DocumentCode
1220811
Title
The SOUT optical intersatellite communication terminal
Author
Baister, G. ; Gatenby, P. ; Lewis, J. ; Wittig, M.
Author_Institution
Matra Marconi Space UK, Stevenage, UK
Volume
141
Issue
6
fYear
1994
fDate
12/1/1994 12:00:00 AM
Firstpage
345
Lastpage
355
Abstract
Optical communications links between satellites promise to become an important element of future space infrastructure and are the subject of considerable development in Europe. Major advantages over conventional microwave links are low mass and power and smaller size leading to easier accommodation on the satellite. The Small Optical User Terminal (SOUT) is an optical communications package for interconnecting a low earth orbiting satellite to future optical data relay terminals and is the subject of an ESA development programme led by MMS (UK). The baseline terminal has a data rate of 2 Mbps over the return interorbit link and a mass of around 25 kg. The terminal configuration uses a unique combination of a periscopic coarse pointing assembly, refractive telescope, passive antivibration mount, combined acquisition and tracking sensor, and fibre coupled lasers and receivers. The paper discusses the design aspects for an asymmetric optical link based on the SOUT, covering link budgets, pointing, acquisition, and tracking and communications performance. Key SOUT subsystems are described and the structural and thermal configuration which allows these features to be combined in a compact unit is reported
Keywords
optical links; space communication links; telecommunication terminals; 2 Mbit/s; 25 kg; SOUT optical intersatellite communication terminal; Small Optical User Terminal; baseline terminal; combined acquisition and tracking sensor; compact unit; fibre coupled lasers; link budgets; low earth orbiting satellite; low mass; low power; optical communications links; optical communications package; optical data relay terminals; passive antivibration mount; periscopic coarse pointing assembly; receivers; refractive telescope; return interorbit link; smaller size; structural configuration; thermal configuration;
fLanguage
English
Journal_Title
Optoelectronics, IEE Proceedings -
Publisher
iet
ISSN
1350-2433
Type
jour
DOI
10.1049/ip-opt:19941557
Filename
342259
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