Three-Impulse Transfer

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

A transfer scheme applying three impulses sequentially at departure, perilune, and orbit insertion for LEO-to-DRO powered lunar flyby transfers. The departure impulse is provided by the launch vehicle; perilune and insertion impulses are carried by the spacecraft.

Related Concepts

• Orbital Transfer Stage
• Low-Energy Earth-Moon Transfer

References

• 魏赞等2026北航学报
• Vepa - 2024 - Space vehicle maneuvering, propulsion, dynamics and control