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  • Link budget analysis for small optical transponder onboard small satellites

    Paper number

    IAC-10.B2.5.5

    Author

    Dr. Morio Toyoshima, National Institute of Information and Communications Technology, Japan

    Coauthor

    Mr. Hideki Takenaka, National Institute of Information and Communications Technology, Japan

    Coauthor

    Dr. Yozo Shoji, National Institute of Information and Communications Technology, Japan

    Coauthor

    Dr. Yoshihisa Takayama, National Institute of Information and Communications Technology, Japan

    Coauthor

    Mr. Yoshisada Koyama, National Institute of Information and Communications Technology, Japan

    Coauthor

    Dr. Maki Akioka, National Institute of Information and Communications Technology, Japan

    Year

    2010

    Abstract
    Satellite communications are important to various space-based activities, such as data reception from earth-observation satellites, communication links with manned space stations, and in-orbit operations of space planes.  In particular, optical communication systems have various advantages over other types of communications. They have smaller and lighter equipment, higher data rates, larger communication capacities, limited risk of interference with other optical communication systems, and no licensing requirements or tariffs.
    Recently, the activities on the development of small satellites are very active; however, the small satellite community still uses 9.6-kbps communication links by employing ham radio communications because of resource constraints in the nano-class satellites. The compact terminal can be used in nano-class satellites that have a mass of the order of a few tens of kilograms. In addition, there is a significant advantage with regard to the frequency-licensing problems faced by satellites, and the optical frequency carrier will be very useful to the small satellite community. Therefore, the National Institute of Information and Communications Technology (NICT) has begun to develop a Small Optical TrAnsponder (SOTA) onboard a small satellite, which project is called the Space Optical Communications Research Advanced Technology Satellite (SOCRATES).  The link budget analyses between a low earth orbit (LEO) satellite and an optical ground station (OGS), a geostationary earth orbit (GEO) satellite and the OGS, and the LEO and the GEO are performed by assuming the SOTA onboard small satellites.  
    In this paper, the results of the link budget analyses for the SOTA are presented and its application to small satellites is proposed.
    Abstract document

    IAC-10.B2.5.5.brief.pdf

    Manuscript document

    IAC-10.B2.5.5.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.