Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_900DX
gptkb:Dassault_Falcon_900LX |
| gptkbp:bypassRatio |
4.2:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
two-spool
|
| gptkbp:diameter |
34.2 in
|
| gptkbp:family |
gptkb:TFE731
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasTower |
two-stage low pressure, one-stage high pressure
|
| gptkbp:introducedIn |
2005
|
| gptkbp:length |
72.6 in
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:market |
gptkb:business_jet
|
| gptkbp:thrust |
4600 lbf
|
| gptkbp:weight |
950 lb
|
| gptkbp:bfsParent |
gptkb:Dassault_Falcon_900B
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell TFE731-5BR-1C
|