Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:alternativeName |
HF-2E
|
| gptkbp:countryOfOrigin |
gptkb:Taiwan
|
| gptkbp:diameter |
0.5 m
|
| gptkbp:enteredService |
2005
|
| gptkbp:guidanceSystem |
gptkb:GPS
inertial navigation |
| gptkbp:length |
6.1 m
|
| gptkbp:manufacturer |
gptkb:National_Chung-Shan_Institute_of_Science_and_Technology
|
| gptkbp:platform |
mobile ground launcher
|
| gptkbp:propulsion |
turbojet
|
| gptkbp:range |
600 km
|
| gptkbp:speed |
subsonic
|
| gptkbp:type |
gptkb:surface-to-air_missile
|
| gptkbp:usedBy |
gptkb:Republic_of_China_Armed_Forces
|
| gptkbp:warheadType |
high-explosive
|
| gptkbp:bfsParent |
gptkb:Hsiung_Feng_missile
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Hsiung Feng IIE
|