Near-Rectilinear Halo Orbit Analysis for the Artemis Lunar Gateway Mission

Zenodo (CERN European Organization for Nuclear Research) 2026 Open access

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Authors: Ginevra Cianci
DOI: 10.5281/zenodo.18454887
Cited by: 0

Abstract

Technical analysis of NRHO trajectories for NASA's Artemis Lunar Gateway station using NASA GMAT. Demonstrates orbital characteristics, stability analysis, and mission design for cislunar infrastructure.

Fields of Study & Subjects

Spacecraft Dynamics and Control Space Satellite Systems and Control Spacecraft Design and Technology

Publication details

Journal / source
Zenodo (CERN European Organization for Nuclear Research)
Publication date
2 February 2026
Language
EN