MA
Mehmet Deniz Aksulu
info
Please Note
<p>This page displays the records of the person named above and is not linked to a unique person identifier. This record may need to be merged to a profile.</p>
4 records found
1
Conference paper
(2015)
-
Emrah Kalemci, Alim Rustem Aslan, Mustafa Erdem Bas, Mehmet Deniz Aksulu, Isa Eray Akyol, Mehmet Sevket Uludag
A CdZnTe based semiconductor X-ray detector (XRD) and its associated readout electronics has been developed by the Space Systems Design and Testing Laboratory of Istanbul Technical University and the High Energy Astrophysics Detector I-Aboratory of Sabanci University along with an SME partner. The XRD will be the secondary science mission on board BeEagleSat, which is developed as one of the double CubeSats for the QB50 project. QB50 is a European Framework 7 projcct carried out by a number of international organizations led by the von Karman Institute of Belgium. The heart of the XRD is a 2.5 mm thick, 15 mm x 15 mm CdZnTe crystal with orthogonal electrode strips on top and bottom for position resolution on the crystal. There are 3 sets of steering electrodes in between anodes. A commercial off the shelf (COTS) high voltage source provides necessary potential difference to transport electrons and holes towards electrodes. The signals from each strip are read by a COTS ASIC, RENA-3b, controlled my MSP 430. The XRD board (single -10 cm x 10 cm board) also carries the necessary power regulators and 7 COTS batteries. In a previous paper presented at the IAC 2014, we discussed the main design of the XRD and provided results from some of the early vibration tests of the mechanical design. At the time, the CdZnTe crystal has not been attached, and the readout electronics and software were still in development phase. In this paper, we present the laboratory performance of the electronic readout system and discuss the current phase of the XRD development.
...
A CdZnTe based semiconductor X-ray detector (XRD) and its associated readout electronics has been developed by the Space Systems Design and Testing Laboratory of Istanbul Technical University and the High Energy Astrophysics Detector I-Aboratory of Sabanci University along with an SME partner. The XRD will be the secondary science mission on board BeEagleSat, which is developed as one of the double CubeSats for the QB50 project. QB50 is a European Framework 7 projcct carried out by a number of international organizations led by the von Karman Institute of Belgium. The heart of the XRD is a 2.5 mm thick, 15 mm x 15 mm CdZnTe crystal with orthogonal electrode strips on top and bottom for position resolution on the crystal. There are 3 sets of steering electrodes in between anodes. A commercial off the shelf (COTS) high voltage source provides necessary potential difference to transport electrons and holes towards electrodes. The signals from each strip are read by a COTS ASIC, RENA-3b, controlled my MSP 430. The XRD board (single -10 cm x 10 cm board) also carries the necessary power regulators and 7 COTS batteries. In a previous paper presented at the IAC 2014, we discussed the main design of the XRD and provided results from some of the early vibration tests of the mechanical design. At the time, the CdZnTe crystal has not been attached, and the readout electronics and software were still in development phase. In this paper, we present the laboratory performance of the electronic readout system and discuss the current phase of the XRD development.
Conference paper
(2015)
-
A Rustem Aslan, M Erdem Bas, M Sevket Uludag, Sibel Turkoglu, I Eray Akyol, M Deniz Aksulu, Erdinc Yakut, Murat Suer, Bogac Karabulut, Ahmet Sofyali
Conference paper
(2014)
-
A.R. Aslan, E. Kalemci, M.E. Bas, I.E. Akyol, M.S. Uludag, M.D. Aksulu, E. Umit
Conference paper
(2013)
-
A.R. Aslan, H.B. Yagci, M.E. Umit, A. Sofyali, M.E. Bas, M.S. Uludag, O.E. Ozen, M.D. Aksulu, E. Yakut, More Authors...