Title :
Multimedia Asia (M2A) satellite antennas
Author :
Schennum, Gary H. ; Tang, Minh
Author_Institution :
Space Syst. Loral, Palo Alto, CA, USA
Abstract :
The latest generation of high power communication and direct broadcast satellites often require the antenna subsystem to create several simultaneous isolated antenna beams. One such satellite with this requirement, currently under development at Space Systems/Loral, is termed the Multimedia Asia (M2A) satellite. The M2A spacecraft communications subsystem includes all the necessary antennas and repeaters to provide voice, fax, data, and Internet service simultaneously to the home. This service is scheduled to start at the end of 1999 in the defined coverage areas. The extended C-band coverage (3.4-3.7 GHz transmit, 6.425-6.725 GHz receive) will provide Asia beams and seven spot beams. The X-band feeder link (7.25-7.75 GHz transmit, 7.9-8.4 GHz receive) will provide additional Asia coverage. The standard C-band coverage (3.7-4.2 GHz transmit, 5.9-6.4 GHz receive) provides added coverage to Indonesia, Malaysia, Brunei and Hong Kong. The paper illustrates the M2A Communication Subsystem beams, their geographical coverage and downlink polarizations. The uplink polarizations are orthogonal to the downlink polarizations
Keywords :
direct broadcasting by satellite; electromagnetic wave polarisation; reflector antennas; satellite antennas; 3.4 to 3.7 GHz; 3.7 to 4.2 GHz; 5.9 to 6.4 GHz; 6.425 to 6.725 GHz; 7.25 to 7.75 GHz; 7.9 to 8.4 GHz; M2A satellite antennas; Multimedia Asia satellite; X-band feeder link; antenna subsystem; direct broadcast satellites; downlink polarizations; extended C-band coverage; isolated antenna beams; spacecraft communications subsystem; uplink polarizations; Asia; Downlink; Multimedia systems; Polarization; Power generation; Repeaters; Satellite antennas; Satellite broadcasting; Space vehicles; Web and internet services;
Conference_Titel :
Aerospace Conference, 1998 IEEE
Conference_Location :
Snowmass at Aspen, CO
Print_ISBN :
0-7803-4311-5
DOI :
10.1109/AERO.1998.685846