Thermal Modeling & Analysis
Summer 2026
During Summer 2026, I led a four-member team advancing the thermal design of Rutgers’ SPICEsat CubeSat fluid payload. Our work focused on selecting a space-compatible working fluid, evaluating heater configurations, and improving the spacecraft’s Thermal Desktop model. We compared candidate fluids across thermal, safety, compatibility, and integration criteria, then used MATLAB and orbital simulations to evaluate temperature behavior under hot and cold-case conditions. The project strengthened the mission’s thermal-control strategy and supported preparation for Critical Design Review.
Slide 1: ISS orbit cold case temperature contour
Slide 2: ISS orbit cold case plot of satellite temperature over time
Slide 3: ISS orbit hot case temperature contour
Slide 4: ISS orbit hot case plot of satellite temperature over time
Slide 5: 10 W Thermal Desktop case set run after model correlation