MATERIAL ANSWERS, LLC — National Aeronautics and Space Administration SBIR Phase I: H8

Description

The proposed work will develop lightweight multifunctional composites based on novel continuous fiber reinforced fluorinated polybenzoxazine (FPBZ) resin with an ultra-high nanofiller concentration nanocomposite coating.nbsp; The composites are designed to provide exceptional atomic oxygen erosion resistance as well as thermal stability and structural performance. Atomic oxygen erosion resistance will be provided primarily through the application of a nacre-memetic coating comprised of layered silicate.nbsp; This approach provides a path towards addressing the need for a lightweight alternative to aluminum in low earth orbit (LEO) applications such as satellites and orbiting spacecraft.nbsp; FPBZrsquo;s can be processed using liquid resin molding techniques such as lay-up, compression molding, and autoclaving.nbsp; Thus, polymers and composites developed during this project are expected to provide a unique combination of properties and processing characteristics to meet the needs of NASA and the rapidly expanding commercial space market.nbsp;Ground-based testing and modeling tasks will be utilized during Phase I to provide a preliminary assessment of atomic oxygen resistance; ultimately leading to testing aboard the International Space Station (ISS) during Phase II using the MISSE-FF (Materials International Space Station Experiment ndash; Flight Facility).