Example of reflectance data generated for a PSB silicate white paint from France.
The components and materials of spacecraft in low Earth orbit can degrade in thermal and optical performance through interaction with atomic oxygen and vacuum ultraviolet (VUV) radiation, which are predominant in low Earth orbit. Because of the importance of low Earth orbit durability and performance to manufacturers and users, an international test program for assessing the durability of spacecraft materials and components was initiated. Initial tests at the NASA Glenn Research Center consisted of exposure of samples representing a variety of thermal control paints, multilayer insulation materials, and Sun sensors that have been used in space. Materials donated from various international sources were tested alongside materials whose performance is well known, such as Teflon FEP, Kapton H, or Z-93-P white paint. The optical, thermal, or mass loss data generated during the tests were then provided to the participating material suppliers. Data were not published unless the participant donating the material consented to publication. The test program is intended to give spacecraft builders and users a better understanding of degradation processes and effects so that they can improve their predictions of spacecraft performance.
Find out more from Glenn's Electro-Physics Branch
Glenn contacts: Sharon K. Miller, 216-433-2219, Sharon.K.Miller@grc.nasa.gov; Bruce A. Banks, 216-433-2308, mailto:Bruce.A.Banks@grc.nasa.gov; and Joyce A. Dever, 216-433-6294, Joyce.A.Dever@grc.nasa.gov
Author: Sharon K. Miller
Headquarters program office: OAT
Programs/Projects: ISS, other low-Earth-orbit satellites
Last updated June 13, 2001, by Nancy.L.Obryan@nasa.gov
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