Paper
23 May 2011 Carbon/Carbon for satellite applications
M. Meftah, S. Lee, A. Irbah, S. Ostergren
Author Affiliations +
Abstract
Carbon/Carbon has many attributes that make it an attractive material for satellite applications. It is low in density, is dimensionally stable under a wide variety of conditions, has very low thermal expansion, is relatively low in cost, and is a mature technology. Moreover, the material is flexible enough to enable the designer to select such variables as fiber type, fabric architecture, fiber volume, and high temperature processing and thus custom tailor the physical and mechanical properties to his specific requirements. A wide range of properties are available - densities from 1.5 to 1.9 g/cm3, room temperature Coefficients of Thermal Expansion (CTE) from -0.3x10-6to -1.3x10-6/K, room temperature thermal conductivities from 7 to 210 W/m.K, and modulus from 60 to 190 GPa. A new type of structure developed by CNRS on the space instrument SODISM uses Carbon/Carbon.
© (2011) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
M. Meftah, S. Lee, A. Irbah, and S. Ostergren "Carbon/Carbon for satellite applications", Proc. SPIE 8044, Sensors and Systems for Space Applications IV, 80440Y (23 May 2011); https://doi.org/10.1117/12.878952
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CITATIONS
Cited by 6 scholarly publications.
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KEYWORDS
Space telescopes

Telescopes

Satellites

Sun

Composites

Mirrors

Carbon

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