Description
The LM-3A launch vehicle represents a significant advancement in space technology, tracing its roots back to the 1980s. Leveraging the proven capabilities of the LM-3 and other Long March launch vehicles, the LM-3A made its successful debut in February 1994. This 3-stage launch vehicle is engineered for precision and reliability, primarily designed for launching spacecraft into Geostationary Transfer Orbit (GTO). The innovative cryogenic third stage utilizes liquid hydrogen and liquid oxygen, enhancing its efficiency and performance. With a robust launch capability of up to 2,600 kg for GTO missions, the LM-3A is a formidable asset in the field of aerospace exploration.
Specifications
| Attribute | Details |
|---|---|
| Stages | 3 |
| Propellant | Cryogenic (Liquid Hydrogen and Liquid Oxygen) |
| Launch Capability (GTO) | 2,600 kg |
| Fairing Diameter | 3 m |
| First Flight | February 1994 |
Additional Information
The LM-3A showcases a blend of historical significance and cutting-edge technology, making it a key player in modern space missions. Its design is rooted in decades of experience, ensuring reliability and successful launches.
