Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.89 m
|
| gptkbp:firstFlight |
1980s
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell F125
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:relatedTo |
gptkb:Honeywell_F124
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
12,000 lbf (53 kN)
9,000 lbf (40 kN) dry |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:AIDC_F-CK-1_Ching-Kuo
AIDC F-CK-1C/D Hsiang Sheng |
| gptkbp:weight |
1,090 kg
|
| gptkbp:bfsParent |
gptkb:Indigenous_Defense_Fighter
gptkb:Honeywell_F124 gptkb:F125 |
| gptkbp:bfsLayer |
8
|