Paper
11 November 2002 Characterization of space environmental effects on candidate solar sail material
David L. Edwards, Whitney Hubbs, Tesia Stanaland, Andrew Hollerman, Richard L. Altstatt
Author Affiliations +
Abstract
The National Aeronautics and Space Administration's (NASA) Marshall Space Flight Center (MSFC) is concentrating research into the utilization of photonic materials for spacecraft propulsion. Spacecraft propulsion, using photonic materials, will be achieved using a solar sail. A sail operates on the principle that photons, originating from the sun, impart pressure and provide a source of spacecraft propulsion. The pressure can be increased, by a factor of two if the sun-facing surface is perfectly reflective. Solar sails are generally composed of a highly reflective metallic front layer, a thin polymeric substrate, and occasionally a highly emissive back surface. The Space Environmental Effects Team at MSFC is actively characterizing candidate solar sail materials to evaluate the thermo-optical and mechanical properties after exposure to a simulated Geosynchronous Transfer Orbit (GTO) radiation environment. This study is the first known characterization of solar sail materials exposed to space simulated environments. The technique of radiation dose verses material depth profiling was used to determine the orbital equivalent exposure doses. The solar sail exposure procedures and results of the material characterization will be discussed.
© (2002) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
David L. Edwards, Whitney Hubbs, Tesia Stanaland, Andrew Hollerman, and Richard L. Altstatt "Characterization of space environmental effects on candidate solar sail material", Proc. SPIE 4823, Photonics for Space Environments VIII, (11 November 2002); https://doi.org/10.1117/12.451455
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Cited by 14 scholarly publications.
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KEYWORDS
Solar sails

Photons

Space operations

Sun

Reflectivity

Aluminum

Chromium

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