Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compressionRatio |
14-stage axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
43.2 in
|
| gptkbp:firstFlight |
1971
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasTower |
2-stage low pressure, 1-stage high pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric TF34
|
| gptkbp:introducedIn |
1972
|
| gptkbp:length |
61.6 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:relatedTo |
gptkb:General_Electric_CF34
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
9,065 lbf
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:usedIn |
gptkb:S-3_Viking
gptkb:Lockheed_S-3_Viking gptkb:Fairchild_Republic_A-10 A-10 Thunderbolt II |
| gptkbp:weight |
1,557 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_CF34
|
| gptkbp:bfsLayer |
6
|