North Logan, Utah – March 2, 2015 - TMT has successfully demonstrated a 1000 watt - 1.0 m x 2.5 m (39.4 in. x 98.4 in.) near isothermal multi-functional spacecraft structural-thermal panel. Funded by the Air Force Research Laboratory Space Vehicles Directorate, through a prime contract to LoadPath, TMT was tasked to demonstrate the viability of extending the multi-functional isothermal panel technology developed for Operational Responsive Space (ORS) isothermal spacecraft to