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.
Collura, A., Barbera, M., Varisco, S., Basso, S., Pareschi, G., Tagliaferri, G., et al. (2009). Simbol-X Mirror Module Thermal Shields: I-Design and X-Ray Transmission. In AIP Conference Proceedings, Volume 1126, pp. 44-47 (2009) (pp.44-47) [10.1063/1.3149461].
Simbol-X Mirror Module Thermal Shields: I-Design and X-Ray Transmission
BARBERA, Marco;
2009-01-01
Abstract
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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