From Earth Escape to Lunar Touchdown: A Simulated Lunar Lander Mission

Authors

  • Syleen Edwards Systems Engineer at Collins Aerospace, Former Spaceflight Mechanics intern at STAR

DOI:

https://doi.org/10.61359/11.2106-2508

Keywords:

Spaceflight, Orbital Mechanics, GMAT, Lunar Exploration, Prototyping, Conceptual Design, Design Thinking, Trajectory Prediction, Orbits, Spacecraft Operation

Abstract

This report investigates the application of design thinking principles to optimize the trajectory and operations of a lunar lander. By considering the spacecraft as the "user" within the design thinking framework, we aim to identify and address critical challenges during key mission phases: Earth Escape, Orbital Insertion, Lunar Transfer Trajectory Injection, and Powered Descent & Lunar Landing. Leveraging the General Mission Analysis Tool (GMAT), we translate design thinking solutions into testable virtual prototypes, allowing for iterative refinement and optimization of the mission plan. This approach prioritizes efficiency and functionality, ultimately paving the way for more cost-effective and successful lunar exploration endeavors.

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Published

2025-02-28

How to Cite

Edwards, S. (2025). From Earth Escape to Lunar Touchdown: A Simulated Lunar Lander Mission. Acceleron Aerospace Journal, 4(2), 886–910. https://doi.org/10.61359/11.2106-2508

Issue

Vol. 4 No. 2 (2025): Acceleron Aerospace Journal (AAJ), Volume 4, Issue 2, 2025

Section

Articles

Categories

License

Copyright (c) 2025 Acceleron Aerospace Journal

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This work is licensed under a Creative Commons Attribution 4.0 International License.

The Acceleron Aerospace Journal, with ISSN 2583-9942, uses the CC BY 4.0 International License. You're free to share and adapt its content, as long as you provide proper attribution to the original work.