Design, Assessment, and Calibration of the Moon-Aiming Thai-Chinese Hodoscope for Observing Cosmic Ray Electrons, Solar Energetic Particles, and Lunar Albedo Ions
3
Issued Date
2025-12-30
Resource Type
eISSN
18248039
Scopus ID
2-s2.0-105029010865
Journal Title
Proceedings of Science
Volume
501
Rights Holder(s)
SCOPUS
Bibliographic Citation
Proceedings of Science Vol.501 (2025)
Suggested Citation
Puprasit K., Chaiwongkhot K., Amratisha K., Lakronwat J., Mitthumsiri W., Pattarakijwanich P., Ruffolo D., Torteeka P., Burom S., Panyalert T., Charoenvicha P., Jamlongkul P., Khonsri P., Manuthasna S., Marsri T., Pittayang Y., Zhang N., Zhang S., Zhao H., He X. Design, Assessment, and Calibration of the Moon-Aiming Thai-Chinese Hodoscope for Observing Cosmic Ray Electrons, Solar Energetic Particles, and Lunar Albedo Ions. Proceedings of Science Vol.501 (2025). doi:10.22323/1.501.1357 Retrieved from: https://repository.li.mahidol.ac.th/handle/123456789/114900
Title
Design, Assessment, and Calibration of the Moon-Aiming Thai-Chinese Hodoscope for Observing Cosmic Ray Electrons, Solar Energetic Particles, and Lunar Albedo Ions
Corresponding Author(s)
Other Contributor(s)
Abstract
The Moon-Aiming Thai-Chinese Hodoscope (MATCH) is designed as a space weather payload for the Chang’E-7 lunar orbiter, aimed at enhancing space weather monitoring in the Earth-Moon region and measuring lunar albedo ions up to approximately 100 MeV/n. Additionally, it will provide continuous measurements of cosmic ray electrons up to around 120 MeV/n, thereby clarifying the contributions from Jovian and Galactic sources. Furthermore, Jovian electrons, together with solar energetic particles (SEPs) to a certain degree, constitute particles from a recognized source that can be utilized to investigate the effects of Earth’s magnetotail during a segment of the Moon’s orbit around Earth. The engineering challenges for Thailand’s nascent space program include integrated sensor design and fabrication, mechanical design, readout electronics with high resolution and sensitivity yet low power consumption and ensuring seamless integration with and safe operation of the Chang’E-7 orbiter spacecraft itself. This presentation will include the scientific objectives and technical design of the payload, validation via GEANT4 simulations of geometrical acceptance and angular resolution, along with the results from the detector payload’s calibrations using standard radiation testing in a space environment control chamber. The expected detection range will also be confirmed.