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

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

May 2009

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2009aipc.1126...44c&link_type=abstract

SIMBOL-X: FOCUSING ON THE HARD X-RAY UNIVERSE: Proceedings of the 2nd International Simbol-X Symposium. AIP Conference Proceedi

Astronomy and Astrophysics

Astronomy

X- And Gamma-Ray Telescopes And Instrumentation, Astronomical And Space-Research Instrumentation, Optical Coatings

Scientific paper

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.

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