Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:trainer_aircraft
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
8-stage axial
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
17.7 in (0.45 m)
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
Jet-A, JP-4, JP-5, JP-8
|
| https://www.w3.org/2000/01/rdf-schema#label |
J85-GE-21
|
| gptkbp:length |
45.4 in (1.15 m)
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
2,950 lbf (13.1 kN)
|
| gptkbp:type |
afterburning turbojet
|
| 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 |
6
|