Two-Stage Orbital Launch Vehicle
This two-stage rocket is designed for launching satellites into low Earth orbit (LEO) and sun-synchronous orbit (SSO). It features a payload fairing of 3350mm in diameter and attitude control engine.
Technical Specifications
Product Overview
Orbital Launch Capability
This two-stage orbital launch vehicle is designed for high reliability and mature operational performance. Optimized for deployment into Low Earth Orbit (LEO) and Sun-Synchronous Orbit (SSO), it features advanced capabilities including attitude control and precise propellant management. Since its development, the system has been refined to meet the evolving demands of satellite deployment.
Technical Specifications
Development History
| Year | Milestone |
|---|---|
| 1990 | Development Initiated |
| 2002 | SSO capability and fairing upgrade |
- Stages
- 2
- Payload Fairing Diameter
- 3350 mm
Operational Capabilities
Primary Launch Sites
- Jiuquan Satellite Launch Center
- Other domestic satellite launch centers
- Target Orbits
- LEOSSO
Key Features
Performance Highlights
High ReliabilityMature TechnologyWide ApplicationAttitude ControlDe-orbit Capability
