DocumentCode :
1882309
Title :
Multigigabit optical transceivers for high data rate military applications
Author :
Catanzaro, Brian ; Kuznia, Charlie
Author_Institution :
CFE Services, San Diego, CA, USA
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
7
Abstract :
Avionics has experienced an ever increasing demand for processing power and communication bandwidth. Currently deployed avionics systems require gigabit communication using optoelectronic transceivers connected with parallel optical fiber. Ultra Communications has developed a series of transceiver solutions combining ASIC technology with flip-chip bonding and advanced opto-mechanical molded optics. Ultra Communications custom high speed ASIC chips are developed using an SoS (silicon on sapphire) process. These circuits are flip chip bonded with sources (VCSEL arrays) and detectors (PIN diodes) to create an OptoElectronic Integrated Circuit (OEIC). These have been combined with micro-optics assemblies to create transceivers with interfaces to standard fiber array (MT) cabling technology. We present an overview of the demands for transceivers in military applications and how new generation transceivers leverage both previous generation military optical transceivers as well as commercial high performance computing optical transceivers.
Keywords :
application specific integrated circuits; data communication; military communication; optical transceivers; ASIC technology; PIN diodes; VCSEL arrays; avonics; communication bandwidth; fiber array cabling technology; flip-chip bonding; high data rate military applications; micro-optics assemblies; multigigabit optical transceivers; opto-mechanical molded optics; optoelectronic integrated circuit; power bandwidth; silicon on sapphire; Connectors; Optical fibers; Optical interconnections; Optical transmitters; Transceivers;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187163
Filename :
6187163
Link To Document :
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