Specifications |
|
| Contractor | Academy of Rocket Motors Technology - ARMT |
| Configuration | Two Stage |
| Length [meters] | 10.7 |
| Diameter [meters] | 1.4 |
| Mass [kilograms] | 14,700 |
| Propellant | Solid |
| Guidance | Inertial |
| First Flight | 12 October 1982 |
| IOC | 1988 |
| Deployment | type-092 SSBN |
| Range (km) | 1,700 |
| Re-entry Vehicle Mass (kg) | 600 |
| Warhead Yield | 200-300 KT |
| CEP (meters) | 300-400 |
| CEP (meters) | |