From Earth Escape to Lunar Touchdown: A Simulated Lunar Lander Mission
Year: 2025
Type: article
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.
Source: Acceleron Aerospace Journal
Author: Syleen Edwards
Institution: Collins Aerospace (United States)
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: diamond
OpenAlex ID: W4408160602