Date of Award

Spring 2011

Document Type

Thesis

Degree Name

Master of Science (MS)

Department

Mechanical & Aerospace Engineering

Program/Concentration

Aerospace Engineering

Committee Director

Robert L. Ash

Committee Member

Brett Newman

Committee Member

Colin P. Britcher

Call Number for Print

Special Collections; LD4331.E535 D355 2011

Abstract

This thesis studies the feasibility of incorporating a large autonomously deployed photovoltaic solar array power system as the primary power source for a large fixed Mars base. A mission duration of 10 Earth years has been assumed and the nominal power demands have been specified as a minimum of 40 kW, during daytime operation and a continuous 10 kW. demand for nighttime operation.

The overall system design developed in this thesis has an estimated total mass of 7,400 kg, when utilizing hydrogenated amorphous silicon thin film solar arrays and an estimated total mass of 5,100 kg when utilizing polycrystalline copper-indium-diselenide CIGS solar cells. Because the technology readiness level required to deploy the CIGS cells has not yet been achieved, both options have been included. Energy storage using a proton exchange membrane regenerative fuel cell system has been recommended for both solar array types.

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DOI

10.25777/2y2m-yh06

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