Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
8:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:US_Air_Force
|
| gptkbp:firstFlight |
1968
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric TF39
|
| gptkbp:introduced |
1970
|
| gptkbp:length |
183 in
|
| gptkbp:mainRotorDiameter |
97 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableFor |
first high-bypass turbofan in military service
|
| gptkbp:numberOfAxles |
3
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:General_Electric_CF6
|
| gptkbp:thrust |
43,000 lbf
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:usedIn |
gptkb:Lockheed_C-5_Galaxy
|
| gptkbp:weight |
8,400 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_CF6
|
| gptkbp:bfsLayer |
5
|