TMI is currently studying the possibility of combining the role of solar/cosmic radiation shielding and thermal insulation for use in a vacuum and low pressure gas environment. The development of this innovation is intended for use in the design of lunar and martian habitation structures. Combining the roles of thermal insulation and radiation shielding will reduce the complexity of any habitable structure developed for future space exploration.  Having an insulation that can operate in both vacuum and low pressure gas environments will allow a single design for both lunar and Mars exploration structures. However, the successful development of this technology may lead to uses in other areas. Sensitive electronics aboard communications and research satellites have shown vulnerability to Solar Particle Event’s. The addition of radiation shielding combined with thermal insulation will increase the reliability and longevity of satellites while maintaining mass limitations. Additionally, airline crews operating at high altitudes are exposed to potentially harmful levels of cosmic radiation. Incorporating even the smallest amount of radiation shielding materials in the aircraft insulation may significantly reduce the cumulative exposure that is experienced over long term operations.

Space Programs
POC: Mala Thompson • 256.721.6672