Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:trainer_aircraft
light fighter aircraft |
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
8-stage axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
17.7 in (450 mm)
|
| gptkbp:firstFlight |
1956 (J85 series)
|
| gptkbp:fuelType |
Jet-A, JP-4, JP-5, JP-8
|
| gptkbp:hasTower |
2-stage axial-flow
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J85-GE-21B
|
| 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:F-5S/T_Tiger_II
|
| gptkbp:bfsLayer |
7
|