LM-3A Orbital Launch Vehicle
The LM-3A launch vehicle was developed starting in the 1980s, building on proven technology. It successfully performed its maiden flight in February 1994.
Technical Specifications
Overview
LM-3A Orbital Launch Vehicle
The LM-3A is a sophisticated 3-stage orbital launch vehicle designed to deliver payloads into Geostationary Transfer Orbit (GTO). Developed with flight-proven heritage technology, it represents a reliable solution for spacecraft deployment. Its third stage utilizes high-efficiency cryogenic propellants, specifically liquid hydrogen and liquid oxygen, to ensure optimal performance during mission execution.
Technical Specifications
GTO Payload Capacity
2,600 kg
GTO Mission Capability
- Number of Stages
- 3
- Fairing Static Envelope Diameter
- 3 m
Propulsion
- Third Stage Propellants
- Liquid HydrogenLiquid Oxygen
Mission Profile
- Primary Mission Type
- GTO (Geostationary Transfer Orbit)
History
- Maiden Flight Date
- February 1994
