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February 5, 2026Open Access

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

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Authors

GCGinevra Cianci

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Overview

Technical analysis reveals orbital characteristics and stability for cislunar infrastructure in the Artemis mission.

Key Points

  • Analyze near-rectilinear halo orbit trajectories for the Artemis Lunar Gateway mission.
  • Utilized NASA GMAT for trajectory analysis
  • Conducted stability analysis of NRHO
  • Assessed mission design parameters for the lunar gateway
  • Identified key orbital characteristics of NRHO
  • Demonstrated stability for proposed trajectories
  • Outlined mission design factors essential for cislunar operations

Cite This Study

Ginevra Cianci (2026) studied this question.

synapsesocial.com/papers/698434dff1d9ada3c1fb3849https://doi.org/10.5281/zenodo.18454888
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