Masters Theses
Keywords and Phrases
characterization; experiment; photovoltaics; simulation
Abstract
This research delves into the design, implementation, and analysis of a controlled experimental framework for photovoltaic cell characterization and its application in spacecraft power systems. Such a system was simulated and validated by benchmarking characteristics of a photovoltaic module and implementing them in a system design simulation yielding performance data for comparative analysis. A hardware setup was developed to perform IV characterization tests under steady state thermal conditions. Experiments conducted across various thermal regulation profiles helped quantify the effects of temperature on the photovoltaic performance parameters. Active cooling reduced the steady state cell temperature by 17.9% and improved the cell output efficiency 8.3%. The IV characteristics are used in the spacecraft power budget for defining the power generation in the experiment. The spacecraft power system is simulated using relevant hardware components, operating real time mission modes under varying load configurations. Comparative analysis between theoretical power budget and experimental results shows systematic and conversion losses. This highlighted the significance of realistic power flow modeling in the system design experiment. This study establishes a reproducible methodology for bridging static photovoltaic characterization with dynamic spacecraft power system validation.
Advisor(s)
Pernicka, Henry J.
Committee Member(s)
Stutts, Daniel S.
Anklesaria, Yezad H.
Department(s)
Mechanical and Aerospace Engineering
Degree Name
M.S. in Aerospace Engineering
Publisher
Missouri University of Science and Technology
Publication Date
Fall 2025
Pagination
ix, 83 pages
Note about bibliography
Includes_bibliographical_references_(pages 80-82)
Rights
© 2026 Jay Bakulkumar Kamdar , All Rights Reserved
Document Type
Thesis - Open Access
File Type
text
Language
English
Thesis Number
T 12569
Recommended Citation
Kamdar, Jay Bakulkumar, "Design of a Spacecraft Power System Experiment" (2025). Masters Theses. 8267.
https://scholarsmine.mst.edu/masters_theses/8267
