| 发明名称 | Deployable satellite reflector with a low passive intermodulation design | ||
| 摘要 | A passive intermodulation modulation reducing structure for a multicarrier reflector system, including a plurality of flexible reflector gores, each gore having a thin layer of conductive metal, a first layer of dielectric material laminated to one face of the conductive metal, and a second layer of dielectric material laminated to an opposite face of the conductive metal. Capacitive coupling joins the reflector's RF components. The structure can be a deployable parabolic reflector for a satellite antenna. | ||
| 申请公布号 | US9112282(B2) | 申请公布日期 | 2015.08.18 |
| 申请号 | US201313735769 | 申请日期 | 2013.01.07 |
| 申请人 | The United States of America, as represented by the Secretary of the Navy | 发明人 | Nurnberger Michael W.;Amend Christopher P. |
| 分类号 | H01Q15/16;H01Q1/28;H01Q19/13 | 主分类号 | H01Q15/16 |
| 代理机构 | US Naval Research Laboratory | 代理人 | US Naval Research Laboratory ;Ferrett Sally A. |
| 主权项 | 1. A passive intermodulation modulation reducing structure for a multicarrier reflector system, comprising: a plurality of flexible reflector gores, each gore having a thin layer of conductive metal, a first layer of dielectric material laminated to one face of the conductive metal, and a second layer of dielectric material laminated to an opposite face of the conductive metal. | ||
| 地址 | Washington DC US | ||