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) |