Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:armament |
gptkb:M61_Vulcan
bombs air-to-air missiles air-to-surface missiles |
| gptkbp:countryOfOrigin |
gptkb:Taiwan
|
| gptkbp:crew |
1
|
| gptkbp:developedBy |
gptkb:AIDC_F-CK-1_Ching-Kuo
|
| gptkbp:engine |
Honeywell F125-70
|
| gptkbp:engineType |
turbofan
|
| gptkbp:height |
4.42 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
F-CK-1C
|
| gptkbp:introduced |
2002
|
| gptkbp:length |
14.21 m
|
| gptkbp:manufacturer |
gptkb:Aerospace_Industrial_Development_Corporation
|
| gptkbp:maximumSpeed |
Mach 1.8
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:primaryUser |
gptkb:Republic_of_China_Air_Force
|
| gptkbp:role |
multirole fighter
|
| gptkbp:usedBy |
gptkb:Republic_of_China_Air_Force
|
| gptkbp:wingspan |
9.46 m
|
| gptkbp:bfsParent |
gptkb:F-CK-1_Ching-kuo
gptkb:AIDC_F-CK-1_Ching-Kuo |
| gptkbp:bfsLayer |
6
|