DocumentCode :
2073319
Title :
GOLGE: a case study of a secure data communication subsystem for micro-satellites
Author :
Yesil, S. ; Sever, R. ; Okcan, B. ; Ismailoglu, N.
Author_Institution :
Middle East Tech. Univ., Ankara, Turkey
fYear :
2005
fDate :
9-11 June 2005
Firstpage :
438
Lastpage :
441
Abstract :
This paper presents a real-time data encryption/decryption subsystem developed for a satellite, which is planned to be launched in 2007 by TUBITAK-BILTEN. The subsystem GOLGE contains two ASICs, which perform encryption/decryption using AES (Advanced Encryption Standard) and RSA (Rivest-Shamir-Adleman) algorithms and a communication interface unit. The data/command interface of the GOLGE module is implemented on a reconfigurable ASIC (FPGA), where the encryption/decryption processors have previously been designed in TUBITAK-BILTEN and prototyped in ANTIS 0.35-μm CMOS technology. The system uses an 8-bit bidirectional data bus, which operates at a maximum frequency of 40 MHz supplying a throughput of 160 Mbit/sec and a SpaceWire interface, which provides a 100 Mbit/sec serial data communication link.
Keywords :
CMOS integrated circuits; application specific integrated circuits; cryptography; field programmable gate arrays; satellite communication; AES; ASICs; CMOS; FPGA; GOLGE; Micro-Satellites; RSA; Rivest-Shamir-Adleman algorithm; SpaceWire interface; advanced encryption standard; bidirectional data bus; communication interface unit; data/command interface; real-time data encryption/decryption subsystem; secure data communication subsystem; Application specific integrated circuits; CMOS process; CMOS technology; Communication standards; Cryptography; Data communication; Field programmable gate arrays; Prototypes; Satellites; Space technology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies, 2005. RAST 2005. Proceedings of 2nd International Conference on
Print_ISBN :
0-7803-8977-8
Type :
conf
DOI :
10.1109/RAST.2005.1512607
Filename :
1512607
Link To Document :
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