Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
9823130 | Acta Astronautica | 2005 | 9 Pages |
Abstract
The MBSAT spacecraft was launched on 13 March 2004 from Cape Canaveral Air Force Station on an Atlas III-A launch vehicle. The satellite is now in service at its orbital location of 144âE longitude. The satellite is designed to provide high-quality audio, video and data services to mobile users in Japan and Korea. Broadcast transmissions use 25Â MHz of bandwidth at the S-band frequency of 2.6Â GHz, while uplinks and feeder links to terrestrial repeaters use the Ku-band. The MBSAT satellite design incorporates a large, unfurlable, mesh reflector for S-band broadcast. This 12Â m (effective aperture) reflector coupled with phase-combined arrays of Traveling Wave Tube Amplifiers result in Effective Isotropic Radiated Power levels of 67-69Â dBW over Japan and Korea coverage areas. The use of Stationary Plasma Thrusters for North-South stationkeeping significantly enhances the mission lifetime as well as minimizes potential disturbances to the 12Â m reflector.
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Authors
Masashi Suenaga, Robert J. Prevaux,