DocumentCode :
2239604
Title :
Small optical transponder for small satellites
Author :
Toyoshima, M. ; Takenaka, H. ; Shoji, Y. ; Takayama, Y. ; Koyama, Y. ; Akioka, M.
Author_Institution :
Space Commun. Group, Nat. Inst. of Inf. & Commun. Technol., Koganei, Japan
fYear :
2010
fDate :
21-23 July 2010
Firstpage :
558
Lastpage :
561
Abstract :
Space optical communications from small satellites need to be developed for the high-data-rate communications link to the ground. The requirements for the onboard resources are discussed with respect to the antenna diameter, the mass, and the consumption power. The development for a small optical transponder has begun and the data rate will be on the order of several ten-Mbps. The mass of the small optical transponder will be about 5 kg, which can be embarked on 50-kg-class small satellites as the piggyback of launch vehicles.
Keywords :
optical communication equipment; satellite links; space communication links; transponders; data rate communications link; optical transponder; small satellites; space optical communication; Antennas; Driver circuits; Optical sensors; Optical transmitters; Radio frequency;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Communication Systems Networks and Digital Signal Processing (CSNDSP), 2010 7th International Symposium on
Conference_Location :
Newcastle upon Tyne
Print_ISBN :
978-1-4244-8858-2
Electronic_ISBN :
978-1-86135-369-6
Type :
conf
Filename :
5580351
Link To Document :
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