In-Orbit Performance of the Cooling Systems for the X-Ray Instruments on XMM-NEWTON

2003-01-2640

07/07/2003

Event
International Conference On Environmental Systems
Authors Abstract
Content
The ESA mission XMM-Newton was launched on 10 December 1999. The payload includes five cooled Charge Coupled Device (CCD) cameras. To allow for single photon detection, the detectors are operated between −60 and −130 degree C. These temperatures are achieved through passive cooling. It is required to warm up to room temperature for decontaminating the camera heads and even to heat the detectors to +130 degree C to anneal the CCDs. Additional constraints relate to the high mechanical stability and shielding mass required around the CCDs. All X-ray instruments feature a nested detector housing and multistage passive radiators. The in-orbit thermal characteristics are compared to the corresponding instrument models for selected periods
Meta TagsDetails
DOI
https://doi.org/10.4271/2003-01-2640
Pages
10
Citation
Thomsen, K., Mapson-Menard, H., Fauste, J., Djavidnia, S. et al., "In-Orbit Performance of the Cooling Systems for the X-Ray Instruments on XMM-NEWTON," SAE Technical Paper 2003-01-2640, 2003, https://doi.org/10.4271/2003-01-2640.
Additional Details
Publisher
Published
Jul 7, 2003
Product Code
2003-01-2640
Content Type
Technical Paper
Language
English