Faraday Technology, Inc. — National Aeronautics and Space Administration SBIR Phase I: S5

Faraday Technology, Inc. — SBIR Phase I award from National Aeronautics and Space Administration.

Amount
$124,997
Agency
National Aeronautics and Space Administration
Program / Phase
SBIR · Phase I
Topic
S5
Solicitation
SBIR_20_P1
NAICS
Place of performance
OH
Period
2020-08-27 → 2021-03-01

Description

This program will address the stated need from the National Space Weather Strategy and Action plan to ldquo;enhance the Protection of National Security, Homeland Security, and Commercial Assets and Operations against the Effects of Space Weatherrdquo;. Specifically, we will develop and demonstrate an ion erosion resistant passive high emissivity coating that mitigates charging and erosion effects brought on by ionizing radiation. Ionizing radiation occurs as a result of space weather events like solar flares or cosmic rays and has the potential to incur cascading spacecraft damage that could lead to loss of key services such as communications, national security, remote sensing, and environmental monitoring. In Phase I we will develop a scalable electrophoretic deposition approach to apply tunable erosion resistant and highly emissive passive coatings consisting of mixtures of low work function ceramics and hard/conductive boron doped diamond materials. Both electrophoretic deposition cell and process parameters will be optimized to obtain the desired performance. The coating development activities will be guided by an evaluation of the electron-emitting properties of the coating before and after Xenon ion sputtering, across a broad range of energies, and identify first and second crossover energies, maximum yields, and energies of maximum yields. Finally, we will estimate the feasibility of transitioning this technology to pertinent spacecraft components of interest to NASA and our Phase II commercialization partners. In Phase II, Faraday, USU, and commercial partners will apply the optimized coatings to testable components and expose them to simulated launch conditions, space weather, ionospheric charging, and ion sputtering erosion. If successful we envision these materials could then be applied to platforms used within Materials International Space Station Experiment (MISSE) for further qualification, optimization, and validation within Phase III.