Harnessing Deep-Space Thermal Gradients to Power Orbital Spacecrafts With the Use of Thermoelectric Effects

Faculty Mentor

Dr. Valentin Soloiu

Location

Russell Union Ballroom

Type of Research

On-going

Session Format

Poster Presentation

College

Allen E. Paulson College of Engineering & Computing

Department

Mechanical Engineering

Abstract

Orbital power generation faces a great challenge in maintaining electrical networks remotely, with photovoltaic panels having a short lifespan and high maintenance. Thermoelectric generators(TEGs) offer a strong alternative, using extreme temperature gradients between sunlit and shadowed surfaces in deep-space. Utilizing thermoelectric effects will provide constant, reliable energy for the spacecraft, without the expensive ten-year cycles required for solar panels. This apparatus is a TEG utilizing the Seebeck effect, where a temperature gradient between two junctions generates an electric voltage. I hypothesized that as the temperature gradient increases, within the region of 20°C-110°C, the amount of energy produced will increase, up to 5mV. I measured the electric voltage, the platinum resistance, and the thermistor. The results that I obtained confirmed a positive linear relationship between temperature difference and voltage, affirming my hypothesis. I also obtained a direct relationship between the platinum resistance and temperature and an inverse relationship between thermistor and temperature.

Program Description

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Start Date

4-23-2026 10:00 AM

End Date

4-23-2026 12:00 PM

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Apr 23rd, 10:00 AM Apr 23rd, 12:00 PM

Harnessing Deep-Space Thermal Gradients to Power Orbital Spacecrafts With the Use of Thermoelectric Effects

Russell Union Ballroom

Orbital power generation faces a great challenge in maintaining electrical networks remotely, with photovoltaic panels having a short lifespan and high maintenance. Thermoelectric generators(TEGs) offer a strong alternative, using extreme temperature gradients between sunlit and shadowed surfaces in deep-space. Utilizing thermoelectric effects will provide constant, reliable energy for the spacecraft, without the expensive ten-year cycles required for solar panels. This apparatus is a TEG utilizing the Seebeck effect, where a temperature gradient between two junctions generates an electric voltage. I hypothesized that as the temperature gradient increases, within the region of 20°C-110°C, the amount of energy produced will increase, up to 5mV. I measured the electric voltage, the platinum resistance, and the thermistor. The results that I obtained confirmed a positive linear relationship between temperature difference and voltage, affirming my hypothesis. I also obtained a direct relationship between the platinum resistance and temperature and an inverse relationship between thermistor and temperature.