Solar X-ray Spectrometer (Soxs) Mission on Board GSAT2 Indian Spacecraft: The Low-Energy Payload
| Autor: | Chirag M. Solanki, K. S. B. Manian, Jayshree J. Trivedi, V. D. Patel, Sumit Kumar, Vishal Shah, N. M. Vadher, M. R. Deshpande, Amish B. Shah, Rajmal Jain, Girish P. Ubale, Hemant Dave, K. J. Shah, S. L. Kayasth |
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| Rok vydání: | 2005 |
| Předmět: |
Physics
Solar flare Spacecraft Spectrometer Physics::Instrumentation and Detectors business.industry Payload Astrophysics::High Energy Astrophysical Phenomena Detector Astrophysics::Instrumentation and Methods for Astrophysics Astronomy and Astrophysics SOXS Optics Space and Planetary Science Geostationary orbit Astrophysics::Solar and Stellar Astrophysics High Energy Physics::Experiment business Space research |
| Zdroj: | Solar Physics. 227:89-122 |
| ISSN: | 1573-093X 0038-0938 |
| DOI: | 10.1007/s11207-005-1712-3 |
| Popis: | The first space-borne solar astronomy experiment of India, namely “Solar X-ray Spectrometer (SOXS)”, was successfully launched on 08 May 2003 on board geostationary satellite GSAT-2 of India. The SOXS is composed of two independent payloads, viz. SOXS Low-Energy Detector (SLD) Payload and SOXS High-Energy Detector (SHD) Payload. The SOXS aims to study the full-disk integrated X-ray emission in the energy range from 4 keV to 10 MeV. In this paper we present the first report on the SLD instrumentation and its in-orbit performance. The SLD payload was designed and developed at the Physical Research Laboratory in collaboration with various centers of Indian Space Research Organisation (ISRO). The basic scientific aim of the SLD payload is to study solar flares in the energy range from 4 to 60 keV with high spectral and temporal resolution. To meet these requirements, the SLD payload employs state-of-the-art solid state detectors, the first time for a solar astronomy experiment, viz. Si PIN (4 –25 keV), and cadmium–zinc–telluride (4 –60 keV). With their superb high-energy resolution characteristics, SLD can observe iron and iron–nickel complex lines that are visible only during solar flares. In view of its 3.4∘ FOV, the detector package is mounted on a Sun Aspect System, for the first time, to get uninterrupted observations in a geostationary orbit. The SLD payload configuration, its in-flight operation, and the response of the detectors are presented. We also present the first observations of solar flares made by the SLD payload and briefly describe their temporal and spectral mode results. |
| Databáze: | OpenAIRE |
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