发明名称 |
Shaped reflector antenna system configuration for use on a communication satellite |
摘要 |
A shaped reflector antenna system for use on a communication satellite that comprises a plurality of shaped reflector antenna configurations. In an exemplary system, a first one of the antenna configurations is a diverged shaped reflector antenna and a second one of the antenna configurations is a converged shaped reflector antenna. Each of the shaped reflector antennas comprise a main reflector, a subreflector, and a feed horn. The feed horn illuminates the subreflector with RF energy in the shape of a feed cone that is reflected to the main reflector. The direction of RF energy propagation emitted by each of the shaped reflector antennas is in a direction that is different from a direction defined by a vector between a predetermined vertex and focal point associated with the respective shaped reflector antenna. In a specific embodiment, the direction of the coverage for the diverged shaped reflector antenna is counterclockwise with respect to a direction defined by a vector between a predetermined vertex and focal point associated with the shaped reflector antenna. The direction of the coverage for the converged shaped reflector antenna is clockwise with respect to a direction defined by a vector between a predetermined vertex and focal point associated with the shaped reflector antenna.
|
申请公布号 |
US6411262(B1) |
申请公布日期 |
2002.06.25 |
申请号 |
US20000643269 |
申请日期 |
2000.08.22 |
申请人 |
SPACE SYSTEMS/LORAL, INC. |
发明人 |
LUH HOWARD HO-SHOU;SUAREZ-BARNES I. MARIANA |
分类号 |
H01Q19/18;H01Q1/28;H01Q19/02;H01Q19/19;(IPC1-7):H01Q19/14 |
主分类号 |
H01Q19/18 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|