Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_10
gptkb:Learjet_35 gptkb:Learjet_36 |
| gptkbp:bypassRatio |
2.8:1
|
| gptkbp:compressor_type |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
31 in
|
| gptkbp:family |
gptkb:TFE731
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Garrett TFE731-2-2B
|
| gptkbp:introducedIn |
1972
|
| gptkbp:length |
63 in
|
| gptkbp:manufacturer |
gptkb:Garrett_AiResearch
|
| gptkbp:numberOfStages |
2
4 axial, 1 centrifugal |
| gptkbp:thrust |
3700 lbf
|
| gptkbp:weight |
820 lb
|
| gptkbp:bfsParent |
gptkb:Learjet_35A
|
| gptkbp:bfsLayer |
6
|