General Electric J85-GE-21 turbojet
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressor_type |
8-stage axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
17.7 in (450 mm)
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric J85-GE-21 turbojet
|
| gptkbp:length |
45.4 in (1,153 mm)
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:part_of |
gptkb:General_Electric_J85_engine_family
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
yes
5,000 lbf (22.24 kN) with afterburner |
| gptkbp:turbineType |
2-stage axial-flow
|
| gptkbp:usedInAircraft |
gptkb:Northrop_F-5_Freedom_Fighter
T-38 Talon |
| gptkbp:weight |
584 lb (265 kg)
|
| gptkbp:bfsParent |
gptkb:F-5E_Tiger_II
|
| gptkbp:bfsLayer |
6
|