Advanced materials with large and dynamic variation in thermal properties, sought for urgent defense and space applications, have heretofore been elusive. Conducting polymers (CPs) have shown some intrinsic variation of mid‐ to far‐infrared (IR) signature in this respect, but the practical utilization of this has remained elusive. We report herein the first significant IR electrochromism in any material, to our knowledge, in the 0.4 through 45 μm region. This is seen in practical CP devices in the form of thin (<0.5 mm), flexible, entirely solid‐state, variable area (1 cm2 to 1 m2) flat panels. Typical properties include: very high reflectance variation; switching times <2 s; cyclabilities of 105 cycles; emittance variation from 0.32 to 0.79; solar absorptance variation from 0.39 to 0.79; operating temperatures of –35 to +85 °C; durability against γ‐radiation to 7.6 Mrad, vacuum to 10–6 torr, and simulated solar wind (e.g., 6.5 × 1016 e/cm2 @ 10 keV).

Technology development is inevitably a dynamic process in search of an elusive goal. It is never truly clear whether the need for a particular technology drives its development, or the existence of a new capability initiates new applications. Technology development for the thermal control of spacecraft presents an excellent example of this situation.Nevertheless, it is imperative to have a basic plan to help guide and focus such an effort.Although this plan will be a living document that changes with time to reflect technological developments, perceived needs, perceived opportunities, and the everchanging funding environment, it is still a very useful tool. This presentation summarizes the current efforts at NASNGoddard and NASNJPL to develop new thermal control technology for future robotic NASA missions.Kev Words: advanced thermal control, capillary pumped loops, loop heat pipes, variable emissivity surface, cryogenic, heat switches, thermal storage

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