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Simbol-X Mirror Module Thermal Shields: I-Design and X-Ray Transmission

2009

The Simbol‐X mission is designed to fly in formation flight configuration. As a consequence, the telescope has both ends open to space, and thermal shielding at telescope entrance and exit is required to maintain temperature uniformity throughout the mirrors. Both mesh and meshless solutions are presently under study for the shields. We discuss the design and the X‐ray transmission.

Physicsbusiness.industryAstrophysics::High Energy Astrophysical PhenomenaAstrophysics::Instrumentation and Methods for AstrophysicsShieldsX- and gamma-ray telescopes and instrumentation Astronomical and space-research instrumentation Optical coatingsParticle detectorlaw.inventionTelescopeOpticsOptical coatingSettore FIS/05 - Astronomia E AstrofisicaTransmission (telecommunications)lawElectromagnetic shieldingThermalMeasuring instrumentbusiness
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