Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
8-stage axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
17.7 in (450 mm)
|
| gptkbp:family |
gptkb:General_Electric_J85
|
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
45.4 in (1,153 mm)
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:thrust |
yes
2,950 lbf (13.1 kN) |
| gptkbp:usedIn |
gptkb:Northrop_F-5_Freedom_Fighter
gptkb:Aero_L-39_Albatros_(modified) T-38 Talon |
| gptkbp:weight |
584 lb (265 kg)
|
| gptkbp:bfsParent |
gptkb:General_Electric_J85
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
J85-GE-13
|