T. Bumbary
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Summer 2020NASA JPL

Summer Researcher

Lunar regolith thermal modeling

Thermal FEA of cryogenic instruments to measure lunar regolith conductivity.

01 / Project notes

Context

At NASA JPL’s Applied Low Temperature Physics Group, Turner modeled cryogenic instruments designed to measure the thermal conductivity of lunar regolith.

02 / Project notes

Problem

Lunar regolith thermal conductivity is relevant to polar ice stability, internal heating, and future habitation.

03 / Project notes

My role

Turner modeled and simulated cryogenic instruments using thermal finite-element analysis.

04 / Project notes

Approach

Thermal finite-element analysis in ANSYS and SolidWorks supported the modeling and simulation of the cryogenic instruments.

05 / Project notes

Tools

ANSYS · SolidWorks · Thermal finite-element analysis

06 / Project notes

Results

Turner presented this research at the Caltech research symposium.