, where RE is radius of Earth, RSR is the radius of the orbit SR, h is the minimum allowable height of the passage of the intersatellite line above the Earth's surface.;EFFECT: technical result consists in developing a method which enables to establish minimum required parameters of a low-orbital spacecraft transmitting system, represented in the form of equivalent isotropically emitted power, by taking into account features of transmitting information over an inter-satellite line to a high-orbit relay satellite.;1 cl, 4 dwg, 1 tbl"/>
机译:在低圆轨道上的航天飞机发射系统的等效等效辐射功率的确定方法
公开/公告号RU2699821C2
专利类型
公开/公告日2019-09-11
原文格式PDF
申请/专利权人 AKTSIONERNOE OBSHCHESTVO INFORMATSIONNYE SPUTNIKOVYE SISTEMY IMENI AKADEMIKA M.F. RESHETNEVA;
申请/专利号RU20170143276
申请日2017-12-11
分类号H04B7/185;
国家 RU
入库时间 2022-08-21 11:45:59