The iXRD on Sharjah-Sat-1 CubeSat, the science mission, and ground calibration

Kalemci, Emrah and Alketbi, Fatima and Faroukh, Yousuf and Altıngün, Ali Mürteza and AlKaabi, Tarifa and Alhammadi, Amel and Alansaari, Maryam and Bozkurt, Ayhan and Fernini, Ilias and Aslan, Alim Rustem and Karabulut, Bogac and Manousakis, Antonios and Al Naimiy, Hamid and Yalçın, Refik and Gökalp, Kaya (2022) The iXRD on Sharjah-Sat-1 CubeSat, the science mission, and ground calibration. In: 73rd International Astronautical Congress, IAC 2022, Paris, France

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Abstract

The Sharjah-Sat-1 3U CubeSat is designed and realized together with the Sharjah Academy for Astronomy, Space Sciences, and Technology (SAASST), the University of Sharjah (UoS), Istanbul Technical University (ITU), and Sabanci University (SU). It has two scientific objectives: performing X-ray astronomy observations and capturing remote sensing and Earth observation images of the United Arab Emirates. The CubeSat is to be launched by the fourth quarter of 2022 and is currently in the Flight-Model integration phase. The primary science payload is the iXRD (Improved X-Ray Detector), with the main objective of observing very bright transient and persistent galactic hard X-ray sources. It will use a pixelated 5 mm CdZnTe-based crystal as an active material with an energy range of 25keV to 300keV and a spectral resolution between 5-10 keV at 60keV, depending on the pixel size. In addition, a Tungsten collimator with a field of view of 4.26 degrees and a tungsten shield at the back decreases the cosmic X-ray and Earth's albedo background. Its' second objective is solar observations to study the hard X-ray spectra of flares and coronal holes. Other potential targets are transient bright events (e.g., GRBs and magnetar bursts). This presentation will show the results of laboratory calibration, TVAC tests, and sensitivity analysis based on in-orbit background simulations to support its science objectives.
Item Type: Papers in Conference Proceedings
Uncontrolled Keywords: Calibration; CubeSat; Design; iXRD; Thermal-Vacuum Testing; Vibration Testing
Divisions: Faculty of Engineering and Natural Sciences
Depositing User: Emrah Kalemci
Date Deposited: 04 Sep 2023 16:33
Last Modified: 04 Sep 2023 16:33
URI: https://research.sabanciuniv.edu/id/eprint/47692

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