DocumentCode
2279401
Title
A low-cost, injection-molded satellite phased array
Author
Metzen, P.L.
Author_Institution
Space Syst./Loral, USA
fYear
2000
fDate
2000
Firstpage
219
Lastpage
222
Abstract
The current trend in synchronous orbit satellites and satellite antennas is toward increased power, increased payload capability, and more independent antenna beams. Spacecraft antennas must also be low in cost, be quickly produced, and fit within the available spacecraft mounting locations. The transmit and receive functions are often performed by separate antennas. A deployed shaped-reflector antenna is frequently used to satisfy the transmit requirements, and an Earth-facing, deck-mounted reflector antenna is used to satisfy the receive functions. An Earth-deck structure is necessary to hold the Ku-band receive antenna reflector, subreflector, and feed. An Earth-deck-mounted passive array antenna is being developed that has the same RF performance and the same mass as a 1.2 m reflector antenna, yet costs 75% less and occupies 80% less Earth-deck area and 95% less shroud volume. Furthermore, the array has a lower center of gravity which improves spacecraft inertial characteristics
Keywords
antenna phased arrays; microwave antenna arrays; moulding; receiving antennas; reflector antenna feeds; satellite antennas; transmitting antennas; Earth-deck structure; Ku-band antenna; deck-mounted reflector antenna; injection molding; passive array antenna; receiving antenna; reflector antenna feed; satellite antennas; satellite phased array; shaped-reflector antenna; spacecraft antennas; transmitting antenna; Antenna arrays; Costs; Feeds; Payloads; Phased arrays; Receiving antennas; Reflector antennas; Satellite antennas; Space vehicles; Transmitting antennas;
fLanguage
English
Publisher
ieee
Conference_Titel
Phased Array Systems and Technology, 2000. Proceedings. 2000 IEEE International Conference on
Conference_Location
Dana Point, CA
Print_ISBN
0-7803-6345-0
Type
conf
DOI
10.1109/PAST.2000.858944
Filename
858944
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