发明名称 DATA REPEAT SATELLITE SYSTEM
摘要 PURPOSE:To distribute a data from a spacecraft continuously to the user on ground by arranging two data repeat satellites whose longitude is apart nearly by 180 deg. onto a counter-ground stationary orbit, arranging an earth station to a longitude respectively close to the stationary orbit and connecting the earth station with on-ground network. CONSTITUTION:The system consists of two data repeat satellites 1, 2 arranged to a counter-ground stationary orbit whose longitude is apart nearly by 180 deg. arranged, two earth stations 3, 4 arranged to the longitude close to the data repeat satellites 1, 2 and an on-ground network 5 interconnecting the two earth stations 3, 4. Thus, any of the data repeat satellites on two counter-ground stationary orbits whose longitude is apart nearly by 180 deg. at all times is in a visible area of a spacecraft circulating on a low altitude orbit whose altitude is less than 1200km and more than 73km and a data from the spacecraft 6 is sent to the earth station 3 or 4 via the data repeat satellites 1, 2. Thus, the data from the spacecraft 6 is continuously transmitted onto ground.
申请公布号 JPH03278726(A) 申请公布日期 1991.12.10
申请号 JP19900079854 申请日期 1990.03.28
申请人 NEC CORP 发明人 KATO HIRONORI
分类号 B64G99/00;H04B7/195 主分类号 B64G99/00
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