Work

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

Year: 2026

Type: article

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.

Source: Zenodo (CERN European Organization for Nuclear Research)

DOI: 10.5281/zenodo.18454887

Author: Cianci, Ginevra

Institution: Politecnico di Torino

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

OpenAlex ID: W7127187368

FWCI:

Cites:

Cited by:

Related to: