
| gptkbp:family |
gptkb:General_Electric_CF34
|
| gptkbp:firstRun |
1990s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
2.13 m
|
| gptkbp:mainRotorDiameter |
0.97 m
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:market |
regional aviation
|
| gptkbp:thrust |
8,729 lbf
|
| gptkbp:turbine_stages |
4
|
| gptkbp:usedInAircraft |
gptkb:Bombardier_CRJ200
|
| gptkbp:weight |
907 kg
|
| gptkbp:bfsParent |
gptkb:Challenger_650
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF34-3B M
|