公开(公告)号：US3534376A

公开(公告)日：1970-10-13

申请号：US3534376D

申请日：1968-01-30

Applicant: WEBB JAMES E ,  NASA

Inventor： WOO KENNETH E

IPC: H01Q13/02 ,  H01Q13/06 ,  H01Q13/18

CPC classification number: H01Q13/06 ,  H01Q13/0241 ,  H01Q13/18

公开(公告)号：US3665481A

公开(公告)日：1972-05-23

申请号：US3665481D

申请日：1970-05-12

Applicant: NASA

Inventor： WOO KENNETH E

IPC: H01P1/16 ,  H01Q25/04 ,  H01Q19/14

CPC classification number: H01P1/16 ,  H01Q25/04

Abstract: A microwave antenna useful on a spacecraft, which utilizes a single dish reflector and single coaxial horn structure to transmit at two frequencies, and to receive signals at a third frequency that allow tracking. The horn structure includes a coaxial wave-guide with an inner pipe for transmitting X-band waves, an intermediate pipe, surrounding the inner pipe for transmitting S-band waves through the space between it and the inner pipe, and an outer pipe surrounding the intermediate pipe for receiving S-band tracking signals. An outer horn flares from the outer pipe and an inner horn flares from the inner pipe, to efficiently illuminate the dish reflector at both X and S bands.

Abstract translation: 用于航天器的微波天线，其利用单个碟形反射器和单个同轴喇叭结构以两个频率发射，并以允许跟踪的第三频率接收信号。 喇叭结构包括具有用于传输X波段的内管的同轴波导，围绕内管的中间管，用于通过其与内管之间的空间传输S波段，以及围绕着 用于接收S波段跟踪信号的中间管道。 外喇叭从外管弹起，内喇叭从内管弹起，以有效地在X和S带照射碟形反射器。