Team 05: A Thermal Analysis of a 6U CubeSat
Abstract
With no convection, orbital spacecraft temperatures can reach extreme highs and lows. The stability ofcraft temperature is critical forcontinued hardware functionality. Creation of a thermal model allowed for the examination of temperature stability from the environment and surface coating choice. Lab tests confirmed the efficacy of using a mylar-based insulation, along with including a thermal control system, to achieve temperature stability.
Sponsorship
UCAR
Director
Scott Sewell
Team Members
- Connie Childs
- Nick Zarilla