Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
17.7 in
|
| gptkbp:family |
gptkb:General_Electric_J85
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:length |
45.4 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfStages |
2
8 |
| gptkbp:status |
in service
|
| gptkbp:thrust |
2,950 lbf dry
4,300 lbf with afterburner |
| gptkbp:usedIn |
gptkb:Northrop_F-5_Freedom_Fighter
T-38 Talon |
| gptkbp:weight |
584 lb
|
| gptkbp:bfsParent |
gptkb:Cessna_A-37B_Dragonfly
gptkb:A-37B_Dragonfly gptkb:Cessna_A-37_Dragonfly |
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
General Electric J85-GE-17A
|