What is it about?

We show the trajectory design method transferring from the Earh-moon NRHO to halo orbits around the sun-Earth L1 and L2 points, with example results and discussion.

Featured Image

Read the Original

This page is a summary of: Transfer from Lunar Gateway to Sun-Earth Halo Orbits Using Solar Sails, Journal of Spacecraft and Rockets, September 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35559.
You can read the full text:

Read

Contributors

Be the first to contribute to this page