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Virginia Tech

A Low-Lunar Orbit CubeSat Solution to Mission-Oriented Lunar Surface Imagery Requirements

Abstract

dc:description.abstract

For spaceflight activities in Earth orbit or in Earth's atmosphere, such as on-orbit operations, flight tests, launches, and landings, remote-sensing optical-infrared assets can be used to monitor and document mission performance. These observations can be made using assets in the diverse orbital, airborne, and ground-based infrastructure built up for operations on or near Earth. Public and private sector entities from various countries are formulating plans and developing architectures for missions on and near the lunar surface, which are forecast to proliferate in the coming years. The paradigm for lunar imaging assets has historically been limited to standalone, expensive projects such as the Lunar Reconnaissance Orbiter (LRO) or its planned follow on, the Lunar Exploration and Science Orbiter (LExSO). Aside from the expense involved in developing, deploying, and operating such assets, they are inherently limited as singular platforms. This work proposes a low-lunar-orbit, CubeSat-based solution to mission-oriented remote sensing for activities on and near the lunar surface, on the basis that CubeSats can be developed and deployed in greater numbers and involve less expense than their larger counterparts. Analysis in this work includes an exploration of orbital stability and an assessment of suitability for imagery objectives. The data discussed herein include a summary of the results of 3,420 individual circular orbital initial configurations in the low-lunar-orbit regime. Each orbit's data set is the result of a high-fidelity simulation including high-resolution lunar gravitational models. Results explored include a discussion of orbital longevity and parametric stability, suitability for imagery objectives, and assessment of surface imagery coverage from spatial and temporal perspectives.

Degree

thesis:*
Name thesis:degree_name
Master of Science
Level thesis:degree_level
masters
Discipline thesis:degree_discipline
Aerospace Engineering
Department dc:contributor.department
Aerospace and Ocean Engineering
Grantor dc:publisher
Virginia Tech
Year dc:date.issued
2025

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • McCleary, Meaghan Leigh
Chair dc:contributor.committeechair
  • Kenyon, Samantha Parry
Committee members dc:contributor.committeemember
  • England, Scott Leslie
  • Inman, Jennifer A.

Subjects

dc:subject × 3

Rights

dc:rights
Statement dc:rights
  • In Copyright
Language dc:language.iso
en

Identifiers

dc:identifier.*
Dc Identifier Other
vt_gsexam:43446
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/134251

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

McCleary, Meaghan Leigh. A Low-Lunar Orbit CubeSat Solution to Mission-Oriented Lunar Surface Imagery Requirements. masters thesis, Virginia Tech, 2025. https://hdl.handle.net/10919/134251