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Passive alignment optical subassemblies for military/aerospace fiber-optic transmitter/receiver modules

Under the DARPA sponsored Avionics Optoelectronic Module Technology program, new passive alignment carrier (PAC) optical subassemblies (LED-PAC and PIN-PAC) ruggedized for military/aerospace avionics fiber-optic transmitter and receiver applications have been developed, LED-PAC and PIN-PAC silicon m...

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Bibliographic Details
Published in:IEEE transactions on advanced packaging 2000-08, Vol.23 (3), p.461-469
Main Authors: Beranek, M.W., Chan, E.Y., Chiu-Chao Chen, Davido, K.W., Hager, H.E., Chi-Shain Hong, Koshinz, D.G., Rassaian, M., Soares, H.P., St. Pierre, R.L., Anthony, P.j., Cappuzzo, M.A., Gates, J.V., Gomez, L.T., Henein, G.E., Shmulovich, J., Occhionero, M.A., Fennessy, K.P.
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Language:English
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Summary:Under the DARPA sponsored Avionics Optoelectronic Module Technology program, new passive alignment carrier (PAC) optical subassemblies (LED-PAC and PIN-PAC) ruggedized for military/aerospace avionics fiber-optic transmitter and receiver applications have been developed, LED-PAC and PIN-PAC silicon micro-optical bench substrates were fabricated together on a 5 in diameter silicon wafer via multistage photolithography, thin-film, and substrate processing. Alignment v-grooves designed for passive optical alignment of 100/140 /spl mu/m multimode optical fiber to the optoelectronic devices were terminated by solder locking the fiber to the silicon PAC substrates. The LED-PAC comprising a surface emitting LED die-bonded onto a novel precision molded AM submount passively mounted onto the silicon microbench achieves the required high coupling efficiency to 100/140 /spl mu/m multimode optical fiber to meet stringent avionics transmitter output power requirements. The 100/130 /spl mu/m multimode optical fiber-pigtailed PIN-PAC with a refractive lens etched into the p-i-n photodiode backside surface exhibited responsivities greater than 0.8 A/W at 1.3 /spl mu/m wavelength. The LED-PAC and PIN-PAC optical subassemblies integrated with Boeing ARINC 636 (FDDI) transmitter and receiver thick film multichip (MCM-C) circuitry are capable of meeting both ARINC 636 and FDDI physical layer requirements.
ISSN:1521-3323
1557-9980
DOI:10.1109/6040.861561