Title: Timepix in LEO orbit onboard the VZLUSAT-1 nanosatellite: 1-year of space radiation dosimetry measurements
Authors: Báča, Tomáš
Jílek, Miroslav
Veřtát, Ivo
Urban, Martin
Nentvich, Ondřej
Filgas, Robert
Granja, Carlos
Inneman, Adolf
Daniel, Vladimír
Citation: BÁČA, T., JÍLEK, M., VEŘTÁT, I., URBAN, M., NENTVICH, O., FILGAS, R., GRANJA, C., INNEMAN, A., DANIEL, V. Timepix in LEO orbit onboard the VZLUSAT-1 nanosatellite: 1-year of space radiation dosimetry measurements. Journal of Instrumentation, 2018, roč. 13, č. November, s. 0-8. ISSN 1748-0221.
Issue Date: 2018
Document type: článek
URI: 2-s2.0-85057612019
ISSN: 1748-0221
Keywords in different language: on-board space electronics;particle detectors;space instrumentation;X-ray detectors and telescopes
Abstract in different language: The VZLUSAT-1 satellite, the first Czech CubeSat, was successfully launched on June 23, 2017, to a 510 km Sun-synchronous low-Earth orbit. It carries several scientific payloads including a Timepix detector as focal plane imager for the X-Ray telescope onboard. The Timepix detector contributes significantly to the satellite data collection, with more than 25 000 sampling acquisitions in the first year of deployment. Despite limitations of the satellite attitude control system, necessary for capturing X-Ray images of the Sun, the Timepix detector allows measuring the space radiation environment along the satellite orbit. As of September 2018, we conducted 33 whole-Earth mappings, recording radiation doses around the planet. Further, we show data from scans of the South Atlantic Anomaly and polar radiation horns, where the location and acquisition time were tailored to minimize event pile-up and particle track overlap. Since October 2017, the optics segment of the onboard X-Ray telescope was deployed, which exposed the Timepix detector unshielded to free open space. This change produced entirely new observations namely of low energy charged particles and a significant increase of measured particle flux. We also registered the effects of exposing the sensor to direct intense sunlight. We will summarize on the actual performance of the custom readout interface, which exceeds expectations in the constrained environment of the low-cost and low-powered CubeSat nanosatellite.
Rights: Plný text je přístupný v rámci univerzity přihlášeným uživatelům.
© IOP Publishing
Appears in Collections:Články / Articles (KAE)

Files in This Item:
File SizeFormat 
Vertat_JINST.pdf5,03 MBAdobe PDFView/Open    Request a copy

Please use this identifier to cite or link to this item: http://hdl.handle.net/11025/33698

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.

  1. DSpace at University of West Bohemia
  2. Publikační činnost / Publications
  3. OBD