Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_20
gptkb:Dassault_Falcon_50 gptkb:Learjet_55 |
| gptkbp:bypassRatio |
2.8:1
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
34.5 in
|
| gptkbp:family |
gptkb:TFE731
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:introducedIn |
1982
|
| gptkbp:length |
72.5 in
|
| gptkbp:manufacturer |
gptkb:Garrett_AiResearch
|
| gptkbp:number_of_shafts |
2
|
| gptkbp:thrust |
4200 lbf
|
| gptkbp:weight |
950 lb
|
| gptkbp:bfsParent |
gptkb:BAe_125-1000
gptkb:BAe_125-800 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Garrett TFE731-5R-1H
|