Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:accuracy |
30-45 m CEP
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:diameter |
1 m
|
| gptkbp:enteredService |
1990s
|
| gptkbp:guidanceSystem |
inertial
satellite guidance |
| gptkbp:launchWeight |
6,200 kg
|
| gptkbp:length |
9.1 m
|
| gptkbp:manufacturer |
gptkb:China_Academy_of_Launch_Vehicle_Technology
|
| gptkbp:NATOReportingName |
gptkb:CSS-6
|
| gptkbp:platform |
road-mobile transporter erector launcher
|
| gptkbp:propulsion |
solid fuel
|
| gptkbp:range |
600 km
|
| gptkbp:usedBy |
gptkb:People's_Liberation_Army_Rocket_Force
|
| gptkbp:variant |
DF-15A
DF-15B DF-15C |
| gptkbp:warheadType |
nuclear
conventional |
| gptkbp:bfsParent |
gptkb:PLARF
gptkb:PLA_Rocket_Force |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
DF-15 SRBM
|