Article

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

Ginevra CianciPolytechnic University of Turin

Zenodo (CERN European Organization for Nuclear Research)repository2026en

ABI

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.

Topics

Spacecraft Dynamics and Control Space Satellite Systems and Control Astro and Planetary Science

Identifiers

DOI: 10.5281/zenodo.18454888

Citations and references

Cited by 00 references

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