General Electric TF34-GE-100A
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
6.2:1
|
| gptkbp:compressionRatio |
2-stage fan, 14-stage axial compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
43 in
|
| gptkbp:family |
gptkb:General_Electric_TF34
|
| gptkbp:firstFlight |
1972
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasTower |
4-stage low-pressure, 2-stage high-pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric TF34-GE-100A
|
| gptkbp:length |
100 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:relatedTo |
gptkb:General_Electric_CF34
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
9,065 lbf
|
| gptkbp:type |
turbofan
|
| gptkbp:usedIn |
A-10 Thunderbolt II
|
| gptkbp:weight |
1,557 lb
|
| gptkbp:bfsParent |
gptkb:Fairchild_Republic_A-10_Thunderbolt_II
|
| gptkbp:bfsLayer |
6
|