|
| General Information |
| Developed by |
China |
| Deployed by |
China |
| Development Year |
1965 |
| Deployment Year |
1981 |
| Platform |
silo or, stored in caves and moved outside before launching |
| Number manufactured |
about 30 |
| Number deployed |
10-20(as of 1997) |
| Contractor |
the Wan Yuan Industry Corporation |
| Design |
First Academy of the Ministry of Aerospace Industries |
| Dimensions and Performance |
|
Length |
28.0m(1st-stage:16.7m,2nd-stage:7.0m,warhead:4.3m) |
|
Body Diameter |
2.25m |
|
Launch Weight |
82,000kg |
|
Range |
1,200-4,750km |
|
Accuracy |
1,500m CEP |
| Components |
|
Propulsion |
2-stage liquid-fuel rocket motor |
|
Engine |
1st-stage:4xYF-2A(104T thrust), 2nd-stage:1xYF-3(32T thrust) |
|
Payload |
single warhead 2,200kg |
|
Warhead |
1-3MT nuclear warhead |
|
Guidance |
inertial |
|