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

Project Links