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  • Elliptic Orbit Communication System Molniya-Zond: Launch, Spacecraft Assembling and Communication Equipment

    Paper number

    IAC-05-B3.4.04

    Author

    Dr. Yuri Ulybyshev, S.P. Korolev Rocket and Space Corporation Energia, Russia

    Coauthor

    Dr. Victor N. Doniants, Zond-Holdings, Russia

    Coauthor

    Mr. Evgeny Zemskov, S.P. Korolev Rocket and Space Corporation Energia, Russia

    Year

    2005

    Abstract
    An overview of the satellite communication  system MOLNIYA-ZOND using a mid-altitude elliptic orbit constellation, focusing on the spacecraft launch and main features of the space segment , including the spacecraft assembling  and communication equipment, is presented. The MOLNIYA-ZOND  will  provide a zonal  communication for North hemisphere areas (such as the Russia, Canada, and North Europe). The space segment consists six satellites on a MOLNIYA-type orbit placed in two orbital planes (at elliptic 4-hours orbit with critical inclination and apogee in the North hemisphere).  For the spacecraft launch to orbit will be used the launch vehicle SOYUZ-2 with the boost block FREGAT for simultaneously launch of three spacecraft or the launch vehicle DNEPR for single launch. The spacecraft assembling based on the universal space bus VICTORIA and placing at payload fairing are  described. Orbit positioning strategies, in case of cluster and single launch, using the spacecraft propulsion including possible constellation reconfiguration are presented. Station-keeping requirements based on an analysis for long-term changes of satellite constellation coverage and communication network characteristics. Connection between user terminals is established through satellites and fixed terrestrial gateways. The mobile links (between the user terminals and the satellites) will operate at the 312-315 MHz for uplink and 387-390 MHz for downlink, the feeder links (between the control center/gateway Earth stations and the satellites) will operate at the Ku-band (11/14 GHz). Communication equipment for the MOLNIYA-ZOND spacecraft is shortly described.
    Abstract document

    IAC-05-B3.4.04.pdf

    Manuscript document

    IAC-05-B3.4.04.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.