Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
6.2:1
|
| gptkbp:compressionRatio |
axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
46 in
|
| gptkbp:family |
gptkb:General_Electric_TF34_family
|
| gptkbp:firstFlight |
1971
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
75 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
9,065 lbf
|
| gptkbp:usedInAircraft |
gptkb:S-3_Viking
A-10 Thunderbolt II |
| gptkbp:weight |
1,557 lb
|
| gptkbp:bfsParent |
gptkb:CF34
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
TF34 military engine
|